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MAINTENANCE / OPERATIONAL / PLACARDING PROCEDURES MANUAL Including Aircraft GV-SP (G550/G500) and Aircraft GIV-X (G450/G350) Revision 8 November 7, 2014 GAC DOC. No. V-1 C 2014 Gulfstream Aerospace DISCLAIMER FOR MAINTENANCE / OPERATIONAL / PLACARDING PROCEDURES MANUAL (GAC DOC. NO. GV-1) The technical information presented herein has been determined to be correct at time of publication. However, should a direct conflict exist between this and other official publications, e.g., Master Minimum Equipment List (MMEL), Airplane Flight Manuals (AFM), Maintenance Manuals, those publications take precedence. COPYRIGHT 2014 GULFSTREAM AEROSPACE CORPORATION All rights reserved, including the right to reproduce this publication. No part may be reproduced, stored in any retrieval system, or transmitted in any part or form or by any means, electronic, photocopying, microfilm, microfiche, mechanical, or otherwise, without prior written permission of Gulfstream Aerospace Corporation. TABLE OF CONTENTS PAGE FRONT MATTER ....................................................................................................................................................................................................................................................... F-1 Table of Contents ................................................................................................................................................................................................................................ F-1 General Information .......................................................................................................................................................................................................................... F-14 Revision Log ..................................................................................................................................................................................................................................... F-16 Minimum Navigational Equipment Table ......................................................................................................................................................................................... F-18 En Route Navigation Requirements .................................................................................................................................................................................................. F-20 Future Air Navigation System (FANS) Requirement ....................................................................................................................................................................... F-21 SECTION ONE – LINE REPLACEABLE UNIT (LRU) COMPONENT RELIEF ............................................................................................................................................. 1-1 ATA 21 AIR CONDITIONING ........................................................................................................................................................................................................................... 21-1 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. Cabin Altitude Indicator (Overhead Panel) ....................................................................................................................................................................................... 21-1 Cabin Differential Pressure Indicator ................................................................................................................................................................................................ 21-2 HON TUS Calculator ........................................................................................................................................................................................................................ 21-3 Cabin Rate of Climb Indicator .......................................................................................................................................................................................................... 21-4 Automatic Pressurization Control Systems ....................................................................................................................................................................................... 21-4 Manual Pressurization Control System ............................................................................................................................................................................................. 21-5 Semi-Auto Pressurization Control System ........................................................................................................................................................................................ 21-5 Cabin Altitude Pressure Warning System ......................................................................................................................................................................................... 21-6 Pressurization Outflow Valve Position Indicator .............................................................................................................................................................................. 21-6 Cockpit Zone Temperature Control System & Cabin Zone Temperature Control Systems.............................................................................................................. 21-7 Cockpit/Cabin Zone Temperature Indicators (Overhead Panel) ....................................................................................................................................................... 21-8 Duct Temperature Indicators (Overhead Panel) ................................................................................................................................................................................ 21-8 Environmental Control System (ECS) Packs .................................................................................................................................................................................... 21-9 Three-In-One Cabin Pneumatic Pressurization Monitoring Instrument ............................................................................................................................................ 21-9 Air Conditioning System Pack Inlet Valves .................................................................................................................................................................................... 21-10 Outflow Valve System .................................................................................................................................................................................................................... 21-10 Pressure Relief Valve ...................................................................................................................................................................................................................... 21-11 Cabin Pressure Indicator and Control Panel .................................................................................................................................................................................... 21-12 Selector Panel (Semi-Auto) ............................................................................................................................................................................................................. 21-13 Remote Filter (Pressure Relief Valve PRV) .................................................................................................................................................................................... 21-13 CPAM (Cabin Pressure Acquisition Module) ................................................................................................................................................................................. 21-13 Ram Air System .............................................................................................................................................................................................................................. 21-14 PSU Fan .......................................................................................................................................................................................................................................... 21-15 Front Matter F-1 TABLE OF CONTENTS (CONTINUED) ATA 22 AUTO FLIGHT ...................................................................................................................................................................................................................................... 22-1 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. ATA 23 Autothrottle Systems ......................................................................................................................................................................................................................... 22-1 Performance Management Systems (SmartPerf/TOLD) ................................................................................................................................................................... 22-1 Control Wheel Autopilot Disconnect Buttons ................................................................................................................................................................................... 22-1 Autothrottle Disconnect Buttons (on Thrust Lever Handles) ............................................................................................................................................................ 22-2 Autothrottle Engage/Disengage Switches (on Thrust Lever Stem) ................................................................................................................................................... 22-2 Touch Control Steering Switches (TCS) ........................................................................................................................................................................................... 22-2 Autopilots (Flight Guidance Computer (FGC) / Flight Directors) .................................................................................................................................................... 22-3 Yaw Damper Systems ....................................................................................................................................................................................................................... 22-3 Takeoff/Go-Around (TO/GA) Buttons (on Power Lever Handles) ................................................................................................................................................... 22-4 Mach Trim Systems (GV/SP/G-IV-X only) ...................................................................................................................................................................................... 22-5 COMMUNICATIONS ........................................................................................................................................................................................................................... 23-1 1. Communications Systems (VHF, UHF) ............................................................................................................................................................................................ 23-1 2. Cockpit Voice Recorder (CVR) ........................................................................................................................................................................................................ 23-2 3. Selective Call System (SELCAL) ..................................................................................................................................................................................................... 23-3 4. Emergency Locator Transmitters (ELT) ........................................................................................................................................................................................... 23-4 5. Crewmember Interphone System ...................................................................................................................................................................................................... 23-5 6. Interphone Systems ........................................................................................................................................................................................................................... 23-8 7. Cockpit Speakers ............................................................................................................................................................................................................................... 23-8 8. Passenger Address Systems (PA) ...................................................................................................................................................................................................... 23-9 9. Satellite Communication Systems ................................................................................................................................................................................................... 23-11 10. Prerecorded Passenger Announcement Systems ............................................................................................................................................................................. 23-11 11. Flight Deck Hand Microphones ...................................................................................................................................................................................................... 23-11 12. Flight Deck Headsets Earphones / Headphones and Boom Microphones ....................................................................................................................................... 23-12 13. Right Side Radio Frequency Management Unit (RFMU) (GV)...................................................................................................................................................... 23-14 14. Alerting System (Audio/Visual) ...................................................................................................................................................................................................... 23-14 15 Handset Systems ............................................................................................................................................................................................................................. 23-15 16. Radio Tuning Functions (GV-SP, GIV-X) ...................................................................................................................................................................................... 23-16 17. High Frequency (HF) Communication Systems ............................................................................................................................................................................. 23-17 18. NAVCOM Radio (GV-SP, GIV-X) ................................................................................................................................................................................................ 23-17 19. Audio Interface Units (AIUs) (GV only) ........................................................................................................................................................................................ 23-18 20. Datalink System (GV) ..................................................................................................................................................................................................................... 21-18 21. Modular Radio Cabinet (MRC) Power Supplies (GV-SP, GIV-X) ................................................................................................................................................. 23-19 22. Headsets .......................................................................................................................................................................................................................................... 23-19 23. Flight Deck Hand Microphones ...................................................................................................................................................................................................... 23-19 24. Communications Management Function / CMF (GV-SP/GIV-X) .................................................................................................................................................. 23-20 25. Controller Pilot Data Link Communications (CPDLC) .................................................................................................................................................................. 23-20 Front Matter F-2 TABLE OF CONTENTS (CONTINUED) ATA 24 ELECTRICAL POWER ........................................................................................................................................................................................................................ 24-1 1. Engine Generators ............................................................................................................................................................................................................................. 24-1 2. APU Generator .................................................................................................................................................................................................................................. 24-4 3. Transformer-Rectifier Units (TRUs) ................................................................................................................................................................................................. 24-4 4. Battery Chargers ................................................................................................................................................................................................................................ 24-5 5. Main Airplane Batteries .................................................................................................................................................................................................................... 24-5 6. Battery Ammeters (Overhead Panel)................................................................................................................................................................................................. 24-6 7. Battery Voltmeters ............................................................................................................................................................................................................................ 24-6 8. Electrical Power System EICAS Displays ........................................................................................................................................................................................ 24-7 9. Master Power Switch Lights (Left, Right, APU, EXT) ................................................................................................................................................................... 24-11 10. Battery Temperature Indicating System .......................................................................................................................................................................................... 24-11 11. Standby Electrical System ............................................................................................................................................................................................................... 24-11 12. External Power System ................................................................................................................................................................................................................... 24-12 13. Low Battery Power Audible Warning System (Sonalert) ............................................................................................................................................................... 24-12 14. Ground Service Bus System ............................................................................................................................................................................................................ 24-12 15. 50Hz/60Hz AC Electrical Power Systems ...................................................................................................................................................................................... 24-12 16. IRU Back Up Batteries (GV) .......................................................................................................................................................................................................... 24-12 ATA 25 EQUIPMENT/FURNISHINGS ............................................................................................................................................................................................................. 25-1 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. Overwater Equipment........................................................................................................................................................................................................................ 25-1 Passenger Seats ................................................................................................................................................................................................................................. 25-1 Crewmember Shoulder Harnesses ..................................................................................................................................................................................................... 25-4 Observer Seat(s) ................................................................................................................................................................................................................................ 25-5 Megaphones ...................................................................................................................................................................................................................................... 25-6 Floatation Devices ............................................................................................................................................................................................................................. 25-6 "Fasten Seat Belt While Seated" Signs or Placards ........................................................................................................................................................................... 25-7 Storage Bins/Cabin, Galley and Lavatory Storage Compartment/Closets ........................................................................................................................................ 25-7 Cargo Restraint System ..................................................................................................................................................................................................................... 25-9 Flight Attendant Seat Assembly ...................................................................................................................................................................................................... 25-10 Galley/Cabin Waste Receptacles Access Doors/Covers ................................................................................................................................................................. 25-12 Exterior Lavatory Door Ashtrays .................................................................................................................................................................................................... 25-13 External Camera System ................................................................................................................................................................................................................. 25-13 Emergency Vision Assurance System (EVAS) ............................................................................................................................................................................... 25-13 Pilot Seat(s) ..................................................................................................................................................................................................................................... 25-14 Rudder Pedal Adjustment ................................................................................................................................................................................................................ 25-15 Cockpit Convenience Items............................................................................................................................................................................................................. 25-15 Keyed Locks .................................................................................................................................................................................................................................... 25-15 Front Matter F-3 TABLE OF CONTENTS (CONTINUED) ATA 25 EQUIPMENT/FURNISHIGNS (continued) ....................................................................................................................................................................................... 25-15 19. 20. 21. 22. 23. 24. 25. ATA 26 FIRE PROTECTION ............................................................................................................................................................................................................................. 26-1 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. ATA 27 Airplane Ladders ............................................................................................................................................................................................................................. 25-15 Baggage Compartment Shelves ....................................................................................................................................................................................................... 25-16 Crewmember Flashlight Holder Assemblies (Including Flashlight) ............................................................................................................................................... 25-16 Non-Essential Equipment & Furnishings NEF ............................................................................................................................................................................... 25-17 Automatic External Defibrillator (AED) and/or Associated Equipment ......................................................................................................................................... 25-18 Emergency Medical Kit (EMK) and/or Associated Equipment ...................................................................................................................................................... 25-18 First Aid Kit and/or Associated Equipment .................................................................................................................................................................................... 25-19 Portable Fire Extinguishers ............................................................................................................................................................................................................... 26-1 Wing Overheat Warning Systems ..................................................................................................................................................................................................... 26-1 APU Fire Detection System .............................................................................................................................................................................................................. 26-1 Rear Baggage Compartment Smoke Detector Systems ..................................................................................................................................................................... 26-2 Lavatory Smoke Detection Systems .................................................................................................................................................................................................. 26-3 Lavatory Fire Extinguisher Systems ................................................................................................................................................................................................. 26-4 Galley Smoke Detection Systems ..................................................................................................................................................................................................... 26-4 Galley Fire Extinguishing Systems ................................................................................................................................................................................................... 26-5 Engine Fire Detection Systems ......................................................................................................................................................................................................... 26-5 Flame Detectors................................................................................................................................................................................................................................. 26-5 Electronic Equipment Rack Overheat Warning System .................................................................................................................................................................... 26-5 Passenger Compartment Closet Smoke Detectors ............................................................................................................................................................................. 26-5 Entranceway Baggage Compartment Smoke Detectors .................................................................................................................................................................... 26-6 Cargo Compartment Fire Detection/Suppression Systems ................................................................................................................................................................ 26-6 APU Fire Bottle ................................................................................................................................................................................................................................. 26-7 FLIGHT CONTROLS ........................................................................................................................................................................................................................... 27-1 1. 2. 3. 4. 5. 6. 7. 8. 9. Rudder Limit Indication System ....................................................................................................................................................................................................... 27-1 Single Rudder Indication System ...................................................................................................................................................................................................... 27-1 Automatic Ground Spoiler System .................................................................................................................................................................................................... 27-1 Electric Elevator Trim System .......................................................................................................................................................................................................... 27-1 Control Wheel Elevator Trim Switches ............................................................................................................................................................................................ 27-2 Flap/Stabilizer Control Channels ...................................................................................................................................................................................................... 27-2 Single Speed Brake Indication System .............................................................................................................................................................................................. 27-2 Elevator Trim Actuator Heater Systems ............................................................................................................................................................................................ 27-2 Aileron Trim Actuator Heater ........................................................................................................................................................................................................... 27-3 Front Matter F-4 TABLE OF CONTENTS (CONTINUED) ATA 27 FLIGHT CONTROLS (continued)........................................................................................................................................................................................................ 27-3 10. 11. 12. 13. 14. 15. 16. ATA 28 FUEL ....................................................................................................................................................................................................................................................... 28-1 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. ATA 29 Autopilot Elevator Servos (GV-SP, GIV-X) ..................................................................................................................................................................................... 27-3 Autopilot Pitch Trim Servos (GV-SP, GIV-X) ................................................................................................................................................................................. 27-3 Autopilot Aileron Servos (GV-SP, GIV-X) ...................................................................................................................................................................................... 27-3 Autopilot Yaw Damper Servos (GV-SP, GIV-X) ............................................................................................................................................................................. 27-4 Stall Barrier Systems ......................................................................................................................................................................................................................... 27-4 Flight Control Synoptic Display........................................................................................................................................................................................................ 27-5 Gust Lock .......................................................................................................................................................................................................................................... 27-5 Fuel Tank Temperature Systems ....................................................................................................................................................................................................... 28-1 EICAS or Standby RFMU (GV) / MCDU (GV-SP, GIV-X) Fuel Quantity Indicating Systems ..................................................................................................... 28-1 Fuel Low Quantity Warning Systems ............................................................................................................................................................................................... 28-3 Fuel Boost Pumps.............................................................................................................................................................................................................................. 28-3 Fuel Intertank Valve .......................................................................................................................................................................................................................... 28-4 Heated Fuel Return System (HFRS) (GV, GV-SP)........................................................................................................................................................................... 28-4 Fuel Boost Pump Warning Systems .................................................................................................................................................................................................. 28-4 Fuel Crossflow Valve ........................................................................................................................................................................................................................ 28-5 Pressure Fueling System (Single Point Refueling) ............................................................................................................................................................................ 28-6 Ground Service Control Panel ........................................................................................................................................................................................................... 28-6 Automatic Fueling System ................................................................................................................................................................................................................ 28-6 Fuel Cap Chains ................................................................................................................................................................................................................................ 28-6 Single Point Refueling Cap ............................................................................................................................................................................................................... 28-7 Mid Wing Ejector (MWE) System (GV, GV-SP) ............................................................................................................................................................................. 28-7 HYDRAULIC POWER ......................................................................................................................................................................................................................... 29-1 1. 2. 3. 4. 5. 6. 7. 8. 9. Brake Accumulator Pressure Gauge (Nose Wheel Well) .................................................................................................................................................................. 29-1 Auxiliary Hydraulic Pump Pressure Indicator................................................................................................................................................................................... 29-1 Power Transfer Unit (PTU) Hydraulic Pressure Indication............................................................................................................................................................... 29-1 PTU Hydraulic Pump (Auto Mode) .................................................................................................................................................................................................. 29-1 Auxiliary Hydraulic Pump (Auto Mode) .......................................................................................................................................................................................... 29-1 Left Hydraulic System Quantity Gauge (Ground Service Control Panel - Aft Equipment Area) ..................................................................................................... 29-2 Right Hydraulic System Quantity Gauge (Ground Service Control Panel - Aft Equipment Area) ................................................................................................... 29-2 Left Hydraulic System Quantity Indication (EICAS) ....................................................................................................................................................................... 29-2 Right Hydraulic System Quantity Indication (EICAS) ..................................................................................................................................................................... 29-2 Front Matter F-5 TABLE OF CONTENTS (CONTINUED) ATA 29 HYDRAULIC POWER (continued) ...................................................................................................................................................................................................... 29-2 10. 11. 12. 13. ATA 30 ICE AND RAIN PROTECTION .......................................................................................................................................................................................................... 30-1 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. ATA 31 Hydraulic Reservoir Temperature Sensors ........................................................................................................................................................................................ 29-3 Hydraulic Reservoir Replenishing System ........................................................................................................................................................................................ 29-3 Brake Accumulator Pressure Gauge (cockpit dial) ........................................................................................................................................................................... 29-3 Brake Synoptic Page Accumulator Pressure Indication .................................................................................................................................................................... 29-4 Cowl Anti-Ice Pressure Indication Systems ...................................................................................................................................................................................... 30-1 Wing Anti-Ice Systems ..................................................................................................................................................................................................................... 30-1 Windshield Heat Systems .................................................................................................................................................................................................................. 30-2 Side Window Heat Systems .............................................................................................................................................................................................................. 30-2 Anti-Ice Heater Switch Lights ........................................................................................................................................................................................................... 30-3 Pitot Heaters ...................................................................................................................................................................................................................................... 30-3 Ice Detection Systems ....................................................................................................................................................................................................................... 30-3 Cowl Anti-Ice Systems ...................................................................................................................................................................................................................... 30-4 Cowl Pressure Differential Indication System .................................................................................................................................................................................. 30-6 Windshield Blower System ............................................................................................................................................................................................................... 30-6 Cabin Window Heat System ............................................................................................................................................................................................................. 30-7 INDICATING/RECORDING SYSTEM .............................................................................................................................................................................................. 31-1 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. Clocks (Cockpit) ............................................................................................................................................................................................................................... 31-1 Flight Data Recorder (FDR) Systems ................................................................................................................................................................................................ 31-1 Brake Temperature Monitoring System (BTMS) .............................................................................................................................................................................. 31-3 G Monitor System ............................................................................................................................................................................................................................. 31-3 Electronic Checklist ......................................................................................................................................................................................................................... 31-4 Data Acquisition Unit (DAU) Channels (GV) .................................................................................................................................................................................. 31-4 Security System ................................................................................................................................................................................................................................. 31-4 Engine Cowl Open Indicating System............................................................................................................................................................................................... 31-4 Airplane Personality Modules (APM) (GV-SP, GIV-X) .................................................................................................................................................................. 31-5 Plastic Guard Switch Covers ............................................................................................................................................................................................................. 31-5 Configuration Management Systems (GV-SP, GIV-X) .................................................................................................................................................................... 31-5 InfraRed Counter Measuring System (IRCM) or Directional InfraRed Counter Measuring System (DIRCM) ............................................................................... 31-5 Quick Access Recorder (QAR) ......................................................................................................................................................................................................... 31-6 XM Weather ...................................................................................................................................................................................................................................... 31-6 Modular Avionics Unit (MAU) Channels (GV-SP/GIV-X).............................................................................................................................................................. 31-6 Front Matter F-6 TABLE OF CONTENTS (CONTINUED) ATA 32 LANDING GEAR ................................................................................................................................................................................................................................... 32-1 1. 2. 3. 4. 5. 6. 7. 8. ATA 33 Anti-Skid System .............................................................................................................................................................................................................................. 32-1 Rudder Pedal Steering System .......................................................................................................................................................................................................... 32-1 Landing Gear Position Indicators ...................................................................................................................................................................................................... 32-2 Variable Gain Nose Wheel Steering.................................................................................................................................................................................................. 32-2 Nosewheel Steering Accessory Hardware (Torque Link Lanyards) ................................................................................................................................................. 32-2 Emergency Landing Gear Extension Bottle Pressure Gauge (Nose Wheelwell) .............................................................................................................................. 32-2 Emergency Landing Gear Extension Bottle Pressure Cockpit CAS Indication (Summary Page) ..................................................................................................... 32-2 Landing Gear Extension / Retraction System (includes dump valve, gear handle, and blow down bottle) (GIV-X) ....................................................................... 32-3 Landing Gear Extension / Retraction System (includes dump valve, gear handle, and blow down bottle) (GV/GV-SP) ................................................................ 32-4 LIGHTS................................................................................................................................................................................................................................................... 33-1 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. Cockpit/Flight Deck/Flight Compartment Instrument Lighting Systems (Excluding EFIS and EICAS) ......................................................................................... 33-1 Passenger Cabin Interior Illumination Systems ................................................................................................................................................................................. 33-1 Passenger Lighted Information Signs ................................................................................................................................................................................................ 33-2 Position Light Bulbs .......................................................................................................................................................................................................................... 33-3 Beacon Light ..................................................................................................................................................................................................................................... 33-4 Strobes (Anti-Collision Lights) ......................................................................................................................................................................................................... 33-4 Wing Inspection Lights ..................................................................................................................................................................................................................... 33-4 Landing Lights .................................................................................................................................................................................................................................. 33-5 Taxi Light System ............................................................................................................................................................................................................................. 33-5 Wing Tip Taxi Light Systems ........................................................................................................................................................................................................... 33-5 Floor Proximity Emergency Escape Path Marking System Lights ................................................................................................................................................... 33-6 Pulselight System (Identification Lights) .......................................................................................................................................................................................... 33-6 Recognition Light System ................................................................................................................................................................................................................. 33-6 Logo Light System ............................................................................................................................................................................................................................ 33-6 Ramp Lights Systems ........................................................................................................................................................................................................................ 33-7 Flashlight Charging Systems ............................................................................................................................................................................................................. 33-7 Aft Compartment Lights (Boiler Room) ........................................................................................................................................................................................... 33-7 Cargo Compartment Light ................................................................................................................................................................................................................. 33-7 Pylon Mounted Exterior Baggage Loading Light Systems ............................................................................................................................................................... 33-7 Front Matter F-7 TABLE OF CONTENTS (CONTINUED) ATA 33 LIGHTS (continued) ............................................................................................................................................................................................................................... 33-8 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. ATA 34 Wheel Well Lights ............................................................................................................................................................................................................................ 33-8 Exterior Emergency Evacuation Lighting System ............................................................................................................................................................................ 33-8 Service Door Lights .......................................................................................................................................................................................................................... 33-8 Dim and Test Enunciator Channels ................................................................................................................................................................................................... 33-8 Airstair Lights ................................................................................................................................................................................................................................... 33-9 Dome Light ....................................................................................................................................................................................................................................... 33-9 Baggage Compartment Light ............................................................................................................................................................................................................ 33-9 Cockpit Flashlight ............................................................................................................................................................................................................................. 33-9 Wing Tip Position Light LED Element Banks ................................................................................................................................................................................ 33-10 Tail Position Light LED Element Banks ......................................................................................................................................................................................... 33-10 NAVIGATION........................................................................................................................................................................................................................................ 34-1 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. Directional Compass Reference Sensors ........................................................................................................................................................................................... 34-1 Attitude Reference Sensors ............................................................................................................................................................................................................... 34-1 Standby Flight Displays .................................................................................................................................................................................................................... 34-1 Weather Radar Systems..................................................................................................................................................................................................................... 34-5 VOR/ILS Navigation Systems .......................................................................................................................................................................................................... 34-6 Marker Beacon Systems .................................................................................................................................................................................................................... 34-6 Automatic Direction Finding Systems .............................................................................................................................................................................................. 34-6 ATC Transponder and Automatic Altitude Reporting Systems ........................................................................................................................................................ 34-7 Distance Measuring Equipment (DME) Systems .............................................................................................................................................................................. 34-8 Standby RMI (Electro-Mechanical) (GV) ......................................................................................................................................................................................... 34-8 Radio Altimeter Systems ................................................................................................................................................................................................................... 34-9 Long Range Navigation Systems (IRS, GPS and GNSSU)............................................................................................................................................................... 34-9 Terrain Awareness and Warning System (TAWS) ......................................................................................................................................................................... 34-10 Lasertrak NDU (GV) ....................................................................................................................................................................................................................... 34-16 Flight Management Systems (CDU & Nav Computer Only) (GV only) ........................................................................................................................................ 34-17 Navigation Management System..................................................................................................................................................................................................... 34-18 Lightning Sensor Systems (LSS)..................................................................................................................................................................................................... 34-19 Stormscope ...................................................................................................................................................................................................................................... 34-19 Traffic Alert Collision and Avoidance System ............................................................................................................................................................................... 34-19 Microwave Landing Systems (MLS) .............................................................................................................................................................................................. 34-22 Symbol Generators (GV)................................................................................................................................................................................................................. 34-22 Guidance Panel Digital Indications and Mode Select Indications ................................................................................................................................................... 34-22 Front Matter F-8 TABLE OF CONTENTS (CONTINUED) ATA 34 NAVIGATION (continued) .................................................................................................................................................................................................................. 34-26 23. Altitude Alerting System ................................................................................................................................................................................................................. 34-26 24. Display Units ................................................................................................................................................................................................................................... 34-27 25. Standby Magnetic Compass System (Flux Valve) (GV) ................................................................................................................................................................. 34-29 Magnetometer (GV-SP, GIV-X) ..................................................................................................................................................................................................... 34-29 26. Non-Stabilized Magnetic Compass ................................................................................................................................................................................................. 34-30 27. Head Up Display System ................................................................................................................................................................................................................ 34-30 28. Airborne Flight Information System (AFIS) ................................................................................................................................................................................... 34-31 29. Slip-Skid Indicator .......................................................................................................................................................................................................................... 34-31 30. Data Loader (GV)............................................................................................................................................................................................................................ 34-32 Data Management Unit (DMU) (GV-SP, GIV-X) .......................................................................................................................................................................... 34-32 31. Air Data Computers/Systems .......................................................................................................................................................................................................... 34-32 32. Integrated Avionics Computers (IACs) (GV) ................................................................................................................................................................................. 34-33 33. Bus Controllers (GV) ...................................................................................................................................................................................................................... 34-34 34. Airshow Controller System ............................................................................................................................................................................................................. 34-34 35. Windshear Warning and Flight Guidance System (Reactive) ......................................................................................................................................................... 34-35 36. Windshear Detection and Avoidance System (Predictive) .............................................................................................................................................................. 34-35 37. Cockpit Video Monitors .................................................................................................................................................................................................................. 34-35 38. Heads Up Checklist ......................................................................................................................................................................................................................... 34-35 39. Enhanced Vision System (EVS) ...................................................................................................................................................................................................... 34-36 40. Terrain Server Function/EGPWM Modules (GV-SP, GIV-X) ....................................................................................................................................................... 34-36 41. Electronic Flight Bag ...................................................................................................................................................................................................................... 34-36 42. Advanced Graphics Modules (AGM) (GV-SP, GIV-X) ................................................................................................................................................................. 34-37 43. Cockpit Printer ................................................................................................................................................................................................................................ 34-38 44. Cursor Control Devices (GV-SP, GIV-X) ....................................................................................................................................................................................... 34-38 45. Multifunction Control Display Units (MCDU) (GV-SP, GIV-X) ................................................................................................................................................... 34-39 46. Advanced Graphics Module (AGM) Databases (GV-SP, GIV-X) .................................................................................................................................................. 34-41 47. Charts Function (GV-SP, GIV-X) ................................................................................................................................................................................................... 34-41 48. Video Function (GV-SP, GIV-X).................................................................................................................................................................................................... 34-41 49. Automatic Dependent Sueviellance-Broadcast (ADS-B) System ................................................................................................................................................... 34-42 50. Right Side Display Controller (GV) ................................................................................................................................................................................................ 34-43 Right Side Display Controller (GV-SP/GIV-X) .............................................................................................................................................................................. 34-44 51. Synthetic Vision Primary Flight Display (SV PFD) Functions ....................................................................................................................................................... 34-45 52. DDA (Digital to Distance Adapter) (GV only) ............................................................................................................................................................................... 34-45 53. GNSSU WASS (Wide Area Augmentation System or SBAS – Space Based Augmentation System) Function............................................................................ 34-45 54. CAS Scroll Switches ....................................................................................................................................................................................................................... 34-45 Front Matter F-9 TABLE OF CONTENTS (CONTINUED) ATA 35 OXYGEN ................................................................................................................................................................................................................................................ 35-1 1. Passenger Oxygen System and Supply.............................................................................................................................................................................................. 35-1 2. Cabin Oxygen ON Warning System ................................................................................................................................................................................................. 35-1 3. Oxygen Service Panel Pressure Gauges ............................................................................................................................................................................................ 35-3 4. Portable Oxygen Dispensing Units (Bottle and Mask)...................................................................................................................................................................... 35-3 5. Oxygen Supply Warning Systems ..................................................................................................................................................................................................... 35-3 6. Protective Breathing Equipment (PBE) ............................................................................................................................................................................................. 35-4 7. Electronic Equipment Rack Oxygen Pressure Gauges ...................................................................................................................................................................... 35-4 8. Cockpit Oxygen Pressure Indications ............................................................................................................................................................................................... 35-4 9. Therapeutic Oxygen .......................................................................................................................................................................................................................... 35-4 10. High Landing Field Elevation Passenger Oxygen Controller high Altitude Switch ......................................................................................................................... 35-5 ATA 36 PNEUMATIC ......................................................................................................................................................................................................................................... 36-1 1. 2. 3. 4. ATA 38 WATER/WASTE ................................................................................................................................................................................................................................... 38-1 1. 2. 3. 4. ATA 45 Bleed Air Systems ............................................................................................................................................................................................................................. 36-1 Bleed Air Hot Warning Systems ....................................................................................................................................................................................................... 36-4 Isolation Valve .................................................................................................................................................................................................................................. 36-6 Bleed Air System Switch Capsule Lights.......................................................................................................................................................................................... 36-6 Potable Water Systems ...................................................................................................................................................................................................................... 38-1 Lavatory Waste Systems (Including Wheelchair Accessible Lavatories) ......................................................................................................................................... 38-1 Lavatory Dump/Drain System ........................................................................................................................................................................................................... 38-2 Vacuum Toilet Holding Tank Indicator ............................................................................................................................................................................................ 38-2 CENTRAL MAINTENANCE COMPUTER ....................................................................................................................................................................................... 45-1 1. 2. Maintenance Data Acquisition Unit (MDAU) (GV) ......................................................................................................................................................................... 45-1 Central Maintenance Computer (CMC) (GV-SP, GIV-X) ................................................................................................................................................................ 45-1 Front Matter F - 10 TABLE OF CONTENTS (CONTINUED) ATA 46 NEW TECHNOLOGY .......................................................................................................................................................................................................................... 46-1 1. ATA 49 Electronic Flight Bag Systems (EFBs) .............................................................................................................................................................................................. 46-1 AIRBORNE AUXILIARY POWER..................................................................................................................................................................................................... 49-1 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. Auxiliary Power Unit (APU) ............................................................................................................................................................................................................. 49-1 APU EGT Indicators (EICAS and Overhead) ................................................................................................................................................................................... 49-1 APU Tachometers (EICAS and Overhead) ....................................................................................................................................................................................... 49-1 APU "READY" Light System........................................................................................................................................................................................................... 49-2 APU Remote Oil Quantity/Servicing System ................................................................................................................................................................................... 49-2 APU Oil Pressure Gauges ................................................................................................................................................................................................................. 49-2 APU Oil Temperature Gauges........................................................................................................................................................................................................... 49-2 APU Fuel Pressure Gauges ............................................................................................................................................................................................................... 49-2 APU Start Indicator Light ................................................................................................................................................................................................................. 49-2 APU Air Load Control Valve ............................................................................................................................................................................................................ 49-3 APU External Fire Warning Alarm (Fire Warning Bell) .................................................................................................................................................................. 49-3 APU Air Inlet Door System .............................................................................................................................................................................................................. 49-3 Bleed Air Augmentation Valve (GV, GV-SP) .................................................................................................................................................................................. 49-4 Surge Control Valve (GV, GV-SP) ................................................................................................................................................................................................... 49-4 Ignition System Channels (GV, GV-SP) ........................................................................................................................................................................................... 49-4 EGT Thermocouple System (GV, GV-SP) ....................................................................................................................................................................................... 49-4 Temperature Resistance Bulb (T2) .................................................................................................................................................................................................... 49-5 Inlet Pressure Transmitter (P2) (GV, GV-SP) ................................................................................................................................................................................... 49-5 RPM Speed Sensor Channels (GV, GV-SP) ..................................................................................................................................................................................... 49-5 APU Hour Meter ............................................................................................................................................................................................................................... 49-5 Oil Temperature (GV, GV-SP).......................................................................................................................................................................................................... 49-5 Deprime Solenoid (GV, GV-SP) ....................................................................................................................................................................................................... 49-6 Oil Heater (GV, GV-SP) ................................................................................................................................................................................................................... 49-6 APU Start/Engine Cowl Interrupt System ......................................................................................................................................................................................... 49-6 Front Matter F - 11 TABLE OF CONTENTS (CONTINUED) ATA 52 DOORS .................................................................................................................................................................................................................................................... 52-1 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. ATA 71 POWERPLANT ..................................................................................................................................................................................................................................... 71-1 1. ATA 73 EPA Tank Ejector Pump ................................................................................................................................................................................................................... 71-1 ENGINE FUEL & CONTROL ............................................................................................................................................................................................................. 73-1 1. 2. 3. ATA 74 Door Warning Light System ............................................................................................................................................................................................................. 52-1 Cargo Door Operating System .......................................................................................................................................................................................................... 52-1 Cargo Door Warning Light System ................................................................................................................................................................................................... 52-1 Door Seal Pressure Indicator ............................................................................................................................................................................................................. 52-2 Main Entry Door Normal Operating System ..................................................................................................................................................................................... 52-2 Main Entry Door Acoustic Curtain/Door System ............................................................................................................................................................................. 52-2 Lavatory Door ................................................................................................................................................................................................................................... 52-3 Baggage Door Warning System ........................................................................................................................................................................................................ 52-3 Main Entry Door Warning System .................................................................................................................................................................................................... 52-3 Internal Baggage Door Warning System (GV, GV-SP) .................................................................................................................................................................... 52-3 Internal Pocket Doors ........................................................................................................................................................................................................................ 52-4 Cabin Over Wing Exit Window Warning System ............................................................................................................................................................................. 52-4 Fuel Flow Indication Systems ........................................................................................................................................................................................................... 73-1 Fuel Low Pressure Warning Systems (EICAS) ................................................................................................................................................................................. 73-1 Engine FADEC Systems (GV, GV-SP) ............................................................................................................................................................................................ 73-2 Engine FADEC System (GIV-X) ...................................................................................................................................................................................................... 73-3 IGNITION ............................................................................................................................................................................................................................................... 74-1 1. 2. Ignition Systems ................................................................................................................................................................................................................................ 74-1 Ignition ON Indicator Systems .......................................................................................................................................................................................................... 74-2 Front Matter F - 12 TABLE OF CONTENTS (CONTINUED) ATA 77 ENGINE INDICATING ........................................................................................................................................................................................................................ 77-1 1. 2. 3. 4. 5. ATA 78 ENGINE EXHAUST .............................................................................................................................................................................................................................. 78-1 1. ATA 79 Thrust Reversers ................................................................................................................................................................................................................................ 78-1 ENGINE OIL .......................................................................................................................................................................................................................................... 79-1 1. 2. 3. 4. 5. ATA 80 HP Tachometer Indications EICAS ................................................................................................................................................................................................... 77-1 Engine Vibration Monitor Systems Sensors ...................................................................................................................................................................................... 77-1 Standby Engine Instruments Indicating System (RFMU) (GV) ........................................................................................................................................................ 77-2 Standby Engine Instruments on Multifunction Control Display (MCDU) (GV-SP, GIV-X) ........................................................................................................... 77-2 Engine Vibration Monitoring System ............................................................................................................................................................................................... 77-2 Low Oil Pressure Warning System ................................................................................................................................................................................................... 79-1 Engine Oil Replenishment System .................................................................................................................................................................................................... 79-1 Impending Oil Filter Bypass Indications ........................................................................................................................................................................................... 79-1 Oil Quantity Indication Systems (EICAS/Ground Service Control Panel) ....................................................................................................................................... 79-2 Oil Filter Pressure Switch Fault Indications ...................................................................................................................................................................................... 79-2 STARTING ............................................................................................................................................................................................................................................. 80-1 1. 2. 3. 4. Engine Starting Systems .................................................................................................................................................................................................................... 80-1 Auto Start System.............................................................................................................................................................................................................................. 80-1 Start Valve Position Indications ........................................................................................................................................................................................................ 80-2 Start Valve Position Indicator Lights ................................................................................................................................................................................................ 80-3 SECTION TWO – CREW ALERTING SYSTEM (CAS) MESSAGE RELIEF ................................................................................................................................................... 2-1 Statement Page ........................................................................................................................................................................................................................................... 2-2 CAS Messages ...........................................................................................................................................................................................................................2-3 thru 2-131 Front Matter F - 13 General Information Gulfstream has developed this manual to assist operators in development of their Maintenance, Operational, and Placarding Procedures (MOP) for the Gulfstream V aircraft as required by the Federal Aviation Administration (FAA) Advisory Circular 91-67 dated July 28, 1991. This manual is intended for use in conjunction with the Gulfstream V Master Minimum Equipment List (MMEL), Revision 8, dated November 7, 2014. Operators must apply to local FAA office for approval of a specific MEL and MOP for their aircraft. Part 91 operators should be aware that the published MMEL is intended for 14 CFR 121, 125, 129 and 135 operations as specified in the preamble. 14 CFR 91 operators must obtain a 14 CFR 91 Preamble from the local FAA office. This manual’s revision number will reflect the last issued FAA approved MMEL revision number. Updates to this manual prior to the next FAA approved MMEL revision will be identified by a point and a letter following the assigned FAA revision number, e.g., first update will be reflected as Revision 8a. The Aircraft Discrepancy Log Sheet where all inoperative items will be noted is referred to as ADLS throughout this document. Those items marked with three asterisks (***) are optional items. Those items which are not production installed items will require the operator to develop specific maintenance, operational and placarding procedures for their installation. The following was accomplished by the Original GV Maintenance, Operational, and Placarding Manual. Users should review and become familiar with the manual. 1. 2. 3. 4. Formatted manual in a table format similar to MMEL. Electronically formatted in Microsoft Word for Windows 2.0 Corrected technical errors throughout the manual. Corrected typographical errors throughout the manual. Note: If errors are noted in this manual, submit a fax providing details and suggested corrections for the error to Gulfstream Technical Publications at (912) 965-3520. Note: If assistance is needed regarding the MMEL, MEL or MOP implementation or usage, contact the local FAA office. Front Matter F - 14 NOTICE NOTICE NOTICE Any time an item in the MMEL calls for an (M) procedure to be accomplished prior to dispatch with the listed item inoperative, the definitions at the beginning of the MMEL states that these procedures are normally accomplished by maintenance personnel. However, other personnel may be qualified and authorized to perform certain functions. The ultimate responsibility for the accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the operator. In short, a properly trained flight crew member may perform an (M) procedure such as but not limited to pulling and collaring circuit breakers, changing light bulbs, changing or moving Display Units, making adjustments to seats, verifying proper operation of systems or components, swapping connectors from an inoperative unit to an operative unit, and/or closing/locking of doors if that crew member has been trained to do so. It is recommended that training records be kept at the home base of operations for personnel that have been trained to perform (M) procedures. The applicable paragraph from the MMEL is below. 15."(M)" symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior to operation with the listed item inoperative. Normally these procedures are accomplished by maintenance personnel; however, other personnel may be qualified and authorized to perform certain functions. Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment should be accomplished by maintenance personnel. The satisfactory accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as part of the operator's manual or MEL. The FAA recently revised 14 CFR to address Extended Operations (ETOPS) of Multi-Engine Airplanes. The new rule applies to GAC airplanes operated under 14 CFR Part 135 on stage lengths where the single engine cruise segment exceeds 180 minutes. On those flights, the MMEL becomes more restrictive for certain items. Those items have been identified in this MMEL revision by the words, "Except for ER operations, . . .”. Front Matter F - 15 Revision Dates for Gulfstream Aerospace Model G-V, GV-SP (G550, G500), GIV-X (G450, G350) FAA MOPP: (For an explanation of changes, refer to the Gulfstream Aerospace Model G-V, GV-SP (G550, G500), GIV-X (G450, G350) FAA MMEL Highlights of Change page.) Material Dated: August 19, 1996 August 19, 1998 June 4, 2001 November 9, 2001 August 11, 2003 December 2, 2003 December 14, 2004 June 2, 2006 July 5, 2006 June, 2007 July 24, 2007 February 4, 2010 November 8, 2010 May 17, 2013 November 7, 2014 Reflects Update Type: Original Revision Revision Revision Revision Revision Revision Revision Revision Revision Revision Revision Revision Revision Revision Number: 0 1 2 2a 3 3a 4 4a 4b 5 6 7 7a 7b 8 Front Matter F - 16 THIS PAGE INTENTIONALLY LEFT BLANK Front Matter F - 17 GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MOP REV. NO.: 8 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MOP DATE: 11/07/2014 MINIMUM NAVIGATIONAL EQUIPMENT POSITION SENSORS MINIMUM NAVIGATIONAL EQUIPMENT FMS Enroute Terminal Approach FMS Modes MNPS AC 91-70x AC 120-33 RNP (General) AC 90-105 RNP 10 FAA Order 8400.12x RNAV and RNP Operations Approaches With Required Position Sensors B-RNAV EASA AMC 20-4 AC 90-96A RNP 4 FAA Order 8400.33x RNP 2 AC 90-105 RNAV 2 AC 90-100A RNP 1 AC 90-105 RNAV 1 AC 90-100A P-RNAV AC 90-96A/JAA TGL-10 RNAV-WAAS LPV AC 90-107 RNAV-BARO AC 90-105 RNP AR AC 90-101 NOTE GPS DME/DME VOR/DME IRS 1 1 1 1 1 A, B 1 1 1 1 1 A, B 1 1 1 1 A, B, F A, B, C 2 2 2 1 1 1 1 1 2 1 1 1 1 1 1 1 1 2 2 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 2 A, B A, B, C, D A A, C A, B, D 1 A, B, E A, B 1 A, B, E A, B, F A A A Front Matter F - 18 GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MOP REV. NO.: 8 MOP DATE: 11/07/2014 MINIMUM NAVIGATIONAL EQUIPMENT NOTES: A. When more than one position sensor is available, the FMS will select the one with the lowest EPU. B. The FMS may use any one of the indicated position sensors. 1) Aircraft may be flown on routes requiring two Long Range Navigation (LRN) systems provided that two FMS’s, two GPS position sensors or two Inertial Reference System (IRS) position sensors are operational or one GPS and one IRS sensor are operational. 2) Aircraft may be flown on routes requiring one LRN system provided that one FMS, one GPS sensor, or one IRS position sensor is operational. C. Limited to 5.0 hours of IRS-only navigation after the last GPS, DME/DME, or VOR/DME update. D. When DME/DME position sensor is used, one IRS position sensor must be available to bridge gaps in DME infrastructure. This is referred to on charts as DME/DME/IRU. E. P-RNAV does not require IRS support for the DME/DME position sensor. F. VOR, VOR/DME, TACAN or VOR/DME RNAV approaches. Front Matter F - 19 GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MOP REV. NO.: 8 MOP DATE: 11/07/2014 EN ROUTE NAVIGATION REQUIREMENTS RVSM Operations are authorized: The following equipment must be operative: 2 Air Data Systems (must be two of the following: 1, 2, 3) 1 ATC Transponder with both altitude reporting systems operative on remaining transponder 1 Flight Guidance Computer with operable autopilot “altitude hold” function 1 Altitude Alerting System Traffic Alert and Collision Avoidance System (TCAS II) NAT MNPS Operations are authorized: To meet navigation accuracy requirements, two independent long range navigational systems must be operative. B-RNAV (RNAV 5 or RNP5) Operations are authorized: While at least one FMS is operating, and while at least one of the following pieces of equipment is operating: GPS / VOR and DME / IRS Aircraft may be dispatched in B-RNAV area provided the following is complied with: For IRS only, B-RNAV capability is provided for up to 2 hours without FMS sensor updating. One VOR/DME must be available as a NAV source (possibility to revert to conventional navigation means in case loss of last B-RNAV system). RNP10 Operations are authorized: Aircraft may be dispatched in RNP10 area provided: At least two Flight Management Systems are operative and at least two GPS are operative, or At least two IRS are operative. For IRS only, RNP10 capability is provided for up to 5.0 hours in duration without FMS sensor updating. P-RNAV (RNAV 1 or RNAV 2) Operations are authorized: At least two Flight Management Systems are operative and either of the following navigation modes such that EPU does not exceed RNP requirements: HYBRID GPS DME / DME VOR / DME Front Matter F - 20 GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MOP REV. NO.: 8 MOP DATE: 11/07/2014 FUTURE AIR NAVIGATION SYSTEM (FANS) REQUIREMENTS FANS 1/A Operations are authorized The following equipment must be operative: 2 MCDU's SATCOM for overwater or remote area flights 1 VHF Datalink radio for overland flights 1 CMF (Communications Management Function or Datalink Function) 1 HF radio for overwater or remote area flights Front Matter F - 21 GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL PAGE NUMBER: 1-1 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 SECTION ONE LINE REPLACEABLE UNIT (LRU) COMPONENT RELIEF GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING 1. Cabin Altitude Indicator (Overhead Panel) PAGE NUMBER: 21-1 MMEL REV. NO.: 8 C 1 0 May be inoperative provided cabin altitude is available on EICAS Synoptic display. None required. None required. An Inoperative Placard will be placed adjacent to Cabin Altitude Indicator and will be noted on ADLS. C 1 0 May be inoperative provided: a) Cabin Pressure Selector Panel is operative, and b) Pressurization is operated in AUTO mode. None required. None required. An Inoperative Placard will be placed adjacent to Cabin Altitude Indicator and will be noted on ADLS. C 1 0 May be inoperative provided: a) Cabin Differential Pressure Indicator is operative, and b) A chart is provided to crew to convert Cabin Differential Pressure to Cabin Altitude. NOTE: See chart on page 21-3. None required. None required. An Inoperative Placard will be placed adjacent to Cabin Altitude Indicator and will be noted on ADLS. D 1 0 May be inoperative provided airplane is equipped with additional pneumatic threein-one cabin pressurization monitoring instrument, and Cabin Altitude Indicator portion is fully operative. None required. None required. An Inoperative Placard will be placed adjacent to Cabin Altitude Indicator and will be noted on ADLS. C 1 0 (O) May be inoperative provided airplane is operated in unpressurized configuration. None required. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard will be placed adjacent to Cabin Altitude Indicator and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING Cabin Differential Pressure Indicator MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 2. PAGE NUMBER: 21-2 MMEL REV. NO.: 8 D 1 0 May be inoperative provided cabin differential pressure is available on EICAS Synoptic display. None required. None required. An Inoperative Placard will be placed adjacent to Cabin Differential Pressure Indicator and will be noted on ADLS. C 1 0 May be inoperative provided: a) Cabin Pressure Selector Panel is operative, and b) Pressurization is operated in AUTO mode. None required. None required. An Inoperative Placard will be placed adjacent to Cabin Differential Pressure Indicator and will be noted on ADLS. D 1 0 May be inoperative provided: a) Cabin Altitude Indicator is operative, and b) A chart is provided to crew to convert Cabin Altitude to Cabin Differential Pressure. NOTE: See sample chart on page 21-3. None required. None required. An Inoperative Placard will be placed adjacent to Cabin Differential Pressure Indicator and will be noted on ADLS. D 1 0 May be inoperative provided airplane is equipped with additional pneumatic threein-one cabin pressurization monitoring instrument, and Cabin Altitude Indicator portion is fully operative. None required. None required. An Inoperative Placard will be placed adjacent to Cabin Differential Pressure Indicator and will be noted on ADLS. C 1 0 (O) May be inoperative provided airplane None required. is operated in unpressurized configuration. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard will be placed adjacent to Cabin Differential Pressure Indicator and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. SYSTEM & SEQUENCE NUMBERS 21. AIR CONDITIONING PAGE NUMBER: 21-3 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS Determine Delta P: Input Aircraft Alt (ft) psia 51000 Cabin Alt (ft) 8000 Output 1.603 Delta P (psia) 9.313 10.916 Determine Cabin Altitude: Input Aircraft Alt (ft) 51000 Delta P (psia) 10.694 psia Output 1.603 Cabin Alt (ft) 4848.8 Determine Aircraft Altitude: Input Cabin Alt (ft) 4848.8 Delta P (psia) 10.694 psia 12.297 Aircraft Alt (ft) Output 50997.7 PROCEDURE GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING 3. Cabin Rate of Climb Indicator D 1 0 4. Automatic Pressurization Control Systems B 2 0 (continued) PAGE NUMBER: 21-4 MMEL REV. NO.: 8 (O) Except for ER operations, may be inoperative provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, and e) Airplane is operated in accordance with AFM Limitations. None required. None required. An Inoperative Placard will be placed adjacent to Cabin Rate of Climb Indicator and will be noted on ADLS. None required. Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. AFM, Section 2, Normal Procedures, Before Starting Engines. Flight crew will operate airplane in accordance with AFM, Section 1, Limitations, Cabin Pressurization Control and Section 3, Abnormal Procedures, Loss of Automatic Pressurization Control. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard stating “AUTO INOP” will be placed above FAULT / MANUAL Switch and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 21-5 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING 4. Automatic Pressurization Control Systems (continued) B 2 0 (O) Except for ER operations, may be inoperative provided airplane is operated in unpressurized configuration. None required To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard stating "AUTO INOP" will be placed above FAULT/ MANUAL Switch and will be noted on ADLS. 5. Manual Pressurization Control System C 1 0 May be inoperative provided both Automatic Pressurization Control Systems are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 6. Semi-Auto Pressurization Control System C 1 0 None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 8. Pressurization Outflow Valve Position Indicator MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING Cabin Altitude Pressure Warning System MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 7. PAGE NUMBER: 21-6 MMEL REV. NO.: 8 C 1 0 May be inoperative provided: a) Cabin Altitude and Differential Pressure Indicators are operative, b) Cabin Oxygen On Warning System is operative, and c) Airplane is operated in accordance with AFM Limitations. C 1 0 C 1 0 None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by the flight crew and will be noted on ADLS. (O) May be inoperative provided airplane None required. is operated in unpressurized configuration. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard will be placed in a prominent position to be seen by the flight crew and will be noted on ADLS. May be inoperative provided all other components of the Cabin Pressure Control Panel and Cabin Pressure Indicator are operative. None required. An Inoperative Placard will be placed on Outflow Valve Position Indicator and will be noted on ADLS. None required. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING Cockpit Zone Temperature Control System & Cabin Zone Temperature Control Systems MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 9. PAGE NUMBER: 21-7 MMEL REV. NO.: 8 C 3 2 C 3 1 (O) May be inoperative provided: a) Ram Air system is operative, and b) Airplane is operated in unpressurized configuration. None required. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard will be placed adjacent to Cockpit/Cabin Temperature Indicator and will be noted on ADLS. 1) Automatic System C 3 0 May be inoperative provided: a) Associated manual control system is operative, and b) Associated temperature indicator is operative. None required. None required. An Inoperative Placard will be placed on AUTO half of capsule of Cockpit/Cabin Temperature Selectors and will be noted on ADLS. 2) Manual Systems C 3 0 May be inoperative provided: a) Associated automatic control system is operative, and b) Associated temperature indicator is operative. None required. None required. An Inoperative Placard will be placed on MANUAL half of capsule of Cockpit/Cabin Temperature Selectors and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 11. Duct Temperature Indicators (Overhead Panel) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING Cockpit/Cabin Zone Temperature Indicators (Overhead Panel) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 10. PAGE NUMBER: 21-8 MMEL REV. NO.: 8 D 3 0 May be inoperative provided associated Automatic Temperature Control System is operative. None required. None required. An Inoperative Placard will be placed on affected Temperature Indicator face and will be noted on ADLS. D 3 0 May be inoperative provided associated zone temperature is available on EICAS Synoptic display. None required. None required. An Inoperative Placard will be placed on affected Temperature Indicator face and will be noted on ADLS. D 3 0 May be inoperative provided associated Manual Temperature Control System is operative. None required. None required. An Inoperative Placard will be placed on affected Temperature Indicator face and will be noted on ADLS. D 3 0 None required. None required. An Inoperative Placard will be placed on overhead panel below the Zone/Duct Switch and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING 12. PAGE NUMBER: 21-9 MMEL REV. NO.: 8 Environmental Control System (ECS) Packs 1) Pressurized Configuration C 2 1 Except for ER operations, may be inoperative provided: a) Inoperative ECS Pack is selected OFF, b) Bleed Air Isolation Valve is CLOSED and OPERATIVE, c) Right Main TRU is operative, d) Airplane is operated at or below FL410, and e) Authothrottle must be operative and engaged at or above FL400. None required. None required. An Inoperative Placard will be placed adjacent to affected "ECS PACK" Switch and will be noted on ADLS. 2) Unpressurized Configuration C 2 0 Except for ER operations, may be inoperative provided outflow valve is operative. None required. None required. An Inoperative Placard will be placed adjacent to affected "ECS PACK" Switches and will be noted on ADLS. C 1 0 May be inoperative provided primary Cabin Altitude and primary Cabin Differential Pressure Indicators are operative either in the overhead panel or on the Synoptic Display. None required. None required. An Inoperative Placard will be placed on Three-In-One Cabin Pneumatic Pressurization Monitoring Instrument face and will be noted on ADLS. 13. Three-In-One Cabin *** Pneumatic Pressurization Monitoring Instrument GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 21-10 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING 14. Air Conditioning System Pack Inlet Valves C 2 1 (M) Except for ER operations, may be inoperative provided: a) Affected Valve is CLOSED and deactivated electrically, b) Associated Air Conditioning Pack is selected OFF, and c) Airplane is operated in accordance with AFM Limitations. Maintenance will ensure affected Valve is "CLOSED" and electrically deactivated when associated Air Conditioning Pack switch is selected "OFF". Associated Air Conditioning CB must NOT be pulled. Refer to AMM, Chapter 21-21-00. Flight crew may perform maintenance function if maintenance is unavailable. Flight crew may accomplish this task if properly qualified and authorized. CAUTION: Pulling (de-energizing) associated Air Conditioning CB will cause valve to open, allowing airflow to restart. None required. An Inoperative Placard will be placed on or below affected ECS Pack Switch and will be noted on ADLS. 15. Outflow Valve System C 1 0 (M) (O) May be inoperative provided: a) Outflow valve is positioned to full OPEN position and electrically isolated, b) Airplane is operated in unpressurized configuration, and c) Extended overwater operations are not conducted. Maintenance will ensure Outflow Valve is positioned to full OPEN position and electrically de-energized by pulling the Cab Press Man Cont breaker LEER E-8. To operate the airplane unpressurized, refer to AFM Section 3-21-90. Also refer to AFM Section 4-22-30 in the event that smoke is detected oin the baggage compartment. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. May be inoperative provided: a) DC motor is operative, and b) Airplane is operated in accordance with AFM Limitations. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 1) AC Motors C 2 1 Flight crew may accomplish this task if properly qualified and authorized. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING Pressure Relief Valve MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 16. PAGE NUMBER: 21-11 MMEL REV. NO.: 8 C 1 0 (O) May be inoperative provided: a) Cabin differential pressure and cabin altitude displays are operative, b) Selected cabin altitude is 1,000 feet higher than normal cabin altitude for the cruise flight level, and c) Flight crew monitors actual cabin differential pressure and maintains it at or below 9.5 psi. None required. Flight Crew will ensure: a) Cabin Differential Pressure and Cabin Altitude Displays are operative. b) Select Semi-Auto Operation and selected Cabin Altitude is 1,000 feet higher than normal Cabin Altitude for cruise flight level. c) Monitor actual Cabin Differential Pressure and maintain it at or below 9.5 psi. An Inoperative Placard will be placed on Cabin Pressure Control Panel and will be noted on ADLS. C 1 0 (O) May be inoperative provided airplane is operated in unpressurized configuration. None required. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard will be placed on Cabin Pressure Control Panel and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING 17. PAGE NUMBER: 21-12 MMEL REV. NO.: 8 Cabin Pressure Indicator and Control Panel C 1 0 None required. None required. An Inoperative Placard will be placed on Control Panel and will be noted on ADLS. 1) Manual Light C 1 0 None required. None required. An Inoperative Placard will be placed on Control Panel and will be noted on ADLS. 2) Control Knob Deleted in Revision 7. 3) Flight/Landing Switch C (Light Function Only) 1 0 None required. None required. An Inoperative Placard will be placed on Control Panel and will be noted on ADLS. 4) Fault/Manual Switch (Light Function Only) C 1 0 None required. None required. An Inoperative Placard will be placed on Control Panel and will be noted on ADLS. 5) Auto/Semi Switch (Light Function Only) C 1 0 None required. None required. An Inoperative Placard will be placed on Control Panel and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 21-13 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING 18. Selector Panel (Semi-Auto) B 1 0 19. Remote Filter (Pressure Relief Valve PRV) B 1 0 20. CPAM (Cabin Pressure Acquisition Module) C 1 0 May be inoperative provided: a) Auto system (Cabin Pressure Control Panel) is operative, and, b) Semi-auto mode is considered inoperative. May be inoperative provided both auto systems are operative. None required. None required. An Inoperative Placard will be placed on Selector Panel and will be noted on ADLS. None required. None required. A Placard indicating filter is removed will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING 21. PAGE NUMBER: 21-14 MMEL REV. NO.: 8 Ram Air System 1) Pressurized Configuration C 1 0 May be inoperative provided: None required. a) Automatic Pressurization Control System is operative, b) Manual Pressurization Control System is operative, c) Bleed Air Pressure Regulating and Shut-Off Systems are operative, and d) Airplane is operated in accordance with AFM Limitations and Procedures. None required. An Inoperative Placard will be placed adjacent to the Ram Air Switch to be viewed by the flight crew and will be noted on the ADLS 2) Unpressurized Configuration C 1 0 (O) May be inoperative provided: a) Aircraft is operated in unpressurized configuration, and b) Airplane is operated in accordance with AFM Limitations and Procedures. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard will be placed adjacent to the Ram Air Switch to be viewed by the flight crew and will be noted on the ADLS. None required. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 21. AIR CONDITIONING PSU Fan MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 22. PAGE NUMBER: 21-15 MMEL REV. NO.: 8 C 1 0 (O) May be inoperative provided: a) Ambient Temperature is 95 degrees F (35 degrees C) or cooler, b) TRU electrical loads are 50% or less, c) Right main TRU is operative, and d) Both Environmental Control System (ECS) Packs are operative. None required. Flight crew will: a) Minimize ground operation time, especially during hot weather. b) During Ground operation, monitor TRU load – limit load to 50%. c) For ground operation longer than 15 minutes ensure main and baggage doors are closed, APU air is selected “ON” and outflow valve is fully OPEN. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 22. AUTO FLIGHT 1. Autothrottle Systems C 2 0 2. Performance Management Systems (SmartPerf/TOLD) (GV) C 2 0 (GV-SP / GIV-X) C 2 Control Wheel Autopilot Disconnect Buttons C 2 3. PAGE NUMBER: 22-1 MMEL REV. NO.: 8 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. May be inoperative provided Quick Reference Handbook is immediately available to the flight crew. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 0 May be inoperative provided Performance Handbook is immediately available to the flight crew. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 1 May be inoperative provided: a) Autopilot is not utilized below 1,500 feet AGL, b) Approach minimums do not require the use of the autopilot, and c) Airplane is piloted from the side with operative button. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 5. 6. Autothrottle Engage / Disengage Switches (on Thrust Lever Stem) Touch Control Steering Switches (TCS) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 22. AUTO FLIGHT Autothrottle Disconnect Buttons (on Thrust Lever Handles) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 4. PAGE NUMBER: 22-2 MMEL REV. NO.: 8 C 2 1 C 2 0 C 2 1 C 2 0 D 2 0 May be inoperative provided Autothrottle is not used. May be inoperative provided Autothrottle is not used. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on Thrust Lever Stem and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on Thrust Lever Stem and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on Thrust Lever Stem and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 22. AUTO FLIGHT Autopilots (Flight Guidance Computers (FGC) / Flight Directors) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 7. PAGE NUMBER: 22-3 MMEL REV. NO.: 8 C 2 1 (M) (O) Except for ER operations or where en route operations or approach minimums require its use, may be inoperative provided airplane is operated in accordance with AFM Limitations in the event operative FGC fails and Yaw Damper is inoperative. Maintenance will pull and reset the affected IAC (GV) or MAU Channel (GV-SP/GIV-X) and Guidance Panel circuit breakers in attempt to reset the AP/FGC. If AP/FGC does not recover, no further action required. Flight crew will observe AFM limitations in the event the operative AP/FGC fails and the Yaw Damper is inoperative. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. Flight crew will ensure airplane is operated in accordance with AFM Limitations in the event the operative Yaw Damper fails. AN Inoperative Placard will be displayed in a prominent position to be viewed by the flight crew and will be noted on the ADLS. NOTE: AP/FGC is required for MNPS, RVSM, RNP and PRNAV operations. 8. Yaw Damper Systems C 2 1 (O) Except for ER operations, may be inoperative provided airplane is operated in accordance with AFM Limitations. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 22. AUTO FLIGHT Takeoff/Go-Around (TO/GA) Buttons (on Power Lever Handles) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 9. PAGE NUMBER: 22-4 MMEL REV. NO.: 8 C 2 1 May be inoperative provided approach minimums do not require its use. C 2 0 (O) May be inoperative provided: None required. a) Both power levers are operated manually for takeoff and go-around, and b) Autopilot and Flight Director are not used below 500 feet or MDA, whichever is higher. NOTE: Flight Director Takeoff and GoAround guidance and Autothrottles are not available with both TO/GA switches inoperative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be viewed by the flight crew and will be noted on ADLS. Flight Director and Autothrottle are not available for Takeoff or Go-Around with both TO/GA buttons inoperative. Flight crew shall use raw data and manual throttles for takeoff and goaround. For takeoff, once airborne and above 500 ft AGL, pilot-not-flying (PNF) shall select desired lateral mode (HDG or LNAV) on guidance panel as directed by pilot-flying (PF). Additionally, PNF shall select desired vertical mode (FLCH or VS or FPA) and engage autothrottle as directed by PF. For go-around, after flaps and landing gear have been retracted and airplane is above 500 ft AGL, PNF shall select desired lateral mode (HDG or LNAV) and vertical mode (FLCH or VS or FPA) on guidance panel and engage autothrottle at direction of PF. An Inoperative Placard will be displayed in a prominent position to be viewed by the flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 22. AUTO FLIGHT Mach Trim Systems (GV-SP/GIV-X only) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 10. PAGE NUMBER: 22-5 MMEL REV. NO.: 8 C 2 1 None required. None required. An Inoperative Placard will be displayed in a prominent position to be viewed by the flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS Communications Systems (VHF, UHF) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 23-1 MMEL REV. NO.: 8 D D- 0 Any in excess of those required by 14 CFR may be inoperative provided it is not powered by the Emergency AC Bus, Emergency DC Bus, Battery Bus, Battery Direct Bus, or the DC Transfer Bus and not required for emergency procedures. None required. None required. NOTE: No. 1 VHF COMM must be operative – powered by the emergency bus. An Inoperative Placard will be placed adjacent to affected Radio Frequency Management Unit (GV) or MCDU (GVSP/GIV-X) and will be noted on ADLS. NOTE: Comm 1, NAV 1 and ATC 1 are powered by the Emergency Bus. 1) VHF Communication Control Panels *** a) Frequency Transer Light C - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** b) Frequency Transfer Switch C C- 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** c) Frequency Selector Knob C C- 2 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** d) Frequency Indication C C- 2 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS Cockpit Voice Recorder (CVR) (with Flight Data Recorder (FDR) Installed) A A1 0 *** 1) Independent Power Source C C1 0 Cockpit Voice Recorder (CVR) (without Flight Data Recorder (FDR) Installed) A A1 0 *** 1) Independent Power Source C C1 0 Cockpit Voice Recorder (CVR) (Operator Other Than a Holder of An Air Carrier or Commercial Operator Certificate) A A1 0 *** 1) Independent Power Source MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 2. PAGE NUMBER: 23-2 MMEL REV. NO.: 8 May be inoperative provided: a) Flight Data Recorder (FDR) is operative, and b) Repairs are made within three flight days. NOTE: Part 91 operators should refer to 14 CFR 91.609 for additional relief. May be inoperative provided repairs are made within three flight days. NOTE: Part 91 operators should refer to 14 CFR 91.609 for additional relief May be inoperative provided repairs are made in accordance with applicable 14 CFRs. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Part 91 operators should refer to 14 CFR 91.609 for additional relief C C 1 0 GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. Channels MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 1) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 3. Selective Call *** System (SELCAL) PAGE NUMBER: 23-3 MMEL REV. NO.: 8 C - 0 (O) May be inoperative provided alternate procedures are established and used. None required. One crew member shall monitor the appropriate frequency. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - 0 May be inoperative provided procedures do not require its use. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C - 0 (O) May be inoperative provided alternate procedures are established and used. None required. Flight crew will ensure: a) SELCAL decoder monitors audio from the VHF and HF communications transceivers, b) Recognizes receipt of the tone set assigned to the airplane, and c) Provides the flight compartment with call alert signals. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - 0 May be inoperative provided procedures do not require its use. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 4. PAGE NUMBER: 23-4 MMEL REV. NO.: 8 Emergency Locator Transmitters (ELT) *** 1) Survival Type ELTs D - - Any in excess of those required by 14 CFR may be inoperative or missing. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** 2) Fixed ELTs A - 0 (M) May be inoperative provided: a) System is deactivated, and b) Repairs are made within 90 days. Maintenance will pull and collar the ELT circuit breaker. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. A - 0 May be missing provided repairs are made None required. within 90 days. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - - (M) Any in excess of those required by 14 CFR may be inoperative provided system is deactivated. Maintenance will pull and collar the ELT circuit breaker. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - - Any in excess of those required by 14 CFR may be missing. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 5. Crewmember *** Interphone System PAGE NUMBER: 23-5 MMEL REV. NO.: 8 C 2 1 B - - None required. None required. An Inoperative Placard will be placed on Interphone System and will be noted on ADLS. None required. Flight crew may use the PA to communicate with the cabin crew or speak to the cabin crew directly in either the cockpit or cabin to pass information. An Inoperative Placard will be placed on Interphone System and will be noted on ADLS. 1) Passenger Configuration a) Flight Deck to Cabin, Cabin to Flight Deck Functions (O) May be inoperative provided: a) Flight deck to cabin and cabin to flight deck interphone functions operate normally on at least 50% of the cabin handsets, b) On wide-body airplanes, flight deck to cabin and cabin to flight deck interphone function operates normally at one door for each pair of exit doors, and c) Alternate communications procedures between the affected flight attendants station(s) are established and used. NOTE: Any station function(s) that is operative may be used. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 23-6 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 5. Crewmember *** Interphone System (cont’d) 1) Passenger Configuration b) Cabin to Cabin Functions B 2 0 (O) May be inoperative provided alternate communications procedures between the affected Flight Attendants station(s) are established and used. None required. Cabin crew may use the PA to communicate with the cabin crew or speak to the cabin crew directly in either the cockpit or cabin to pass information. An Inoperative Placard will be placed on Interphone System and will be noted on ADLS. None required. Flight crew may use the PA to communicate with the cabin crew or speak to the cabin crew directly in either the cockpit or cabin to pass information. An Inoperative Placard will be placed on Interphone System and will be noted on ADLS. NOTE: Any station function(s) that is operative may be used. B - - (O) May be inoperative provided: a) Cabin to cabin interphone functions operate normally on at least fifty percent of the cabin handsets, b) On wide-body airplanes, cabin to cabin interphone function operates normally at one door for each pair of exit doors, and c) Alternate communications procedures between the affected flight attendants stations are established and used. NOTE: Any station function(s) that is operative may be used. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 23-7 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 5. Crewmember *** Interphone System (cont’d) 1) Passenger Configuration c) Flight Deck to Ground 1) Large Turbojet Powered Airplanes Operating under Part 121 (continued) C 1 0 (O) Flight interphone flight deck to None required. ground/ground to flight deck function may be inoperative provided: a) Alternate procedures are established and used, and b) Nose gear/forward fuselage service interphone jack operates normally. Flight crew may use hand An Inoperative Placard will signals for communications with be placed on Interphone ground crew. System and will be noted on ADLS. C 1 0 (O) Service interphone flight deck to None required. ground/ground to flight deck function may be inoperative provided: a) Alternate procedures are established and used, and b) Nose gear/forward fuselage service interphone jack operates normally. Flight crew may use hand An Inoperative Placard will signals for communications with be placed on Interphone ground crew. System and will be noted on ADLS. B - 0 (O) May be inoperative provided alternate procedures are established and used. Flight crew may use hand An Inoperative Placard will signals for communications with be placed on Interphone ground crew. System and will be noted on ADLS. None required. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 23-8 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 5. Crewmember *** Interphone System (cont’d) 1) Passenger Configuration c) Flight Deck to Ground (cont’d) 2) All other Aircraft / Operations C - 0 (O) May be inoperative provided alternate procedures are established and used. None required. Flight crew may use hand An Inoperative Placard will signals for communications with be placed on Interphone ground crew. System and will be noted on ADLS. D - 0 May be inoperative provided procedures do not require its use. None required. None required. An Inoperative Placard will be placed on Interphone System and will be noted on ADLS. 6. Interphone Systems *** D - 0 None required. None required. An Inoperative Placard will be placed on Flitephone System and will be noted on ADLS. 7. C 2 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Cockpit Speakers May be inoperative provided: a) Affected speaker is not required for aural warnings, and b) An operative headset is provided for each person on cockpit duty. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 23-9 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 8. Passenger Address *** Systems (PA) 1) Passenger Configuration B 1 0 (O) May be inoperative provided: a) Alternate, normal, and emergency procedures, and/or operating restrictions are established and used, and b) Flight attendant alerting system (audio and visual) operates normally. None required. Flight crew will coordinate with cabin crew prior to the flight. Flight crews may use the flight deck-to-cabin interphone system to pass information to the cabin crew. Also, the flight crew may speak to the cabin crew directly in either the cockpit or cabin to pass information. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. Flight crew will coordinate with cabin crew prior to the flight. Flight crews may use the flight deck-to-cabin interphone system to pass information to the cabin crew. Also, the flight crew may speak to the cabin crew directly in either the cockpit or cabin to pass information. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. Flight crew will ensure alternate procedures are established and used. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Any station function(s) that is operative may be used. C 1 0 (O) May be inoperative provided: a) PA not required by 14 CFR, and b) Alternate, normal and emergency procedures, and/or operating restrictions are established and used. NOTE: Any station function(s) that is operative may be used. a) Lavatory Speakers (continued) C - - (O) May be inoperative provided alternate procedures are established and used. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 23-10 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 8. Passenger Address *** Systems (PA) (cont’d) 2) Cargo Only Configuration (Courier / Supernumerary Address System) a) Lavatory Speakers C 1 0 (O) May be inoperative provided alternate, normal and emergency procedures are established and used. None required. Flight crew will coordinate with cabin crew prior to the flight. Flight crews may use the flight deck-to-cabin interphone system to pass information to the cabin crew. Also, the flight crew may speak to the cabin crew directly in either the cockpit or cabin to pass information. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 May be inoperative provided procedures do not require its use. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 1 0 (O) May be inoperative provided alternate procedures are established and used. None required. Flight crew will ensure alternate procedures are established and used. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 May be inoperative provided procedures do not require its use. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 9. Satellite *** Communication Systems PAGE NUMBER: 23-11 MMEL REV. NO.: 8 D - 0 May be inoperative provided procedures do not require their use. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 10. Prerecorded *** Passenger Announcement Systems D - 0 (O) May be inoperative provided alternate procedures are established and used. None required. Flight crew will comply with proviso in remarks column by using manual PA system to inform passengers. In addition, the flight crew or cabin crew may give direct oral instructions to the passengers. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 11. C - 0 May be inoperative provided associated boom microphone operates normally. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - 0 Any in excess of those required by regulation may be inoperative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Flight Deck Hand Microphones HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 2) Headset Earphones / Headphones 3) Active Noise Canceling / Reduction Function (continued) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS Flight Deck Headsets Earphones / Headphones and Boom Microphones HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE 1) Headset Boom Microphones MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 12. PAGE NUMBER: 23-12 MMEL REV. NO.: 8 A - 0 May be inoperative provided: None required. a) Associated hand microphone is installed and operates normally, and b) Repairs are made within three (3) flight days. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - - Any in excess of those required by regulation may be inoperative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C - 1 May be inoperative provided associated flight deck speaker operates normally. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - - Any in excess of those required by regulation may be inoperative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - 0 May be inoperative provided normal audio function of headset is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 12. PAGE NUMBER: 23-13 MMEL REV. NO.: 8 Flight Deck Headsets D Earphones / Headphones and Boom Microphones OPERATOR OTHER THAN A HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE 1) Headset Boom A Microphones - - Any in excess of those required by regulation may be inoperative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. - 0 May be inoperative provided: None required. a) Associated hand microphone is installed and operates normally, and b) Repairs are made in accordance with applicable regulations. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - - Any in excess of those required by regulation may be inoperative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 2) Headset Earphones / Headphones C - 1 May be inoperative provided associated flight deck speaker operates normally. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 3) Active Noise Canceling / Reduction Function D - 0 May be inoperative provided normal audio function of headset is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS Right Side Radio Frequency Management Unit (RFMU) (GV) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 13. PAGE NUMBER: 23-14 MMEL REV. NO.: 8 C 1 0 May be inoperative provided: a) Cross-side tuning function of the left RFMU is operative, b) Radio tuning function of both FMS’s are operative, and c) Inoperative RFMU is selected OFF. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. a) Flight Deck Call Visual Alerting System B 1 0 May be inoperative provided the flight deck audio alerting system is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. b) Flight Attendant Visual Alerting System B Flight crew will coordinate with the flight attendant prior to departure. Alternate means include use of the PA, internal phone system, or a series of chimes from the NO SMOKE / SEAT BELT ON / OFF feature. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 14. Alerting Systems *** (Audio/Visual) *** 1) Passenger Configuration *** *** (continued) NOTE: The flight deck audio alerting must always be operative. 1 0 (O) May be inoperative provided: None required. a) PA system is operative, b) If affected visual alerting system is used for Lavatory Smoke Detector Alerting, an alternate Lavatory Smoke Detector Alert (audio or visual) is installed and operative, and c) Alternate procedures for contacting flight attendants are established and used. NOTE 1: Passenger to Attendant Call System is considered a Non-Essential Equipment and Furnishings (NEF). NOTE 2: Any visual alerting system function(s) that are operative may be used. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. *** 15. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 14. MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS *** PAGE NUMBER: 23-15 MMEL REV. NO.: 8 Alerting Systems (Audio/Visual) (continued) c) Flight Attendant Audio Alerting System B - 0 (O) May be inoperative provided: None required. a) PA system is operative, b) If affected audio alerting system is used for Lavatory Smoke Detector Alerting an alternate Lavatory Smoke Detector Alert (visual or audio) is installed and operative, and c) Alternate procedures for contacting flight attendants are established and used. NOTE 1: Passenger to Attendant Call System is considered a Non-Essential Equipment and Furnishings (NEF). NOTE 2: Any audio alerting system function(s) that are operative may be used. Flight crew will coordinate with the flight attendant prior to departure. Alternate means include use of the PA, internal phone system, or a series of chimes from the NO SMOKE / SEAT BELT ON / OFF feature. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 1 0 (O) May be inoperative provided: None required. a) Flight deck to cabin communication is operative, and b) Alternate procedures are established and used. Flight crew will use the PA or direct oral communications as necessary. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 May be inoperative provided procedures do not require its use. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Handset Systems 1) Passenger Configuration a) Flight Deck (continued) None required. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS Handset Systems 1) Passenger Configuration b) Cabin B - - (O) May be inoperative provided: a) Fifty percent of cabin handsets operate normally, b) On wide-body airplanes, one handset must operate normally at each pair of exit doors, and c) Alternate communication procedures between the affected flight attendants station(s) are established and used. NOTE 1: An operative handset at an inoperative flight attendant seat shall not be counted to satisfy the fifty percent requirement. NOTE 2: Any handset(s) function(s) that is operative may be used. 16. MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 15. PAGE NUMBER: 23-16 MMEL REV. NO.: 8 Radio Tuning Functions (GV-SP, GIV-X) See item 34-45 MCDU for GV-SP, GIVX Radio Tuning Functions relief. None required. Flight crew will ensure alternate procedures are established and used. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS High Frequency (HF) Communication Systems MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 17. PAGE NUMBER: 23-17 MMEL REV. NO.: 8 D - - Any in excess of those required by 14 CFR may be inoperative. None required. C 2 1 (O) May be inoperative while conducting None required. operations that require two LRCS provided: a) SATCOM Voice or Data Link operates normally, b) Alternate procedures are established and used, c) SATCOM Voice coverage is available over the intended route of flight, and d) If SATCOM Voice is to be used over the intended route of flight, SATCOM Voice short codes (INMARSAT) or direct dial commercial numbers (IRIDIUM) must be available. If not available, prior coordination with appropriate ATS (FIR) facility is required. None required. An Inoperative Placard will be placed adjacent to affected Interphone System and will be noted on ADLS. The flight crew shall perform the SATCOM preflight test on the Datalink Manager menu. Refer to the OM for additional details. For GV, the crew will perform a Satcom datalink and voice call prior to departure. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: SATCOM Voice is to be used only as a backup to normal HF Communications. 18. NAVCOM Radio (GV-SP, GIV-X) C 1 0 May be inoperative provided operations do not require its use. None required. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 19. PAGE NUMBER: 23-18 MMEL REV. NO.: 8 Audio Interface Units (AIUs) (GV only) B 2 1 May be inoperative provided flight does not require use of HF radio. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 20. Datalink System (GV) *** C - 0 (O) May be inoperative provided alternate procedures are established and used. None required. Flight crew will use voice over VHF/HF to relay pertinent information to the air traffic management system. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE 1: Data link system is required for ADS-C and/or CPDLC operations. NOTE 2: Datalink must be operative whenever flights in RNP 4 airspace are conducted. D - 0 May be inoperative provided routine procedures do not require its use. NOTE 1: Data link system is required for ADS-C and/or CPDLC operations. NOTE 2: Datalink must be operative whenever flights in RNP 4 airspace are conducted. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 21. PAGE NUMBER: 23-19 MMEL REV. NO.: 8 Modular Radio Cabinet A (MRC) Power Supplies (GV-SP, GIV-X) 2 1 May be inoperative provided: a) Associated Comm and Nav radios and opposite ATC are operative, and b) Repairs are made within one flight day. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Dispatch is acceptable with a MRC 1 or MRC 2 failed and EICAS blue messages “APM FAIL” and “ASCB FAIL” displayed. 22. Headsets Combined with Item 12 in Rev. 8 23. Flight Deck Hand D Microphones OPERATOR OTHER THAN A HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE - 0 Any in excess of those required by regulations may be inoperative. C - 0 May be inoperative provided associated boom microphone operates normally. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 23. COMMUNICATIONS 24. *** PAGE NUMBER: 23-20 MMEL REV. NO.: 8 Communications C Management Function / CMF (GV-SP/GIV-X) - 0 (O) May be inoperative provided alternate procedures are established and used. None required. Flight crew will use voice over VHF/HF to relay pertinent information to the air traffic management system. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE 1: Data Link system is required for ADS-C and / or CPDLC operations. NOTE 2: Datalink must be operative whenever flights in RNP 4 airspace are conducted. D - 0 May be inoperative provided routine procedures do not require its use. NOTE 1: Data Link system is required for ADS-C and / or CPDLC operations. NOTE 2: Datalink must be operative whenever flights in RNP 4 airspace are conducted. 25. Controller Pilot Data *** Link Communications (CPDLC) 1) ATN B1 *** (PM-CPDLC/Link 2000+) D 1 0 (O) May be inoperative provided alternate None required. procedures do not require its use. Flight crew will use voice over VHF/HF or SATCOM to relay pertinent information to the air traffic management system. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 2) FANS 1/A *** (ADS-C/CPDLC) D 1 0 (O) May be inoperative provided enroute operations do not require its use. Flight crew will use voice over VHF/HF or SATCOM to relay pertinent information to the air traffic management system. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 24. ELECTRICAL POWER 1. PAGE NUMBER: 24-1 MMEL REV. NO.: 8 Engine Generators (GV, GV-SP) B 2 1 Except for ER operations, may be inoperative provided: a) APU Generator is used for all phases of flight, b) Airplane is operated at or below FL 450, and c) Standby Electrical System is operative. None required. None required. An Inoperative Placard will be placed above affected Generator Switch on Electric Power Control Panel (EPCP) and will be noted on ADLS. (GIV-X) B 2 1 (O) Except for ER operations, may be inoperative provided: a) APU Generator is used for all phases of flight, b) Airplane is operated at or below FL 450, c) Standby Electrical System is operative, and d) FSECU SPOST is performed manually prior to the first flight of the day for aiplanes equipped with ASC 086 and dispatching with the left generator inoperative. None required. See (O) procedure on next page. An Inoperative Placard will be placed above affected Generator Switch on Electric Power Control Panel (EPCP) and will be noted on ADLS. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: PAGE NUMBER: 24-2 GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. 24. ELECTRICAL POWER NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS (GIV-X) (cont’d) (O) Flight crew will: a) On the Aircraft Maintenance Test Panel place the 'MAINT TEST Switch' and 'Flap Rig Switch' to the ON position, b) In CMC, Select SYSTEM DIAGNOSTICS -> ATA 27 (Flight Controls) -> 41 (Flap / Stabilizer Controller Command Lane) -> TEST: MANUAL FHCM / HSEMU TEST, c) Verify FHCM/HSEMU Manual Test page 1 of 3 is displayed and read and comply with all warnings, cautions, and notes, d) Select confirm and verify FHCM/HSEMU Manual Test page 2 of 3 is displayed, e) Verify the following is displayed on FHCM/HSEMU Manual Test page 2/3: EXPECTED RESULTS INITIAL DGIO 1 DGIO 2 CONDITIONS FSECU CMD FSECU MON A/C On Ground TRUE TRUE Airspeed <45 KTS TRUE TRUE Flap/Stab Rig SW ON TRUE TRUE CMC COMM Active FALSE FALSE HYDRAULIC STATUS PROC1 PROC4 L HYD >2400 PSI TRUE TRUE AUX HYD >2400 PSI FALSE FALSE f) g) Select the “Initialize” softkey on FHCM/HSEMU Manual Test page 2/3, Verify the following FHCM/HSEMU Manual Test page 2/3: INITIAL CONDITIONS A/C On Ground Airspeed <45 KTS Flap/Stab Rig SW ON CMC COMM Active HYDRAULIC STATUS L HYD >2400 PSI AUX HYD >2400 PSI EXPECTED RESULTS DGIO 1 FSECU CMD TRUE TRUE TRUE TRUE PROC1 TRUE FALSE DGIO 2 FSECU MON TRUE TRUE TRUE TRUE PROC4 TRUE FALSE Note: Several seconds will be required after selecting the “Initialize” softkey before CMC COMM Active becomes “True”. (continued on next page) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. SYSTEM & SEQUENCE NUMBERS 24. ELECTRICAL POWER PAGE NUMBER: 24-3 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS (GIV-X) (cont’d) (O) (continued) h) i) j) Select Confirm and verify FHCM/HSEMU Manual Test page 3/3 is displayed, Select the “FHCM/HSEMU Test” softkey, Verify that “FHCM/HSEMU Test In Progress” becomes active approximately 20 seconds, Note: Flap/Stab Maintenance Required (Blue) will also be displayed in CAS while “FHCM/HSEMU Test In Progress” is active. k) Verify the following is displayed on FHCM/HSEMU Manual Test page 3/3: Maintenance Messages Expected FHCM/HSEMU Test In Progress INACTIVE FHCM/HSEMU Test Abort – 115 VAC INACTIVE FHCM/HSEMU Test Abort – Left Hyd INACTIVE FHCM/HSEMU Test Abort – OGS INACTIVE FHCM/HSEMU Test Abort – Switches INACTIVE l) Select Done to complete the test, m) On the Aircraft Maintenance Test Panel place the ‘Flap Rig Switch’ and ‘MAINT TEST Switch’ to the OFF position, and n) Verify that ‘Flaps Failed’(A), ‘Stab Failed’(A), and ‘Flap/Stab Maint Reqd’(B) are NOT displayed in CAS. PROCEDURE PROCEDURE GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 3. Transformer-Rectifier Units (TRUs) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 24. ELECTRICAL POWER APU Generator MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 2. PAGE NUMBER: 24-4 MMEL REV. NO.: 8 B 1 0 (M) (O) Except for ER operations, may be inoperative provided: a) Both Engine Generators are operative, and b) Standby Electrical System is operative. Maintenance will pull and collar APU GCU PWR circuit breaker on left EER G-11. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will ensure: a) BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS. b) Standby Electrical System is operative. (see QRH) An Inoperative Placard will be placed above AUX PWR Switch on EPCP and will be noted on ADLS. C 1 0 (M) Except for ER operations, may be inoperative provided APU is not used. Maintenance will pull and collar APU CONT #1 – left EER C-13 and APU CONT #2 – right EER C-11. Flight crew may accomplish this task if properly qualified and authorized. None required. An Inoperative Placard will be placed above AUX PWR Switch on EPCP and will be noted on ADLS. B 5 4 (M) May be inoperative provided: a) Both Generators are operative, b) Both essential TRUs are operative, c) Auxiliary TRU is operative, d) APU Generator is operative, e) Both Battery chargers are operative, f) Both Main Airplane Batteries are operative, and g) Inoperative TRU circuit breaker on the Power Distribution Box is pulled and collared. Maintenance will pull and collar affected TRU CONTROL CB on Power Distribution Box (PDB). Maintenance will ensure AUX TRU is operative and both essential TRUs are operative. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 5. Main Airplane Batteries MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 24. ELECTRICAL POWER Battery Chargers MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 4. PAGE NUMBER: 24-5 MMEL REV. NO.: 8 B 2 1 (M) May be inoperative provided: a) Both Engine Generators are operative, b) APU Generator is operative, c) Associated Battery Charger circuit breaker on the Power Distribution Box is pulled and collared, and d) Standby Electrical System is operative. Maintenance will: None required. a) Pull and collar CB of associated Battery Charger (located on PDB), and b) Verify associated Battery Charger by utilizing Operational Test located in AMM Chapter 24-34-03. An Inoperative Placard will be placed above Battery Charger Circuit Breakers and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. B 2 1 (M) May be inoperative provided: a) There are no other electrical power source failures, b) Associated Battery cables are disconnected and secured, c) Associated Battery Charger circuit breaker on the Power Distribution Box is pulled and collared, and d) Associated battery circuit breaker is pulled and collared. Maintenance will ensure: a) Standby Electrical System is operative, b) Pull and collar associated "BATT CHGR" and "BATT CONT" CB, and c) Associated battery cables will be disconnected and secured. Refer to AMM Chapter 24-3400. None required. An Inoperative Placard will be placed on affected "BATT 1, BATT 2" Master Switch on the Electric Master Panel and will be noted on ADLS. B 2 1 (M)(O) May be inoperative provided: a) Airplane is operated in day VMC, b) Standby Electrical System is operative, c) Associated Battery cables are disconnected and secured, d) Associated Battery Charger circuit breaker on the Power Distribution Box is pulled and collared, and e) Associated battery circuit breaker is pulled and collared. Maintenance will pull and collar associated "BATT CHGR" and "BATT CONT" CB. In addition, associated battery cables will be disconnected and secured. Refer to AMM Chapter 24-34-00. Flight crew will ensure airplane is operated in day VMC only. An Inoperative Placard will be placed on affected "BATT 1, BATT 2" Master Switch on the Electric Master Panel and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 7. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 24. ELECTRICAL POWER Battery Ammeters (Overhead Panel) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 6. PAGE NUMBER: 24-6 MMEL REV. NO.: 8 C 2 0 May be inoperative provided: a) Associated voltmeter is operative, and b) Both battery charger fail messages are operative. None required. None required. An Inoperative Placard will be placed on affected Battery Ammeter and will be noted on ADLS. C 2 0 May be inoperative provided battery ammeter indications are available in EICAS. None required. None required. An Inoperative Placard will be placed on affected Battery Ammeter and will be noted on ADLS. (EICAS Indication) C 2 0 May be inoperative provided the battery ammeters in overhead panel are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Battery Voltmeters (Overhead Panel) C 2 0 May be inoperative provided associated ammeter is operative. None required. None required. An Inoperative Placard will be placed on Voltmeter and will be noted on ADLS. C 2 0 May be inoperative provided Battery Voltmeter indications are available on EICAS. None required. None required. An Inoperative Placard will be placed on Voltmeter and will be noted on ADLS. C 2 0 May be inoperative provided Battery Ammeters indications are available on EICAS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 2 0 May be inoperative provided Battery Voltmeters in the overhead panel are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (EICAS Indication) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 24. ELECTRICAL POWER 8. PAGE NUMBER: 24-7 MMEL REV. NO.: 8 Electrical Power System EICAS Displays 1) L Gen Voltmeter C 1 0 May be inoperative if the frequency and loadmeter are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 2) L Gen Frequency Meter C 1 0 May be inoperative if the voltmeter and loadmeter are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 3) L Gen Loadmeter C 1 0 May be inoperative if the voltmeter and frequency meter are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 4) R Gen Voltmeter C 1 0 May be inoperative if the frequency and loadmeter are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 5) R Gen Frequency Meter C 1 0 May be inoperative if the voltmeter and loadmeter are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 24. ELECTRICAL POWER 8. PAGE NUMBER: 24-8 MMEL REV. NO.: 8 Electrical Power System EICAS Displays (continued) 6) R Gen Loadmeter C 1 0 May be inoperative if the voltmeter and frequency meter are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 7) APU Voltmeter C 1 0 May be inoperative if the frequency meter and loadmeter are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 8) APU Frequency Meter C 1 0 May be inoperative if the voltmeter and loadmeter are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 9) APU Loadmeter C 1 0 May be inoperative if the voltmeter and frequency meter are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 11) Ext AC Pwr Frequency Meter 12) Ext AC Loadmeter (continued) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 24. ELECTRICAL POWER Electrical Power System EICAS Displays (continued) 10) Ext AC Pwr Voltmeter MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 8. PAGE NUMBER: 24-9 MMEL REV. NO.: 8 D 1 0 May be inoperative provided: a) the frequency meter and loadmeter are operative, and b) External AC power is not used. None required. None required. D 1 0 May be inoperative if external AC power is not used. None required. None required. D 1 0 May be inoperative if the voltmeter and loadmeter are operative. None required. None required. D 1 0 May be inoperative if external AC power is not used. None required. None required. D 1 0 May be inoperative if the frequency and voltmeter are operative. None required. None required. D 1 0 May be inoperative if external AC power is not used. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 24. ELECTRICAL POWER 8. PAGE NUMBER: 24-10 MMEL REV. NO.: 8 Electrical Power System EICAS Displays (continued) 13) Main, Essential and AUX TRU Voltmeters C 5 0 May be inoperative if loadmeters are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 14) Main, Essential and AUX TRU Loadmeters (GV-SP, GIV-X) C 5 0 May be inoperative if the voltmeters are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. C 5 0 May be inoperative provided: a) Voltmeters are operative, and b) Airplane is operated in accordance with AFM Limitations. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 May be inoperative if the loadmeter is operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 May be inoperative if external DC power is not used. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. (GV) 15) Ext DC Pwr Voltmeter (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 24. ELECTRICAL POWER 8. PAGE NUMBER: 24-11 MMEL REV. NO.: 8 Electrical Power System EICAS Displays (continued) 16) Ext DC Pwr Loadmeter D 1 0 May be inoperative if the voltmeter is operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 May be inoperative if external DC power is not used. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. C 4 3 May be inoperative provided associated AC loadmeter and voltmeter are operative and selected for monitoring on the AC Synoptic. None required. None required. An Inoperative Placard will be placed on affected Master Power Switch and will be noted on ADLS. 10. Battery Temperature *** Indicating System D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 11. C 1 0 None required. None required. An Inoperative Placard will be placed adjacent to Standby Electrical Master System and will be noted on ADLS. 9. Master Power Switch Lights (Left, Right, APU, EXT) Standby Electrical System May be inoperative provided both engine driven generators and APU generator are operative. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 24. ELECTRICAL POWER External Power System MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 12. PAGE NUMBER: 24-12 MMEL REV. NO.: 8 D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 13. Low Battery Power *** Audible Warning System (Sonalert) D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 14. D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 15. 50Hz/60Hz AC *** Electrical Power Systems D - 0 (M)(O) May be inoperative provided affected circuit breaker is pulled and collared. Maintenance will pull and collar affected circuit breaker. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will brief the passengers on the items that are inoperative with the failure of the power source for cabin entertainment. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 16. A 2 0 May be inoperative provided: a) Airplane is operated in day VMC conditions, and b) Repairs are made within one (1) flight day. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. A 2 0 May be inoperative provided: a) All other components of the Electrical Power system are operative, and b) Repairs are made within one (1) flight day. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Ground Service Bus System IRU Back Up Batteries (GV) (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 24. ELECTRICAL POWER 16. PAGE NUMBER: 24-13 MMEL REV. NO.: 8 IRU Back Up Batteries (continued) (GV-SP, GIV-X) B 2 1 (M) May be inoperative provided that the affected battery is located in the #2 or #3 IRU back up battery position. Maintenance will move affected battery to the #2 or #3 position. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. A 2 0 May be inoperative provided: a) Airplane is operated in day VMC conditions, and b) Repairs are made within one (1) flight day. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: EICAS message “IRU Sec Pwr Fail” will be displayed. A 2 0 May be inoperative provided: a) All other components of the Electrical Power system are operative, and b) Repairs are made within one (1) flight day. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. D MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE - - As required by 14 CFR. None required. None required. If installed, an Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. May be inoperative provided: None required. a) Seat does not block an Emergency Exit, b) Seat does not restrict any passenger from access to the main airplane aisle, and c) The affected seat(s) are blocked and placarded "DO NOT OCCUPY". None required. A "Do Not Occupy" Placard will be placed on affected seat and will be noted on ADLS. NOTE: See 14 CFR 91.205, 91.509 or 135.167. 2. Passenger Seats D - - NOTE 1: A seat with an inoperative seat belt is considered inoperative. NOTE 2: Inoperative seats do not affect the required number of Flight Attendants. NOTE 3: Affected seat(s) may include the seat(s) behind and/or adjacent outboard seats. (continued) PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS Overwater Equipment MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 25-1 MMEL REV. NO.: 8 GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS 2. PAGE NUMBER: 25-2 MMEL REV. NO.: 8 Passenger Seats (continued) 1) *** 2) Recline Mechanism Underseat Baggage Restraining Bars (continued) D - - (M) May be inoperative and seat occupied provided seat back is secured in the full upright position. Maintenance will ensure seat back is secured in full upright position. None required. A "Do Not Occupy" Placard will be placed of affected seat not secured in up-right position and will be noted on ADLS. D - - May be inoperative and seat occupied provided seat back is immovable in full upright position. None required. None required. A "Do Not Occupy" Placard will be placed of affected seat not secured in up-right position and will be noted on ADLS. C - - (O) May be inoperative provided: a) Baggage is not stowed under seat with inoperative restraining bar, b) Associated seat is placarded “DO NOT STOW BAGGAGE UNDER THIS SEAT”, and c) Procedures are established to alert Cabin Crew of inoperative restraining bars. None required. Flight crew will advise cabin crew which seat is affected and mark this seat with a tag or placard visible to crew and passengers. A "Do Not Stow Baggage Under This Seat" Placard will be placed of affected seat and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS *** MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 2. PAGE NUMBER: 25-3 MMEL REV. NO.: 8 Passenger Seats (continued) 3) a) Armrests Armrests with Recline Mechanism b) Armrest without Recline Mechanism 4) Swivel Mechanism (continued) D - - (M) May be inoperative or missing and Maintenance will ensure seat is seat occupied provided: secured in the full upright position if a) Armrest does not block an armrest is missing. Emergency Exit, b) Armrest does not restrict any passenger from access to the main airplane aisle, and c) If armrest is missing, seat is secured in the full upright position. None required. A "Do Not Occupy" Placard will be placed of affected seat not secured in up-right position and will be noted on ADLS. D - - May be inoperative or missing and seat occupied provided: a) Armrest does not block an Emergency Exit, and b) Armrest does not restrict any passenger from access to the main airplane aisle. None required. None required. A "Do Not Occupy" Placard will be placed of affected seat and will be noted on ADLS. C - - May be inoperative and seat occupied None required. provided: a) Associated seat does not block an Emergency Exit, b) Associated seat does not restrict any passenger from access to the main airplane aisle, and c) Associated seat remains in takeoff position. None required. A "Do Not Occupy" Placard will be placed of affected seat and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE Passenger Seats (continued) 5) Divan High Backs C - - May be inoperative and seat occupied None required. provided: a) Associated seat does not block an Emergency Exit, b) Associated seat does not restrict any passenger from access to the main airplane aisle, and c) Associated seat remains in takeoff position. None required. A "Do Not Occupy" Placard will be placed of affected seat and will be noted on ADLS. Electrical / Electronic Systems / Components C - - (M) May be inoperative and seat occupied provided associated component(s) is deactivated. Maintenance will disconnect bag and stow the electrical connectors. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Crewmember Shoulder Harnesses B Any in excess of those required by flight deck crewmembers (including official observer in observer's seat) may be inoperative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. ***6) 3. MMEL DATE: 11/07/2014 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS *** MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 2. PAGE NUMBER: 25-4 MMEL REV. NO.: 8 - - Flight crew may accomplish this task if properly qualified and authorized. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS 4. PAGE NUMBER: 25-5 MMEL REV. NO.: 8 Observer Seat(s) 1) Primary Observer Seat (including associated equipment) A A - - - - May be inoperative provided: a) A passenger seat in the passenger cabin is made available to an FAA inspector for the performance of official duties, and b) Repairs are made within two (2) flight days. None required. May be inoperative provided: a) Required minimum safety equipment (safety belt and oxygen) is available, b) Seat is acceptable to the FAA inspector for performance of official duties, and c) Repairs are made within two (2) flight days. None required. NOTE 1: These provisos are intended to provide for occupancy of the above seats by an FAA inspector when the minimum safety equipment (oxygen and safety belt) is functional and the inspector determines the conditions to be acceptable. NOTE 2: The pilot-in-command will determine if the minimum safety equipment is functional for other persons authorized to occupy any observer seat(s). (continued) None required. A "Do Not Occupy" Placard will be placed on affected seat and will be noted on ADLS. NOTE: Does not apply to Part 91 operators. None required. A "Do Not Occupy" Placard will be placed on affected seat and will be noted on ADLS. NOTE: Does not apply to Part 91 operators. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS 4. PAGE NUMBER: 25-6 MMEL REV. NO.: 8 Observer Seat(s) (continued) 2) Observer Seat Not Required by 14 CFR (including associated equipment) 5. Megaphones *** D - 0 NOTE: The pilot-in-command will determine if the minimum safety equipment is functional for other persons authorized to occupy any observer seat(s). None required. None required. A "Do Not Occupy" Placard will be placed on affected seat and will be noted on ADLS. NOTE: Does not apply to Part 91 operators. D - - Any in excess of those required by 14 CFR may be inoperative or missing provided: a) Inoperative megaphone is removed from passenger cabin, b) Associated placard is removed or obscured, and c) Required distribution is maintained. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE 1: Megaphones are available to meet 14 CFR 91.513 distribution requirements. NOTE 2: Not required for all Cargo Operations. 6. Flotation Devices D - - Any in excess of those required by 14 CFR may be inoperative. Inoperative equipment will be removed from airplane. NOTE: Flotation Devices are available to meet 14 CFR 91.205, 91.509 or 135.167 distribution requirements. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS 7. "Fasten Seat Belt *** While Seated” Signs or Placards C - - One or more signs or placards may be None required. illegible or missing provided a legible sign or placard is readable from each occupied passenger seat. 8. Storage Bins/Cabin, *** Galley and Lavatory Storage Compartment / Closets C - - (M) May be inoperative provided: a) Procedures are established to secure the affected bin, compartment or closet in the closed position, b) Associated bin, compartment or closet is prominently placarded DO NOT USE, c) Any emergency equipment located in affected compartment is considered inoperative, and d) Affected bin, compartment or closet is not used for storage of any items except for those permanently affixed. NOTE: For overhead bins, if no partitions are installed, the entire overhead bin is considered inoperative. (continued) PAGE NUMBER: 25-7 MMEL REV. NO.: 8 None required. A "Do Not Occupy" Placard will be placed on any affected seat from which signs are not readable and will be noted on ADLS. Maintenance will verify that no None required. emergency equipment is stored in the compartment, secure the compartment CLOSED and placard it against use for storage of any equipment. An Inoperative Placard will be placed on affected Storage Bins/Cabin, Galley and Lavatory Storage Compartment / Closets and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS C MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 8. Storage Bins/Cabin, *** Galley and Lavatory Storage Compartment / Closets (continued) PAGE NUMBER: 25-8 MMEL REV. NO.: 8 - - (M)(O) May be inoperative provided: a) For non-retractable door, affected doors is removed, (continued) b) For retractable doors, affected door is removed or secured in the retracted (fully open) position, c) Affected bin, compartment or closet is not used for storage of any items, except those permanently affixed, d) Affected bin, compartment or closet is prominently placarded DO NOT USE, e) Procedures are established and used to alert crew members and passengers of inoperative bins, compartments or closets, and f) Passengers are briefed that associated bin, compartment or closet is not used. Maintenance will verify that no Flight crew will ensure emergency equipment is stored in the passengers are briefed that bin compartment, secure the or compartment is not used. compartment CLOSED and placard it against use for storage of any equipment. An Inoperative Placard will be placed on affected Storage Bins/Cabin, Galley and Lavatory Storage Compartment / Closets and will be noted on ADLS. Maintenance will verify that no None required. emergency equipment is stored in the compartment, secure the compartment CLOSED and placard it against use for storage of any equipment. An Inoperative Placard will be placed on affected Storage Bins/Cabin, Galley and Lavatory Storage Compartment / Closets and will be noted on ADLS. NOTE 1: For overhead bins, if no partitions are installed, the entire overhead bin is considered inoperative. NOTE 2: Any emergency equipment located in the affected bin, compartment or closet (permanently affixed) is available for use. *** 1) Storage Compartment Key Locks D - 0 (M) May be inoperative in unlocked position provided doors can be secured by other means. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. C MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS A MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 9. Cargo Restraint *** Systems PAGE NUMBER: 25-9 MMEL REV. NO.: 8 - - - - (M) May be inoperative, or missing provided: a) Acceptable cargo loading limits from an approved source, i.e., an Approved Cargo Loading Manual, or Weight and Balance Document are observed, and b) Repairs are made prior to the completion of the next heavy maintenance visit. Maintenance will provide acceptable cargo loading limits from an approved source, i.e., an Approved Cargo Loading Manual, or Weight and Balance Document are observed. May be inoperative, or missing provided cargo compartment remains empty. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH 1 0 (M)(O) Flight Attendant seat may be inoperative provided: a) Affected seat not occupied, b) Flight Attendant displaced by inoperative seat occupies the passenger seat most accessible to the inoperative seat, c) Alternate procedures are established and used as published in crewmember manuals, d) Folding type seat is stowed or secured in the retracted position, e) Passenger seat assigned to flight attendant is placarded “FOR FLIGHT ATTENDANT ONLY”, and f) Repairs are made within two (2) flight days. NOTE 1: An automatic folding seat that will not stow automatically is considered inoperative. NOTE 2: A seat position with an inoperative or missing restraint is considered inoperative. (continued) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS A MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 10. Flight Attendant *** Seat Assembly PAGE NUMBER: 25-10 MMEL REV. NO.: 8 NOTE 3: The above provisos apply to flight attendant seats. Individual operators, when operating with inoperative seats, will consider the locations and combinations of seats to ensure that the proximity to exits and distribution requirements of applicable regulations are met. Maintenance will ensure: a) Folding type seat is stowed or secured in the retracted position, b) Passenger seat assigned to flight attendant is placarded “FOR FLIGHT ATTENDANT ONLY” and c) Repairs are made within two (2) flight days. Flight crew will ensure: a) Affected seat or seat assembly is not occupied, b) Flight attendant displaced by inoperative seat occupies the passenger seat most accessible to the inoperative seat, and c) Alternate procedures are established and used as published in crewmember manuals. An Inoperative Placard will be placed on affected Flight Attendant Seat and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS D MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 10. Flight Attendant *** Seat Assembly (continued) PAGE NUMBER: 25-11 MMEL REV. NO.: 8 1 0 (M) May be inoperative provided: a) Flight Attendant is not required by 14 CFR, b) Affected seat is not occupied, and c) Folding type seat stows automatically or is secured in the retracted position. Maintenance will ensure: a) Folding type seat is stowed or secured in the retracted position, and b) Passenger seat assigned to flight attendant is placarded “FOR FLIGHT ATTENDANT ONLY”. None required. An Inoperative Placard will be placed on affected Flight Attendant Seat and will be noted on ADLS. Maintenance will ensure: a) Folding type seat is stowed or secured in the retracted position, and b) Passenger seat assigned to flight attendant is placarded “FOR FLIGHT ATTENDANT ONLY”. Flight crew will ensure: a) Affected seat is not occupied, and b) Flight attendant displaced by inoperative seat occupies the passenger seat most accessible to the inoperative seat. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE 1: An automatic folding seat that will not stow automatically is considered inoperative. NOTE 2: A seat position with an inoperative or missing restraint system is considered inoperative. For Operators Other Than Holders of an Air Carrier or Commercial Operator Certificate (continued) D 1 0 (M)(O) May be inoperative provided: a) Affected seat is not occupied, b) Flight Attendant displaced by inoperative seat occupies the passenger seat most accessible to the inoperative seat, c) Folding type seat is stowed or secured in the retracted position, and d) Passenger seat assigned to flight attendant is placarded “FOR FLIGHT ATTENDANT ONLY”. Flight crew may accomplish this task if properly qualified and authorized. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 25-12 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS For Operators Other Than Holders of an Air Carrier or Commercial Operator Certificate (continued) NOTE 1: An automatic folding seat that will not stow automatically is considered inoperative. NOTE 2: A seat position with an inoperative or missing restraint system is considered inoperative. NOTE 3: If one side of a dual seat assembly is inoperative and a flight attendant is displaced to the adjacent seat, the adjacent seat must be operative. 11. Galley/Cabin Waste Receptacles Access Doors/Covers C - - (M)(O) May be inoperative provided: a) The container is empty and the access is secured to prevent waste introduction into the compartment, and b) Procedures are established to ensure that sufficient galley/cabin waste receptacles are available to accommodate all waste that may be generated on a flight. Maintenance will ensure container is empty and the access is secured to prevent waste introduction into the compartment. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will ensure procedures are established to ensure that sufficient galley / cabin waste receptacles (trash bags are considered receptacles) are available to accommodate all waste that may be generated. An Inoperative Placard will be placed on affected Galley / Cabin Waste Receptacles Access Doors/Covers and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 25-13 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS 12. Exterior Lavatory *** Door Ashtrays 1) Airplanes with multiple exterior lavatory door ashtray installed A - - Up to and including 50 percent may be missing or inoperative for 10 days. None required. None required. An Inoperative Placard will be placed on affected Exterior Lavatory Door Ashtray and will be noted on ADLS. A - - More than 50 percent may be missing or inoperative for 3 days. None required. None required. An Inoperative Placard will be placed on affected Exterior Lavatory Door Ashtray and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on affected Exterior Lavatory Door Ashtray and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Crew lavatories are included in total aircraft exterior lavatory door ashtray count. 2) Airplanes with only one exterior lavatory door ashtray installed A 1 - 13. External Camera *** System D 1 0 14. Emergency Vision *** Assurance System (EVAS) STC No. SA00892LA D - 0 May be missing or inoperative for 10 days. May be inoperative. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS 15. PAGE NUMBER: 25-14 MMEL REV. NO.: 8 Pilot Seat(s) 1) Vertical Adjustment C - - (M) May be inoperative provided: a) Seat is secured at the individual crewmember’s requirements, and b) Fore-aft adjustment is operative. Maintenance will secure seat as required by proviso a) and ensure that seat is able to move full fore and aft on its track. None required. An Inoperative Placard will be placed on vertical adjustment handle and will be noted on ADLS. 2) Armrest C - - (M) May be inoperative provided: a) Affected armrest is in the upright position or removed, and b) Seat is acceptable to the affected crewmember. Maintenance will ensure armrest is in None required. the up position or removed. An Inoperative Placard will be placed on affected arm rest and will be noted on ADLS. 3) Recline Adjustment C - - (M) May be inoperative provided: a) Seat is secured at a position acceptable to the affected crewmember, and b) Seat is able to move full Fore-Aft on its track. Maintenance will secure seat as required by proviso a) and ensure that seat is able to move full fore and aft on its track. None required. An Inoperative Placard will be placed on recline adjustment handle and will be noted on ADLS. 4) Lumbar Support C - - May be inoperative provided seat is acceptable to the affected crewmember. None required. None required. An Inoperative Placard will be placed on the pilot’s seat adjustment to lumbar support area and will be noted on ADLS. 5) Thigh Support C - - May be inoperative provided seat is acceptable to the affected crewmember. None required. None required. An Inoperative Placard will be placed on the pilot’s seat adjustment to thigh support area and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS 16. Rudder Pedal Adjustment 17. Cockpit Convenience Items (Expired on April 30, 2008) 18. Keyed Locks D - 0 19. Airplane Ladders C - 0 1) D - 0 Ladder Hardware (Pit Pins, Lanyards, etc.) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS C PAGE NUMBER: 25-15 MMEL REV. NO.: 8 2 0 (M) May be inoperative provided: a) Adjustments can be secured in a position that suits individual pilot(s), and b) Position of pedal(s) permits normal full flight control movement. Maintenance will ensure adjustments can be secured in a position that suits individual pilot(s) requirements and position of pedal(s) permits normal full flight control movement. Flight crew may perform (M) procedures if maintenance is not available. None required. An Inoperative Placard will be on the rudder pedal adjustment handle and will be noted on ADLS. May be inoperative provided the associated access panel, door, compartment, or cap is verified secure before each departure. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (O) May be inoperative or removed. None required. Flight crew will ensure An Inoperative Placard will inoperative ladder is secured or be displayed in a prominent removed prior to each departure. position to be seen by flight crew and will be noted on ADLS. None required. None required. Deleted in Rev. 7 An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 25-16 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS 20. Baggage Compartment *** Shelves *** 1) Shelf Stowage Straps D - 0 May be inoperative or removed provided the shelves remain in the down position. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** 2) Shelf Support Straps D - 0 May be inoperative or removed provided the shelves remain in the stowed (up) position and are not used. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 21. Crewmember Flashlight Holder Assemblies (including Flashlight) C - 0 May be inoperative or missing provided None required. crewmember has a flashlight of equivalent characteristics readily available. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. *** 1) Passenger Convenience Itmes (Expired on April 30, 2008) *** 2) Non-Essential D Equipment and Furnishings (NEF) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS Non-Essential Equipment & Furnishings NEF MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 22. PAGE NUMBER: 25-17 MMEL REV. NO.: 8 Deleted in Rev. 7 - 0 May be inoperative, damaged or missing provided item(s) is deferred in accordance with operator’s NEF deferral program. The NEF program, procedures and processes are outlined in the operator’s (insert name) Manual. (M) and (O) procedures, if required, must be available to flight crew and included in appropriate operator’s document. NOTE: Exterior lavatory door ash trays are not considered NEF items. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 24. *** Emergency Medical Kit (EMK) and/or Associated Equipment MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS Automatic External Defibrillator (AED) and/or Associated Equipment MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 23. *** PAGE NUMBER: 25-18 MMEL REV. NO.: 8 A - 0 (O) May be incomplete, missing or inoperative provided: a) AED is resealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit, and b) Repairs are made within 1 flight. None required. Flight crew will ensure AED unit is placarded “DO NOT USE THIS UNIT. SOME REQUIRED ITEMS MAY BE MISSING.”, and repairs are made within 1 flight. An Inoperative Placard will be will be placed on Automatic External Defibrillator and/or Associated Equipment and will be noted on ADLS. D - - Any in excess of those required by 14 CFR may be incomplete, missing, or inoperative. None required. None required. An Inoperative Placard will be will be placed on Automatic External Defibrillator and/or Associated Equipment and will be noted on ADLS. A - 0 (O) May be incomplete, missing or inoperative provided: a) EMK is resealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit, and b) Repairs or replacements are made within 1 flight. None required. Flight crew will ensure EMK unit is placarded “DO NOT USE THIS UNIT. SOME REQUIRED ITEMS MAY BE MISSING.”, and repairs are made within 1 flight. An Inoperative Placard will be will be placed on Emergency Medical Kit (EMK) and/or Associated Equipment and will be noted on ADLS. D - - Any in excess of those required by 14 CFR may be incomplete missing, or inoperative. None required. None required. An Inoperative Placard will be will be placed on Emergency Medical Kit (EMK) and/or Associated Equipment and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 25. EQUIPMENT/FURNISHINGS First Aid Kit (FAK) and/or Associated Equipment MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 25. PAGE NUMBER: 25-19 MMEL REV. NO.: 8 A - - (O) If more than one is required by 14 None required. CFR, only one of the required first aid kits may be incomplete, missing or inoperative provided: a) FAK is resealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit, and b) Repairs or replacements are made within three (3) flight cycles. D - - Any in excess of those required by 14 CFR may be incomplete, missing or inoperative. None required. Flight crew will ensure FAK unit is placarded “DO NOT USE THIS UNIT. SOME REQUIRED ITEMS MAY BE MISSING.”, and repairs are made within three (3) flight cycles. An Inoperative Placard will be will be placed on First Aid Kit and/or Associated Equipment and will be noted on ADLS. None required. An Inoperative Placard will be will be placed on First Aid Kit and/or Associated Equipment and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 26. FIRE PROTECTION Portable Fire Extinguishers MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 26-1 MMEL REV. NO.: 8 D - - Any in excess of those required by 14 None required. CFR may be inoperative or missing provided: a) Inoperative fire extinguisher is tagged inoperative, removed from the installed location, and placed out of sight so it cannot be mistaken for a functional unit, and b) Required distribution is maintained. None required. If installed, an Inoperative Placard will be placed on Pressure Charge Gauge of affected extinguisher and will be noted on ADLS. None required. An Inoperative Placard will be placed adjacent to affected Wing Anti-Ice Switch and will be noted on ADLS. NOTE: Flight crew will ensure operative fire extinguishers are available to meet 14 CFR 91.513 or 135.155 distribution requirements, i.e., one near cockpit, one in cabin, are required for dispatch. 2. Wing Overheat Warning Systems C 2 0 Except for ER operations, may be inoperative provided: a) Wing Anti-ice is not used, and b) Airplane is not operated in known or forecast icing conditions. None required. 3. APU Fire Detection System C 1 0 (M) Except for ER operations, may be inoperative provided: a) APU is not used, and b) APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. Maintenance will ensure APU CONT None required. #1 and APU CONT #2 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. An Inoperative Placard will be placed on APU "MASTER" Switch and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 26. FIRE PROTECTION Rear Baggage Compartment Smoke Detector Systems MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 4. PAGE NUMBER: 26-2 MMEL REV. NO.: 8 C - 0 May be inoperative provided: a) Internal baggage door remains OPEN, and b) Airplane is operated at or below FL 400. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C - 0 May be inoperative provided: a) Rear baggage compartment is not used, b) Internal baggage door remains CLOSED, c) Flight crew investigates baggage compartment for possible fire in the event the "BAG EER HOT" message displays, and d) Airplane is operated in accord-ance with AFM Limitations. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 26. FIRE PROTECTION 5. Lavatory Smoke *** Detection Systems PAGE NUMBER: 26-3 MMEL REV. NO.: 8 C - - (M)(O) For each lavatory, the lavatory smoke detection system may be inoperative provided: a) Lavatory waste receptacle is empty, b) Associated lavatory door is LOCKED, CLOSED and placarded, "INOPERATIVE - DO NOT ENTER", and c) Lavatory is used only by crewmembers. NOTE 1: These provisos are not intended to prohibit lavatory use or inspections by crewmembers. NOTE 2: Lavatory Smoke Detection System is not required for all-cargo operations. Maintenance will ensure Lavatory Smoke Detector CB is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will inspect lavatory to ensure Lavatory Waste Receptacle is empty and Lavatory Door is LOCKED CLOSED. In addition, flight crew will ensure Lavatory is NOT used for any purpose. An Inoperative Placard will be placed on Lavatory Door stating "Inoperative - Do Not Enter" and will be noted on ADLS. NOTE: These provisos are not intended to prohibit lavatory use or inspections by crewmembers. In addition, Lavatory Smoke Detection System is not required for all cargo operations. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 26. FIRE PROTECTION 6. Lavatory Fire *** Extinguisher Systems PAGE NUMBER: 26-4 MMEL REV. NO.: 8 C - - For each lavatory, the lavatory fire extinguisher system may be inoperative provided Lavatory Smoke Detector system is operative. None required. None required. An Inoperative Placard will be placed on the Lavatory Fire Extinguisher and will be noted on ADLS. C - - (M)(O) For each lavatory, the lavatory fire extinguisher system may be inoperative provided: a) Lavatory waste receptacle is empty, b) Associated lavatory door is LOCKED, CLOSED and placarded, "INOPERATIVE - DO NOT ENTER", and c) Lavatory is used only by crewmembers. Maintenance will verify Lavatory Waste Receptacle is empty. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will inspect lavatory to ensure Lavatory Waste Receptacle is empty and Lavatory Door is LOCKED CLOSED. In addition, flight crew will ensure Lavatory is NOT used for any purpose. An Inoperative Placard will be placed on Lavatory Door stating "Inoperative Do Not Enter" and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on Galley Smoke Detector and will be noted on ADLS. NOTE 1: These provisos are not intended to prohibit lavatory use or inspections by crewmembers. NOTE 2: A Lavatory Fire Extinguisher System is not required for all-cargo operations. 7. Galley Smoke *** Detection Systems D - 0 GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 8. Galley Fire *** Extinguishing Systems D - 0 9. C 2 1 10. Flame Detectors *** D - 11. C D 12. Passenger *** Compartment Closet Smoke Detectors MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 26. FIRE PROTECTION Electronic Equipment Rack Overheat Warning System MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS Engine Fire Detection Systems PAGE NUMBER: 26-5 MMEL REV. NO.: 8 None required. None required. An Inoperative Placard will be placed on Galley Fire Extinguisher and will be noted on ADLS. None required. None required. An Inoperative Placard is placed next to either A or B Switch/Light and will be noted on ADLS. 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. - 0 May be inoperative provided door remains None required. OPEN for visual check from crew stations. None required. An Inoperative Placard will be placed on Passenger Compartment Closet Smoke Detectors and will be noted on ADLS. Except for ER operations, one complete loop (A or B) may be inoperative provided the Fault Switch/ Light is pressed to isolate the faulty loop and illuminate the OFF portion of the switch light. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 26-6 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 26. FIRE PROTECTION 13. Entranceway Baggage *** Compartment Smoke Detectors D - - May be inoperative provided door remains None required. OPEN for visual check from crew stations. None required. An Inoperative Placard will be placed on Entranceway Baggage Compartment Smoke Detectors and will be noted on ADLS. 14. Cargo Compartment *** Fire Detection / Suppression Systems C - 0 (O) May be inoperative provided procedures are established and used to ensure the associated cargo compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballst may be loaded in ULDs) and/or fly away kits. Flight crew will verify that cargo compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast, and/or fly away kits. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE 1: Operators MELs should define which items are approved for inclusion in the fly away kits, and which materials can be used as ballast. (Does not preclude the Carriage of empty cargo containers, pallets, ballast, etc.) NOTE 2: Class E cargo compartments require only the installation of smoke or fire detection systems (not suppression). None required. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 26. FIRE PROTECTION 15. APU Fire Bottle *** PAGE NUMBER: 26-7 MMEL REV. NO.: 8 C 1 0 (M)(O) Except for ER operations, may be inoperative provided: a) APU is considered inoperative, b) Both engine driven generators are operative, c) Standby electrical system is operative, and d) APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. Maintenance will pull and collar APU CONT #1 and APU CONT #2 circuit breakers. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will ensure: a) Maintenance procedures are accomplished if maintenance personnel are not available. AFM Normal Procedures. b) Both Engine Generators are operative. c) Standby Electrical Power System is operative. AFM Emergency Procedures. An Inoperative Placard will be placed on APU Fire Bottle and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 27-1 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 27. FLIGHT CONTROLS 1. Rudder Limit Indication System C 1 0 May be inoperative provided Single Rudder Indication System is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 2. Single Rudder Indication System C 1 0 May be inoperative provided Rudder Limit Indication System is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 3. Automatic Ground Spoiler System C 1 0 (O) May be inoperative provided airplane is operated in accordance with AFM Limitations. None required. Flight crew will ensure airplane is operated in accordance with AFM, Section 1, Limitations, and Automatic Ground Spoilers. (Ground Spoiler may be inoperative for takeoff provided Anti-Skid is operative and 20 degrees flaps are used for takeoff and cowl/wing antiice isn’t used for takeoff.) An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 4. Electric Elevator Trim System C 1 0 (O) May be inoperative provided: a) Electric Elevator Trim remains OFF, b) Both Flap/Stabilizer Control Channels are operative, and c) Airplane is operated in accordance with AFM Limitations. None required. Flight crew will ensure Electric Pitch Trim remains "OFF", both Flap/ Stabilizer Control Channels are operative (no messages on CAS), and airplane is operated in accordance with AFM, Section 1, Limitations, Airspeed Limitations. (Maximum Operating Limit Speed is 0.80 Mt.) An Inoperative Placard will be placed next to Pitch Trim Switch and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 27-2 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 27. FLIGHT CONTROLS 5. Control Wheel Elevator C Trim Switches 2 1 (O) May be inoperative provided pilot flying has operative switch. None required. In the event that the operative Elevator Trim Switch fails after dispatch, the crew shall comply with the Jammed Stabilizer procedure in Section 3 – Abnormal Procedures of the applicable AFM. Maximum flap selection is 20 degrees during the approach and landing. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 6. Flap/Stabilizer Control Channels B 2 1 Channel may be inoperative provided: a) Electric Pitch Trim System is operative, and b) Alternate control is verified operative before each departure. None required None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 7. Single Speed Brake Indication System C 1 0 May be inoperative provided Single Rudder Indication System is operative. None required. None required An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. C 2 0 (M)(O) May be inoperative provided affected circuit breaker(s) are pulled and collared. Maintenance will ensure affected circuit breaker(s) are pulled and collared. Flight crew will ensure maintenance procedures are accomplished if maintenance personnel are not available. An Inoperative Placard will be placed next to Elevator Trim Actuator Switch and will be noted on ADLS. 8. Elevator Trim *** Actuator Heater Systems Flight crew may accomplish this task if properly qualified and authorized. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. Autopilot Elevator Servos (GV-SP, GIV-X) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE C 1 0 (M)(O) May be inoperative provided affected circuit breaker(s) are pulled and collared. Maintenance will ensure affected circuit breaker(s) are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will ensure maintenance procedures are accomplished if maintenance personnel are not available. An Inoperative Placard will be placed next to Aileron Trim Wheel and will be noted on ADLS. C 2 1 (M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared. Maintenance will ensure inoperative servo circuit breaker(s) is pulled and collared. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. 11. Autopilot Pitch Trim Servos (GV-SP, GIV-X) C 2 1 (M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared. Maintenance will ensure inoperative servo circuit breaker(s) is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. 12. Autopilot Aileron Servos (GV-SP, GIV-X) PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 27. FLIGHT CONTROLS 10. MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 9. Aileron Trim *** Actuator Heater PAGE NUMBER: 27-3 MMEL REV. NO.: 8 C 2 1 (M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared. Maintenance will ensure inoperative servo circuit breaker(s) is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE C 2 1 (M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared. Maintenance will ensure inoperative servo circuit breaker(s) is pulled and collared. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. Prior to dispatch, the flight crew will discuss the dispatch situation with the stall barrier inoperative and crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be cross-referenced to Normalized Angle of Attack to 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear at the departure of destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist or consider deviation to an alternate airport in the approach and landing case. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. 14. Stall Barrier Systems PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 27. FLIGHT CONTROLS Autopilot Yaw Damper Servos (GV-SP, GIV-X) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 13. PAGE NUMBER: 27-4 MMEL REV. NO.: 8 A 2 1 (M)(O) May be inoperative provided: a) Angle of Attack indication is available on both PFD’s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled, and d) Repairs are made within two (2) flight days. Maintenance will pull and collar the circuit breakers for the Stall Barrier Valve and Stick Shaker associated with the failed system. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 27. FLIGHT CONTROLS 16. MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 15. PAGE NUMBER: 27-5 MMEL REV. NO.: 8 Flight Control Synoptic Display (GV) C 1 0 May be inoperative provided the affected control surface is visually checked for full, free and correct movement prior to each flight. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. (GV-SP, GIV-X) C - 0 May be inoperative provided the affected control surface is visually checked for full, free and correct movement prior to each flight. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. Gust Lock C 1 0 (O) May be inoperative provided flight controls are secured in an alternate manner. None required. Flight crew will ensure affected surfaces by using rope or some other means to secure the rudder pedals and control yoke from moving between flights. Refer to GAC-OIS-14. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. C 1 0 (O) May be inoperative provided airplane is parked in sheltered area unaffected by atmospheric conditions. None required. Flight crew will park the airplane in a sheltered area (hangar) or determine via weather forecast that the rudder, elevator and ailerons won’t be exposed to windy conditions. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 28. FUEL 2. MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 28-1 MMEL REV. NO.: 8 Fuel Tank Temperature Systems (GV, GV-SP) C 2 0 (O) May be inoperative provided: a) Total Air Temperature is used as an indication of fuel temperature, and b) Airplane is operated in accordance with AFM Limitations. None required. Flight crew will ensure Total Air Temperature (TAT) is used as indication of fuel temperature and airplane is operated in accordance with AFM, Section 1, Limitations, Powerplant EICAS Indications. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Fuel Tank Temperature System (GIV-X) C 1 0 (O) May be inoperative provided: a) Total Air Temperature is used as an indication of fuel temperature, and b) Airplane is operated in accordance with AFM Limitations. None required. Flight crew will ensure Total Air Temperature (TAT) is used as indication of fuel temperature and airplane is operated in accordance with AFM, Section 1, Limitations, Powerplant EICAS Indications. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. EICAS or Standby RFMU (GV) / MCDU (GV-SP, GIV-X) Fuel Quantity Indicating Systems C 2 1 (M)(O) May be inoperative provided associated Standby Fuel Quantity Indicating System or EICAS Fuel Quantity Indicating System is operative. Maintenance will ensure tanks are filled using Standby Fuel Quantity Indicating System or EICAS Fuel Quantity Indicating System. Flight crew will ensure associated Standby Fuel Quantity Indicating System or EICAS Fuel Quantity Indicating System is operative. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 28. FUEL EICAS or Standby RFMU (GV) / MCDU (GV-SP, GIV-X) Fuel Quantity Indicating Systems (continued) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 2. PAGE NUMBER: 28-2 MMEL REV. NO.: 8 C C 2 2 1 1 (M)(O) Except for ER operations, either Left or Right Fuel Quantity display may be inoperative provided: a) Both tanks are completely filled using overwing refueling, b) Both fuel flow meters are operative, c) After takeoff, power is set by matching fuel flow indications on both engines, and d) Flight crew maintains a log of fuel burned. Maintenance will ensure BOTH tanks are completely filled using overwing method of refueling. NOTE: Do not pull Fuel Qty circuit breaker as this disables Fuel Level Low caution message. (M)(O) Except for ER operations, either Left or Right Fuel Quantity display may be inoperative provided: a) Affected tank is defueled before each refueling, b) Affected tank is fueled with a known quantity of fuel, c) Both fuel flow meters are operative, d) After takeoff, power is set by matching fuel flow indications on both engines, and e) Flight crew maintains a log of fuel burned. Maintenance will Defuel affected tank before each refueling and refuel it with Known quantity of fuel. NOTE: Total fuel indication will be invalid with an inoperative indicator. Flight crew will ensure: a) Both Fuel Flow Indicating Systems are operative. b) After takeoff, power is set by matching Fuel Flow indications on both engines. c) A log of fuel burned is maintained. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Total Fuel indication will be INVALID with inoperative indicator. Flight crew will ensure: a) Both fuel flow meters are operative, b) After takeoff, power is set by matching fuel flow indications on both engines, and c) A log of fuel burned is maintained. NOTE: Total fuel indication will be INVALID with inoperative indicator. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 28-3 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 28. FUEL 3. Fuel Low Quantity Warning Systems C 2 0 (O) May be inoperative provided: a) Both Fuel Quantity Indicating Systems are operative, b) All Fuel Boost Pumps are operative, and c) Fuel Crossflow Valve is OPENED when either wing tank contains 2,000 pounds or less fuel. None required. Flight crew will ensure: a) BOTH Fuel Quantity Indicating Systems and all Fuel Boost Pumps are operative. (AFM, Section 2, Normal Procedures, Before Starting Engines, Normal Engine Ground Start and After Starting Engines) b) Fuel Crossflow Valve is OPENED when either wing tank contains 2,000 pounds or less fuel. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 4. Fuel Boost Pumps C 4 3 (O) Except for ER operations, may be inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, and d) Airplane is operated in accordance with AFM Limitations. None required. Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative. AFM, Section 2, Normal Procedures, Before Starting Engines. b) BOTH Fuel Low Quantity Warning Systems are operative. AFM, Section 2, Normal Procedures, Before Starting Engines. c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure. An Inoperative Placard will be placed on Affected Fuel Boost Pump "ON/OFF" Switch and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 28. FUEL Fuel Intertank Valve MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. PAGE NUMBER: 28-4 MMEL REV. NO.: 8 C 1 0 (M) Except for ER operations, may be inoperative provided: a) All Fuel Boost Pumps are operative, b) Fuel Crossflow Valve is operative, c) Fuel Quantity Indicating System is operative, and d) Intertank Valve is verified CLOSED and electrically deactivated. Maintenance will deactivate the intertank valve by pulling and collaring appropriate Fuel Intertank circuit breaker. None required. An Inoperative Placard will be placed on Fuel Intertank Valve Switch and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. NOTE: With Fuel Intertank Valve CLOSED and fuel temperature below 0 degrees C, fuel balancing capabilities may be affected. 6. Heated Fuel Return System (HFRS) (GV, GV-SP) C 2 0 May be inoperative provided: a) Flight crew monitors fuel tank temperature, and b) Airplane is operated in accordance with AFM Limitations. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 7. Fuel Boost Pump Warning Systems C 4 3 (O) Except for ER operations, may be inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, and c) Airplane is operated in accordance with AFM Limitations. None required. The flight crew will ensure the Fuel Crossflow Valve and Fuel Intertank is operative; AFM, Section 2, Normal Procedures, Before Starting Engines and Fuel Synoptic and that AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure are complied with. An Inoperative Placard will be placed on affected Boost Pump Warning Annunciator and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 1) Failed CLOSED MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 28. FUEL Fuel Crossflow Valve MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 8. PAGE NUMBER: 28-5 MMEL REV. NO.: 8 C 1 0 (O) Except for ER operations, may be None required. inoperative provided: a) All Fuel Boost Pumps are operative, b) Fuel Intertank Valve is operative, c) Fuel Quantity Indicating System is operative, d) Fuel Intertank Valve is OPEN when either wing tank contains 2,000 pounds or less fuel, and e) Airplane is operated in accordance with AFM Limitations. Flight crew will comply with provisos a), b) and c) using AFM Section 2, Normal Procedures and Fuel Synoptic. Flight crew will OPEN Fuel Intertank Valve when either wing tank contains 2000 lb or less fuel. Airplane is operated in accordance with AFM, Section 1, Limitations, Fuel Balance (1000 lb takeoff, 2000 lb enroute). An Inoperative Placard will be placed on Fuel Crossflow Valve Switch and will be noted on ADLS. Flight crew will use Normal Procedures and Fuel Synoptic to ensure: a) All Fuel Boost Pumps are operative, b) Fuel Intertank Valve is operative, c) Fuel Quantity Indicating System is operative. d) Fuel tank temperature system is operative. An Inoperative Placard will be placed on Fuel Crossflow Valve Switch and will be noted on ADLS. NOTE: Avoid uncoordinated maneuvers when Fuel Intertank Valve is OPEN. 2) Failed OPEN C 1 0 (O) Except for ER operations, may be inoperative provided: a) All Fuel Boost Pumps are operative, b) Fuel Intertank Valve is operative, c) Fuel Quantity Indicating System is operative, d) Airplane is operated in accordance with AFM Limitations, and e) Fuel tank temperature system must be operative. NOTE: Avoid uncoordinated maneuvers when Fuel Intertank Valve is OPEN. None required. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 28-6 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 28. FUEL 9. Pressure Fueling System (Single Point Refueling) D 1 0 10. Ground Service Control Panel D 1 11. Automatic Fueling System D 12. Fuel Cap Chains D (M) May be inoperative provided procedures are established to deactivate Pressure Fueling System. Maintenance will ensure Pressure Fueling System is deactivated by Manually Closing Fuel Precheck Valves and pulling and collaring appropriate (Left or Right) Fueling Shutoff Valve CB. Refer to AMM, Chapter 28-22-00. Flight crew may perform maintenance function if maintenance is unavailable. Flight crew may accomplish this task if properly qualified and authorized. None required. An Inoperative Placard will be placed on Pressure Refueling Port and between Left and Right Remote Fueling Shutoff Switches and will be noted on ADLS. 0 None required. None required. An Inoperative Placard will be placed on Ground Service Control Panel and will be noted on ADLS. 1 0 None required. None required. An Inoperative Placard will be placed on Automatic Fueling System and will be noted on ADLS. - 0 None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 14. Mid Wing Ejector *** (MWE) System (GV, GV-SP only) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 28. FUEL Single Point Refueling Cap MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 13. PAGE NUMBER: 28-7 MMEL REV. NO.: 8 C 1 0 May be inoperative or missing provided the single point refueling receptacle is checked for leaks before every takeoff. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. C 2 0 (O) May be inoperative provided the maximum fuel load for dispatch is limited to 9,000 lb per tank for a total fuel load of 18,000 lb. None required. The flight crew shall ensure that the maximum fuel load is equil to or less than 9,000 lb per tnak for a maximum total of 18,000 lb. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 29-1 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 29. HYDRAULIC POWER 1. Brake Accumulator Pressure Gauge (Nose Wheelwell) D 1 0 None required. None required. An Inoperative Placard will be placed on face of Accumulator Pressure Indicator and will be noted on ADLS. 2. Auxiliary Hydraulic Pump Pressure Indicator C 1 0 May be inoperative provided cockpit Brake Accumulator Pressure Gauge is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 3. Power Transfer Unit (PTU) Hydraulic Pressure Indication C 1 0 (O) May be inoperative provided: a) Left Hydraulic Pressure Indication is operative, b) PTU Hydraulic system is operative, and c) Prior to left engine start, HMG operational check is performed. None required. Flight crew will ensure Hydraulic Pressure Indication is operative and Power Transfer Unit operation is verified by performing successful flap operational test with only right engine running. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 4. PTU Hydraulic Pump (Auto Mode) C 1 0 May be inoperative provided manual mode is verified to be operative before every flight. None required. None required. 5. Auxiliary Hydraulic Pump (Auto Mode) C 1 0 May be inoperative provided the Auxiliary pump is selected ON for takeoff and landing. None required. None required. An Inoperative Placard will be placed on Power Transfer NOTE: With right engine Unit Arm Switch and will be running, select PTU ON. Verify noted on ADLS. PTU pressure is present (3000 psi +300/-400). An Inoperative Placard will be placed on Auxiliary Hydraulic Pump Arm Switch and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 29-2 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 29. HYDRAULIC POWER 6. Left Hydraulic System Quantity Gauge (Ground Service Control Panel Aft Equipment Area) D 1 0 (O) May be inoperative provided quantity is checked by reservoir indicator or using hydraulic quantity indication on hydraulic synoptic before each departure. None required. Flight crew will verify the hydraulic quantity at the reservoir or on hydraulic synoptic prior to each departure. Refer to AMM Chapter 12-1500. An Inoperative Placard will be placed on Ground Service Control Panel and will be noted on ADLS. 7. Right Hydraulic System Quantity Gauge (Ground Service Control Panel Aft Equipment Area) D 1 0 (O) May be inoperative provided quantity is checked by reservoir indicator or using hydraulic quantity indication on hydraulic synoptic before each departure. None required. Flight crew will verify the hydraulic quantity at the reservoir or on hydraulic synoptic prior to each departure. Refer to AMM Chapter 12-1500. An Inoperative Placard will be placed on Ground Service Control Panel and will be noted on ADLS. 8. Left Hydraulic System Quantity Indication (EICAS) C 1 0 May be inoperative provided quantity is checked by reservoir indicator or Ground Service Control Panel Left Hydraulic Quantity gauges before each departure. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 9. Right Hydraulic System Quantity Indication (EICAS) C 1 0 May be inoperative provided quantity is checked by reservoir indicator or Ground Service Control Panel Right Hydraulic Quantity gauges before each departure. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 29. HYDRAULIC POWER Hydraulic Reservoir Temperature Sensors MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 10. PAGE NUMBER: 29-3 MMEL REV. NO.: 8 C 2 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Accuracy of hydraulic quantity indication will be degraded during long flights in cold soak conditions. If Right Hydraulic System (R SYS) sensor has failed in flight, there is no protection against overheating R SYS pumps during Power Transfer Unit (PTU) operation. In flight, with either or both sensors failed, there is no warning of hot hydraulic system temperatures. 11. Hydraulic Reservoir Replenishing System D 1 0 (M) May be inoperative provided hydraulic reservoirs are replenished as needed using approved servicing techniques. Airplane may continue in service provided maintenance personnel replenish hydraulic reservoirs as needed using approved servicing techniques. Refer to AMM Chapter 12-15-00. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 12. Brake Accumulator Pressure Gauge (cockpit dial) C 1 0 May be inoperative provided the Brake Synoptic Page Accumulator Pressure indication is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 1 0 May be inoperative provided: a) Brake accumulator gauge in the nose wheelwell is operative and checked before each takeoff, and b) Auxiliary hydraulic pump is on and running for every takeoff and landing. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 29. HYDRAULIC POWER Brake Synoptic Page Accumulator Pressure Indication MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 13. PAGE NUMBER: 29-4 MMEL REV. NO.: 8 C 1 0 May be inoperative provided the Brake Accumulator Pressure Gauge (cockpit dial) is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 1 0 May be inoperative provided: a) Brake accumulator gauge in the nose wheelwell is operative and checked before each takeoff, and b) Auxiliary hydraulic pump is on and running for every takeoff and landing. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 2. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 30. ICE and RAIN PROTECTION Cowl Anti-Ice Pressure Indication Systems MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 30-1 MMEL REV. NO.: 8 B 2 0 Except for ER operations, may be inoperative provided both EICAS Cowl Anti-Ice Indications are operative. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. B 2 0 Except for ER operations, may be inoperative provided airplane is operated at greater than +10 deg. C SAT. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. B 2 0 Except for ER operations, may be inoperative provided: a) Airplane is operated in VMC, and b) Airplane is not operated in visible moisture. None required. None required. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. Wing Anti-Ice Systems C 2 0 Except for ER operations, may be inoperative provided airplane is not operated in known or forecast icing conditions. None required. None required. An Inoperative Placard will be placed on affected Wing Anti-Ice "OFF/AUTO/ ON" Switch and will be noted on ADLS. 1) Automatic Functions C 2 0 May be inoperative provided airplane is operated in accordance with AFM Limitations. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Refer to AFM Section 1-30-10, 1-30-20, and 1-30-30. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 30. ICE and RAIN PROTECTION 4. MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 3. PAGE NUMBER: 30-2 MMEL REV. NO.: 8 Windshield Heat Systems C 2 1 Except for ER operations, may be inoperative provided airplane is not operated in known or forecast icing conditions. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 1) Windshield Heat Sensors D 4 2 One sensor may be inoperative for each Windshield Heat System None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Side Window Heat Systems C 2 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 1) D 4 2 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 4 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Side Window Heat Sensors One Side Window Heat Sensor may be inoperative for each Side Window Heat System. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 30-3 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 30. ICE and RAIN PROTECTION 5. Anti-Ice Heater Switch Lights B 4 0 (M)(O) May be inoperative provided all other elements of the anti-ice heater indicating system are verified to operate normally. Maintenance will check all other elements of Probe Heat Control Switch and ensure them to be functional. Refer to AMM Chapter 30-31-03. Flight crew will ensure all other elements of Probe Heat Indicating Switch are functioning normally, i.e. when pitot heat is selected ON, appropriate EICAS fail message extinguishes. An Inoperative Placard will be placed on Probe Heat Switch and will be noted on ADLS. 6. Pitot Heaters (GV, GV-SP) B 4 3 (O) Except for ER operations, may be inoperative provided airplane is not operated in visible moisture or known or forecast icing conditions. None required. Flight crew will select MADC sources that are different and not associated with failed pitot heater element. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (GIV-X) B 3 2 (O) Except for ER operations, may be inoperative provided airplane is not operated in visible moisture or known or forecast icing conditions. None required. Flight crew will select MADC sources that are different and not associated with failed pitot heater element. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Ice Detection Systems C 2 0 (O) May be inoperative provided airplane is operated in accordance with alternate AFM procedures. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 7. NOTE: With both Ice Detection Systems inoperative, automatic anti-ice is not available. Refer to AFM Section 1-30-10, 1-30-20, and 1-30-30. Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and the SAT is +10°C or less. Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. C NUMBER REQ’D FOR DISPATCH PROCEDURE 2 0 (M) Except for ER operations, may be inoperative provided: a) Affected Valve(s) are verified CLOSED, and b) Airplane is not operated in known or forecast icing conditions. MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING PROCEDURE For G-V, GV-SP (G550, G500) None required. aircraft: Maintenance will ensure affected Cowl Anti-Ice Valve(s) is/are verified closed IAW RR EMM, task # 30-21-01-040-801. For GIV-X (G450, G350): Maintenance will ensure affected Cowl Anti-Ice Valve(s) is/are Deactivated IAW AMM, Chapter 3021-01, paragraph 1.A and 1.B, Cowl Anti-Ice System – Operational Test (Static) and follow the steps under B.(1) thru B.(3). Flight crew may accomplish this task if properly qualified and authorized. (continued) MMEL DATE: 11/07/2014 PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 30. ICE and RAIN PROTECTION Cowl Anti-Ice Systems MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 8. PAGE NUMBER: 30-4 MMEL REV. NO.: 8 An Inoperative Placard will be placed on or next to affected Cowl Anti-Ice Switch indicting valve position and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 30. ICE and RAIN PROTECTION 8. PAGE NUMBER: 30-5 MMEL REV. NO.: 8 Cowl Anti-Ice Systems (continued) C 2 1 (M) May be inoperative provided: Maintenance will ensure: None required. a) Affected Valves is verified OPEN, a) BOTH HP Bleed Air Systems b) All components of both HP Bleed and BOTH Environmental Air Systems are operative, Control System (ECS) Packs are c) Both Environmental Control operative. System (ECS) Packs are operative, b) Select the affected Cowl Antid) Performance Computer is initialized Ice switch ON and ensure that with COWL ANTI-ICE selected the affected valve circuit ON for either takeoff or landing breaker is pulled or in the when COWL ANTI-ICE valve is OPEN position. Refer to AMM, pressurized, and Chapter 21-21-00, 30-21-00 and e) Airplane is operated in accordance 36-11-00. with AFM Limitations and Flight crew may accomplish this task Performance. if properly qualified and authorized. 1) Automatic Functions C 2 0 May be inoperative provided airplane is operated in accordance with alternate AFM procedures. None required. None required. An Inoperative Placard will be placed on or next to affected Cowl Anti-Ice Switch indicting valve position and will be noted on ADLS. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 10. Windshield Blower *** System 1) Windshield Surface Seal Protection Systems MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 30. ICE and RAIN PROTECTION Cowl Pressure Differential Indication System MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 9. PAGE NUMBER: 30-6 MMEL REV. NO.: 8 C 1 0 May be inoperative provided Cowl AntiIce Pressure Indications are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 (M) May be inoperative provided the Surface Seal coating has been checked to be servicable in accordance with the Maintenance Manual within the last 12 months or 500 flight hours whichever occurs first. Maintenance will verify that None required. effectiveness of windshield coating is in accordance with AMM within the last 12 months or 500 flight hours. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 (M) May be inoperative provided the Surface Seal coating is checked to be serviceable in accordance with the Maintenance Manual. Maintenance will verify that None required. effectiveness of windshield coating is in accordance with AMM. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 May be inoperative provided there is no precipitation falling on the departure and arrival airport at the time of taxi, takeoff and landing. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D 2 0 May be inoperative provided airplane is not operated in precipitation within 5 NM of the airport of takeoff or intended landing. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 30. ICE and RAIN PROTECTION 11. PAGE NUMBER: 30-7 MMEL REV. NO.: 8 Cabin Window Heat System D 1 0 (M) May be inoperative provided: a) Cabin Window Heat switch is selected OFF, and b) Cabin Window Heat System circuit breakers are pulled and collared. Maintenance will ensure: a) Cabin Window Heat switch is selected OFF, and b) Cabin Window Heat System circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. a) Cabin Window Heating Elements D - 0 (M) May be inoperative provided the associated Windown Heat circuit breakers are pulled and collared. Maintenance will pull and collar the affected cabin window heat system circuit breakers. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 2. Flight Data Recorder (FDR) Systems 5. MAINTENANCE 3. (continued) C MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 31. INDICATING / RECORDING SYSTEMS 1. Clocks (Cockpit) D PAGE NUMBER: 31-1 MMEL REV. NO.: 8 NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS - 1 - 1 Any in excess of those required by 14 CFR may be inoperative. None required. None required. An Inoperative Placard will be placed on affected Clock face and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on FDR Control Panel and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. 31. INDICATING / RECORDING SYSTEMS 2. Flight Data A Recorder (FDR) Systems (continued) PAGE NUMBER: 31-2 MMEL REV. NO.: 8 NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS - 0 (Includes FDR function of Combined Voice and Flight Data Recorder (CVFDR)) May be inoperative provided: a) Cockpit Voice Recorder (CVR) is operative, b) Airplane is not dispatched from a designated airport as listed in the operator’s MEL unless: 1. The FDR failure occurs after pushback but before takeoff, or 2. The FDR repair was attempted but was not successful. c) In those cases where repair is attempted but not successful, the airplane may be dispatched on a flight or series of flights until the next designated airport where repair must be accomplished prior to dispatch, and d) Repairs are made within three (3) flight days. None required. None required. An Inoperative Placard will be placed on FDR Control Panel and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Repair category does not apply to Part 91 operators. See 14 CFR 91.609 or 135.152. FDR Recording Parameters required by 14 CFR (continued) A - - Up to three (3) recording parameters may be inoperative provided: a) Cockpit Voice Recorder (CVR) is operative, and b) Repairs are made within 20 calendar days. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE FDR Recording Parameters not Required by 14 CFR A - - May be inoperative provided repairs are made prior to the completion of the next heavy maintenance visit. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Flight Data Recorder (FDR) Systems (Operator Other Than a Holder of an Air Carrier or Commercial Operator Certificate) C - 1 Any in excess of those required by 14 CFR may be inoperative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. A - 0 May be inoperative provided repairs are made in accordance with applicable 14 CFRs. None required. None required. C 1 0 May be inoperative provided airplane is operated in accordance with AFM Appendix on Brake Kinetic Energy and Carbon Brake Cooling. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Brake Temperature Monitoring System (BTMS) NOTE: This item includes the BTMS displayed on the brakes synoptic page. 4. PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 31. INDICATING / RECORDING SYSTEMS 2. Flight Data Recorder (FDR) Systems (continued) 3. PAGE NUMBER: 31-3 MMEL REV. NO.: 8 G Monitor System D 1 0 An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. 31. INDICATING / RECORDING SYSTEMS 5. Electronic Checklist C (GV) PAGE NUMBER: 31-4 MMEL REV. NO.: 8 NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 2 1 May be inoperative provided the checklist module in Fault Warning Computer (FWC) 1 is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. May be inoperative provided the current AFM is carried on board the airplane. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Electronic Checklist (GV-SP / GIV-X) C 1 0 Data Acquisition Unit (DAU) Channels (GV) B 4 3 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 7. Security System *** D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 8. Engine Cowl Open *** Indicating System D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 6. May be inoperative provided right engine cowl is visually confirmed CLOSED before starting APU on the ground. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. 31. INDICATING / RECORDING SYSTEMS 9. Airplane Personality C Modules (APM) (GV-SP, GIV-X) PAGE NUMBER: 31-5 MMEL REV. NO.: 8 NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 4 3 May be inoperative provided APU fire bottle switch cover is installed and operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 10. Plastic Guard Switch Covers D - 1 11. Configuration Management Systems (GV-SP, GIV-X) C 2 1 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 12. InfraRed Counter *** Measuring System (IRCM) or Directional InfraRed Counter Measurers System (DIRCM) D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 14. XM Weather Receiver *** D 15. A Modular Avionics Unit (MAU) Channels (GV-SP/GIV-X) MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 31. INDICATING / RECORDING SYSTEMS 13. Quick Access Recorder D *** (QAR) PAGE NUMBER: 31-6 MMEL REV. NO.: 8 NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Flight crew will review the next worse failures as described in the GAC-OIS-09 Dispatch with MAU Channels Inoperative. Flight crew will discuss contingency procedures should the next worse failure occur and plan accordingly for the flight. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 6 5 (M)(O) May be inoperative provided: Maintenance will pull and collar the (MAU) Channels a) Failed channel is not MAU 1A or associated MAU circuit breakers. MAU 2B, b) No other failures exist in the Avionics System, c) Associated MAU circuit breakers are pulled and collared, d) Alternate procedures are established and used, and e) Repairs are made within two (2) flight days. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 32. LANDING GEAR Anti-Skid System MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 32-1 MMEL REV. NO.: 8 C 1 0 (O) May be inoperative provided airplane is operated in accordance with AFM Limitations. None required. Flight crew will ensure airplane is operated in accordance with AFM, Section 1, Limitations, and Automatic Ground Spoilers. (Ground Spoiler may be inoperative for takeoff provided Anti-Skid is operative and 20 degrees flaps are used for takeoff.) An Inoperative Placard will be placed on Anti-Skid "ON/OFF" Switch and will be noted on ADLS. Flight crew will select ANTISKID "OFF" and follow AntiSkid Off Braking Procedures. AFM, Section 3, Abnormal Procedures, Anti-Skid Failure, Section 1, Limitations, AntiSkid. NOTE: May be inoperative provided AFM performance penalties are applied. Refer to AFM, Section 5, Performance, Reference Accelerate-Stop Distance. 2. Rudder Pedal Steering System C 1 0 May be inoperative provided Nose Wheel Tiller Steering System is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 32-2 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 32. LANDING GEAR 3. Landing Gear Position Indicators Deleted in Revision 7a. 4. Variable Gain Nose Wheel Steering C 1 0 (O) May be inoperative provided the fixed gain steering mode is operative. None required. Flight crew will use tiller steering at or below 60 KCAS only. Above 60 KCAS, use pedal steering only. If pedal steering is unavailable, use rudder inputs and/or differential braking until below 60 KCAS. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 5. Nosewheel Steering Accessory Hardware (Torque Link Lanyards) D - 0 May be inoperative or missing. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 6. Emergency Landing Gear Extension Bottle Pressure Gauge (Nose Wheelwell) B 1 0 May be inoperative provided Emergency Landing Gear Extension Bottle Pressure Cockpit CAS Indication (Summary Page) is operative and checked prior to each flight. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 7. Emergency Landing Gear Extension Bottle Pressure Cockpit CAS Indication (Summary Page) B 1 0 May be inoperative provided Emergency Landing Gear Extension Bottle Pressure Gauge (Nose Wheelwell) is operative and checked prior to each flight. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 32. LANDING GEAR Landing Gear Extension / Retraction System (includes dump valve, gear handle, and blow down bottle) (GIV-X) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 8. PAGE NUMBER: 32-3 MMEL REV. NO.: 8 A 1 0 (O) May be inoperative provided: a) Airplane is operated with the landing gear in the extended position, b) Landing gear handle remains in the down position, c) Ground lock pins are installed to ensure that all three (3) Landing gears are LOCKED down throughout flight, d) Both pilots use cockpit headsets, e) Operations are not conducted in known or forecasted icing conditions, f) Extended over water operations are prohibited, g) Flight is conducted in accordance with AFM Supplement No. GIV2009-01, h) Category II operations are prohibited, i) EFVS operations below 200 feet above touchdown zone elevation are prohibited, and j) Repairs are made within one (1) flight day. None required. Flight crew will install all three landing gear ground lock pins and ensure that the pin’s flags are removed prior to every takeoff. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 32. LANDING GEAR Landing Gear Extension / Retraction System (includes dump valve, gear handle, and blow down bottle) (GV/GV-SP) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 8. PAGE NUMBER: 32-4 MMEL REV. NO.: 8 A 2 0 (O) May be inoperative provided: a) Airplane is operated with the landing gear in the extended position, b) Landing gear handle remains in the down position, c) Ground lock pins are installed to ensure that all three (3) Landing gears are LOCKED down throughout flight, d) Both pilots use cockpit headsets, e) Operations are not conducted in known or forecasted icing conditions, f) Extended over water operations are prohibited, g) Flight is conducted in accordance with AFM Supplement No. GV2009-02, h) Category II operations are prohibited, i) EFVS operations below 200 feet above touchdown zone elevation are prohibited, and j) Repairs are made within one (1) flight day. None required. Flight crew will install all three landing gear ground lock pins and ensure that the pin’s flags are removed prior to every takeoff. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 33. LIGHTS Cockpit/Flight Deck/ Flight Compartment and Instrument Lighting Systems (Excluding EFIS and EICAS) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 33-1 MMEL REV. NO.: 8 C - - Individual lights may be inoperative None required. provided: a) Remaining Lighting System lights are sufficient to clearly illuminate all required instruments, controls and other devices for which they are provided, b) Remaining Lighting System lights are positioned so that direct rays are shielded from flight crewmembers' eyes, and c) Lighting configuration and intensity is acceptable to the flight crew. None required. An Inoperative Placard will be placed above the affected Lighting Rheostat and will be noted on ADLS. None required. An Inoperative Placard will be placed on affected Cabin Interior "ON/OFF" Switch and will be noted on ADLS. NOTE 1: Individual button/switch lights and/or annunciation/indications are excluded from this relief. NOTE 2: Unaided operation (without NVGs) may be permitted with inoperated NVG supplemental lights; cracked or missing filters. 2. Passenger Cabin Interior Illumination Systems D - - May be inoperative provided: a) Cabin emergency lighting is operative, b) Sufficient lighting is operative for crew to perform required duties, and c) Lighting configuration at dispatch is acceptable to flight crew. None required. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 33. LIGHTS Passenger Lighted Information Signs MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 3. PAGE NUMBER: 33-2 MMEL REV. NO.: 8 C - - (M) May be inoperative provided: Maintenance will ensure: a) Associated passenger seat or a) Associated passenger seat or lavatory is not occupied from which lavatory is not occupied, and a passenger lighted information b) Associated seat or lavatory is sign is not readily legible, and blocked and placarded “DO b) Associated seat or lavatory is NOT OCCUPY.” blocked and placarded - DO NOT OCCUPY. None required. An Inoperative Placard will be placed on associated seat or lavatory stating “DO NOT OCCUPY” and will be noted on ADLS. NOTE: These conditions are not intended to prohibit lavatory use or inspections by crewmembers. 1) All Cargo Supernumerary/ Courier Area Lighted Information Signs (continued) C - - (O) May be inoperative and associated passenger seat or lavatory may be occupied provided: a) PA System operates normally, and b) PA System is used to notify passengers and cabin crew when associated sign(s) are placed ON or OFF. None required. Flight crew will ensure other means of communication are established if PA System does not operate. An Inoperative Placard will be placed on inoperative PA System and will be noted on ADLS. C - - (O) May be inoperative provided alternate procedures are established and used to notify couriers/supernumeraries when associated sign(s) are placed ON or OFF. None required. Flight crew will ensure alternate procedures are established when associated sign(s) are placed ON or OFF. An Inoperative Placard will be placed in a prominent position to notify courier/ supernumerary when associated sign(s) are placed ON or OFF and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 33. LIGHTS 3. PAGE NUMBER: 33-3 MMEL REV. NO.: 8 Passenger Lighted Information Signs (continued) The following pertains only to operations involving aircraft with 19 or less passenger seats, wherein certification or operating rules do not require a public address system or flight attendant. 2) 4. Passenger Lighted Information Signs Position Light Bulbs C - - (O) May be inoperative provided alternate procedures are established and used to notify cabin occupants. None required. Flight crew will ensure alternate An Inoperative placard will procedures are established and be placed on inoperative used. Passenger Lighted Information Signs and will be noted on ADLS. C 6 3 May be inoperative provided one light bulb is operative at each position. None required. None required. An Inoperative Placard will be placed on Position (Navigation) Light "ON/OFF" Switch and will be noted on ADLS. C 6 0 May be inoperative provided airplane is not operated at night. None required. None required. An Inoperative Placard will be placed on Position (Navigation) Light "ON/OFF" Switch and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 6. 7. Strobes (Anti-Collision Lights) Wing Inspection Lights (Airplanes with Wing Critical Surfaces Not Visible from Flight Deck) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 33. LIGHTS Beacon Light MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. PAGE NUMBER: 33-4 MMEL REV. NO.: 8 C 1 0 May be inoperative provided airplane is not operated at night. None required. None required. An Inoperative Placard will be placed on Beacon Light "ON/OFF" Switch and will be noted on ADLS. C 1 0 May be inoperative provided Strobes are installed and operative. None required. None required. An Inoperative Placard will be placed on Beacon Light "ON/OFF" Switch and will be noted on ADLS. C 6 3 Bulbs may be inoperative provided one bulb is operative at each position (wingtip and tail). None required. None required. An Inoperative Placard will be placed on Strobe "ON/OFF" Switch and will be noted on ADLS. C 6 2 May be inoperative provided: a) At least one bulb is operative at each wingtip, and b) Airplane is not operated at night. None required. None required. An Inoperative Placard will be placed on Strobe "ON/OFF" Switch and will be noted on ADLS. C 2 0 May be inoperative provided ground deicing procedures do not require their use. None required. None required. An Inoperative Placard will be placed on Wing Inspection Light "ON/ OFF" Switch and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 9. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 33. LIGHTS Landing Lights MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 8. PAGE NUMBER: 33-5 MMEL REV. NO.: 8 B 2 1 May be inoperative provided all three bulbs of the taxi lights are operative. None required. None required. An Inoperative Placard will be placed on affected Landing Light (L LDG) or (R LDG) "ON/OFF" Switch(es) and will be noted on ADLS. C 2 0 May be inoperative provided airplane is not operated at night. None required. None required. An Inoperative Placard will be placed on affected Landing Light (L LDG) or (R LDG) "ON/OFF" Switch(es) and will be noted on ADLS. Taxi Light System C 1 0 None required. None required. An Inoperative Placard will be placed on Taxi "ON/OFF" Switch and will be noted on ADLS. 1) Individual Light Bulbs C 3 0 None required. None required. An Inoperative Placard will be placed on Taxi "ON/OFF" Switch to indicate the inoperative light bulbs and will be noted on ADLS. C 2 0 None required. None required. An Inoperative Placard will be placed on Wing Tip Taxi "ON/OFF" Switch and will be noted on ADLS. 10. Wing Tip Taxi *** Light Systems GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 33-6 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 33. LIGHTS 11. Floor Proximity *** Emergency Escape Path Marking System Lights C - - 12. Pulse Light System *** (Identification Lights) D - 13. Recognition Light *** System D 14. Logo Light *** System D One (1) lamp in each of the solid red light assembly pairs and two (2) lamps of the five (5) lamp floodlight and exit sign emergency floor path lighting assemblies may be inoperative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 0 None required. None required. An Inoperative Placard will be displayed on affected Pulse Light System Light Switch and will be noted on ADLS. 1 0 None required. None required. An Inoperative Placard will be displayed on affected Recognition Light Switch and will be noted on ADLS. 1 0 None required. None required. An Inoperative Placard will be displayed on affected Logo Light Switch and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 33-7 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 33. LIGHTS 15. Ramp Lights *** Systems D - 0 None required. None required. An Inoperative Placard will be displayed on affected Ramp Light Switch and will be noted on ADLS. 16. Flashlight Charging *** Systems D - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 17. D - 0 None required. None required. An Inoperative Placard will be placed nest to Aft Compartment Light Switch and will be noted on ADLS. D 1 0 May be inoperative provided no emergency equipment is carried in the Cargo Compartment. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 May be inoperative provided an operative flashlight is installed in Cargo Compartment. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Aft Compartment Lights (Boiler Room) 18. Cargo Compartment *** Light 19. Pylon Mounted *** Exterior Baggage Loading Light Systems GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 33-8 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 33. LIGHTS 20. Wheel Well Lights D 3 0 21. Exterior Emergency Evacuation Lighting System C 1 0 22. Service Door Lights D - 0 23. Dim and Test Enunciator Channels C - - May be inoperative provided airplane is not operated at night. May be inoperative provided the switch capsule is not used in an emergency procedure where the actuation of the switch is not displayed elsewhere in the cockpit. NOTE: The following switches 1-4 may not be inoperative: 1. GPWS / Ground Spoiler Override 2. Terrain Display (GV) / Terrain Inhibit (GV-SP) 3. CPCS Panel Flight / Landing (2) 4. Door Safety None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 33-9 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 33. LIGHTS 24. Airstair Lights D - 0 May be inoperative provided an alternate means (e.g. flashlight) is used to illuminate the airstairs. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 25. Dome Light D - 0 May be inoperative provided an alternate means (e.g. flashlight) is used to illuminate the vestibule area. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 26. Baggage Compartment Light D 1 0 May be inoperative provided no emergency equipment is carried in the baggage compartment. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 May be inoperative provided an operative flashlight is installed in the baggage compartment. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C - 1 May be inoperative provided the operative None required. flashlight is in good working order in accordance with the applicable 14 CFR. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 27. Cockpit Flashlight GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 33. LIGHTS 29. Tail Position Light *** LED Element Banks MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 28. Wing Tip Position *** Light LED Element Banks PAGE NUMBER: 33-10 MMEL REV. NO.: 8 C 4 2 One may be inoperative per wing tip position. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 4 0 May be inoperative provided airplane is not operated at night. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 2 1 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 2 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. May be inoperative provided airplane is not operated at night. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 34-1 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 1. Directional Compass Reference Sensors B 3 2 (O) May be inoperative provided both PFD Heading Indicating Systems operate independently. None required. Flight crew will ensure that the same IRS is NOT used as the heading source for both pilots. An Inoperative Placard will be placed on Mode Select Unit (MSU) and will be noted on ADLS. 2. Attitude Reference Sensors B 3 2 (O) May be inoperative provided: a) Both PFD Attitude Indicating Systems operate independently, and b) Standby Attitude Indicator is operative. None required. Flight crew will ensure same IRS is NOT used as attitude source for both pilots. An Inoperative Placard will be placed on MSU and will be noted on ADLS. 3. Standby Flight Displays C - 0 Except for ER operations, may be inoperative provided not required by 14 CFR. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 1) Standby Attitude Indicator (ElectroMechanical Gyro Horizon) B - 0 May be inoperative provided: a) Operations are conducted in day VMC only, and b) Operations are not conducted into known or forecast VFR-on-Top Conditions. None required. None required. An Inoperative Placard will be placed on face of Standby Attitude Indicator and will be noted on ADLS. a) Glideslope/ Localizer Indicator C 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** *** (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 3. PAGE NUMBER: 34-2 MMEL REV. NO.: 8 Standby Flight Displays (continued) *** 2) Standby Altimeter/ Airspeed Indicator (combined unit) C 1 0 May be inoperative provided airplane is operated in day VMC only. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** 3) 3-in-1 Standby Attitude, Altitude, Airspeed Indicator Heading (Color Video Display) (GV Only) C - 0 Except for ER operations, the Attitude position indicator may be inoperative provided not required by 14 CFR. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. B - 0 Attitude position indicator may be inoperative provided: a) Operations are conducted in Day VMC only, and b) Operations are not conducted into known or forecast VFR-on-Top Conditions. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** a) Standby Air Data Unit(Altitude and Airspeed Function) C 1 0 May be inoperative provided the airplane is operated in day VMC only. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** b) Standby Heading Display C 1 0 May be inoperative provided all three (3) Heading Reference Systems are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 3. PAGE NUMBER: 34-3 MMEL REV. NO.: 8 Standby Flight Displays (continued) *** 3) 3-in-1 (Color Video Display) (GV Only) (cont’d) *** c) Glideslope / Localizer Function C 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** d) DME Displays C - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** e) FMS Navigation Functions C 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION *** MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 3. PAGE NUMBER: 34-4 MMEL REV. NO.: 8 Standby Flight Displays (continued) 4) 4-in-1 Standby Attitude, Altitude, Airspeed Indicator Heading (Color Video Display) (GV-SP, GIV-X) C - 0 Except for ER operations, the Attitude position indicator may be inoperative provided not required by 14 CFR. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. B - 0 Attitude position indicator may be inoperative provided: a) Operations are conducted in Day VMC only, and b) Operations are not conducted into known or forecast VFR-on-Top Conditions. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** a) Standby Air Data Unit (Altitude and Airspeed Function) C 1 0 May be inoperative provided the airplane is operated in day VMC only. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** b) Standby Heading Display C 1 0 May be inoperative provided all three (3) Heading Reference Systems are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION *** MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 3. PAGE NUMBER: 34-5 MMEL REV. NO.: 8 Standby Flight Displays (continued) 4) 4-in-1 (Color Video Display) (GV-SP, GIV-X) (cont’d) Heading (Color Video Display) (GV-SP, GIV-X) *** c) Glideslope/ Localizer Function C 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** d) DME Displays C - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** e) FMS Navigation Functions C 1 0 None required. None required. C - - None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. An Inoperative Placard will be placed on Radar Control Heads and will be noted on ADLS. 4. Weather Radar Systems Except for ER operations, as required by 14 CFR. NOTE: See 14 CFR 135.173 or 135.175. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION VOR/ILS Navigation Systems MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. PAGE NUMBER: 34-6 MMEL REV. NO.: 8 C - - As required by 14 CFR and no relief may be provided to an inoperative system or component if powered by an emergency bus. None required. None required. An Inoperative Placard will be placed on affected RFMU and will be noted on ADLS. NOTE: Those required by 14 CFR 91.205, 135.161 or 135.165 are operative. 6. 7. Marker Beacon Systems (GV-SP, GIV-X) C 3 0 May be inoperative provided approach procedures do not require its use. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (GV only) C 2 0 May be inoperative provided approach procedures do not require its use. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Automatic Direction Finding Systems C 2 - As required by 14 CFR. None required. None required. An Inoperative Placard will be placed on or next to affected ADF Indicator and will be noted on ADLS. NOTE: See 14 CFR 91.205, 135.161 or 135.165. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION ATC Transponder and Automatic Altitude Reporting Systems MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 8. PAGE NUMBER: 34-7 MMEL REV. NO.: 8 B - 0 May be inoperative provided: a) Operations do not require its use, and b) Before flight, approval is obtained from ATC facilities having jurisdiction over the planned route of flight. None required. None required. An Inoperative Placard will be placed adjacent to RFMU (GV) or MCDU (GVSP/GIV-X) and will be noted on ADLS. D - 1 Any in excess of those required by 14 CFR may be inoperative. None required. None required. An Inoperative Placard will be placed adjacent to RFMU (GV) or MCDU (GVSP/GIV-X) and will be noted on ADLS. NOTE 1: Flight Director, Autopilot, and Transponder must use the same Air Data source for flight into RVSM airspace. NOTE 2: Transponder and altitude reporting capability must be operative for flight into RVSM airspace. *** 1) Elementary and Enhanced Downlink Airplane Reportable Parameters not Required by 14 CFR A - 0 May be inoperative provided: None required. a) Operations do not require its use, and b) Repairs are made before completion of the next heavy maintenance visit. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** 2) ADS-B Squitter Transmissions A - 0 May be inoperative provided: None required. a) Operations do not require its use, and b) Repairs are made before completion of next heavy maintenance visit. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION Distance Measuring Equipment (DME) Systems MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 9. PAGE NUMBER: 34-8 MMEL REV. NO.: 8 D - - Except where en route operations or None required. approach minimums require its use, any in excess of those required by 14 CFR may be inoperative. None required. An Inoperative Placard will be placed on the RFMU (GV) or MCDU (GV-SP/GIV-X) and will be noted on ADLS. NOTE: Those required by 14 CFR 91.205 or 135.165 are operative. 10. Standby RMI (Electro-Mechanical) (GV) C 1 0 May be inoperative provided all three (3) IRS's are operative. None required. None required. An Inoperative Placard will be placed on Standby RMI (GV) and will be noted on ADLS. *** 1) Standby Navigation C Display (Color Video) 1 0 May be inoperative provided all three (3) IRS’s are operative. None required. None required. An Inoperative Placard will be placed on the EBDI (GVSP/GIV-X) and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** 2) DME Displays C 2 0 *** 3) EBDI (Electronic Bearing / Distance Indicator) (GV-SP / GIV-X) C 1 0 May be inoperative provided all three (3) IRS’s are operative. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 34-9 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 11. Radio Altimeter Systems C 2 0 May be inoperative provided: a) Landing weather minimums or operating procedures do not require its use, and b) Other systems affected (E/GPWS, TCAS, Flight Director, Autopilot, Autothrottle, Altimeter Ground Awareness Display, Synthetic Vision Primary Flight Display) are considered. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 12. Long Range Navigation Systems (IRS, GPS and GNSSU) C - - May be inoperative except where en route operations or approach minimums require the use of GPS or GNSSU. None required. None required. An Inoperative Placard will be placed on affected Instrument Controller and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on affected Instrument Controller and will be noted on ADLS. NOTE: For flights conducted in RNP4 airspace, both GPS receivers must be operative. C - - As required by 14 CFR. NOTE: IRS Navigation Function only. See Attitude Reference Sensors for IRS Attitude Function. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 13. PAGE NUMBER: 34-10 MMEL REV. NO.: 8 Terrain Awareness and Warning System (TAWS) Class A TAWS Equipment Required 1) GPWS A 1 0 (O) May be inoperative provided: a) Alternate Procedures are established and used, and b) Repairs are made within two (2) flight days. None required. a) Modes 1-4 A 4 0 (O) May be inoperative provided: a) Alternate Procedures are established and used, and b) Repairs are made within two (2) flight days. None required. b) Test Modes A 1 0 May be inoperative provided: a) GPWS is considered inoperative, and b) Repairs are made within two (2) flight days. None required. (continued) Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION TAWS (continued) c) Glideslope Deviation(s) (Mode 5) *** MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 13. PAGE NUMBER: 34-11 MMEL REV. NO.: 8 d) Advisory Callouts (continued) C - 1 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. B - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. B - 0 (O) May be inoperative provided alternate procedures are established and used. None required. Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C - 0 (O) May be inoperative provided: None required. a) Advisory callout not required by 14 CFR, and b) Alternate procedures are established and used. Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. *** e) Windshear Mode (Reactive) NUMBER REQ’D FOR DISPATCH PROCEDURE B 1 0 (O) May be inoperative provided alternate procedures are established and used. MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE None required. Flight crew will comply with AFM/AOM guidance in windshear situations and recommend procedures when encountering windshear. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (O) May be inoperative provided: None required. a) Alternate procedures are established and used, and b) Windshear Detection and Avoidance System (Predictive) is operative. Flight crew will comply with AFM/AOM guidance in windshear situations and recommend procedures when encountering windshear. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Operator’s alternate procedures should include reviewing windshear avoidance and windshear recovery procedures. C (continued) MMEL DATE: 11/07/2014 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION TAWS (continued) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 13. PAGE NUMBER: 34-12 MMEL REV. NO.: 8 1 0 GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. *** MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION *** MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 13. PAGE NUMBER: 34-13 MMEL REV. NO.: 8 TAWS (conttinued) 2) Terrain System Forward Looking Terrain Avoidance (FLTA) and Premature Descent Alert (PDA) Functions B 1 0 3) Terrain Display C - B 4) Runway Awareness C & Advisory System (RAAS) (continued) (O) May be inoperative provided alternate procedures are established and used. None required. Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 1 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 13. PAGE NUMBER: 34-14 MMEL REV. NO.: 8 TAWS (continued) Class B TAWS Equipment Required *** 1) GPWS A 1 0 (O) May be inoperative provided: None required. a) Alternate procedures are established and used, and b) Repairs are made within two (2) flight days. Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. a) Modes 1 & 3 A 2 0 (O) May be inoperative provided: None required. a) Alternate procedures are established and used, and b) Repairs are made within two (2) flight days. Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. b) Test Mode A 1 0 May be inoperative provided: a) GPWS is considered inoperative, and b) Repairs are made within two (2) flight days. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. c) Modes 2, 4 & 5 C 3 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. *** d) Advisory Callouts *** e) Windshear Mode (Reactive) (continued) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION TAWS (continued) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 13. PAGE NUMBER: 34-15 MMEL REV. NO.: 8 B - 0 (O) May be inoperative provided alternate procedures are established and used. None required. Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C - 0 (O) May be inoperative provided: None required. a) Advisory callouts are not required by 14 CFR, and b) Alternate procedures are established and used. Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 1 0 (O) May be inoperative provided alternate None required. procedures are established and used. Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 13. PAGE NUMBER: 34-16 MMEL REV. NO.: 8 TAWS (continued) 2) Terrain System Forward Looking Terrain Avoidance (FLTA) and Premature Descent Alert (PDA) Functions B 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** 3) Terrain Displays C - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** 4) Runaway Awareness & Advisory System (RAAS) C 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 1 0 None required. Flight crew will comply with AFM/AOM guidance and recommend procedures. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Class C TAWS Equipment *** 1) TAWS/GPWS (O) May be inoperative provided alternate procedures are established and used. NOTE: Any mode that is operative may be used. 14. Lasertrak NDU *** (GV) C 1 0 May be inoperative provided at least one Flight Management System is operative. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION Flight Management Systems (CDU & Nav Computer Only) (GV only) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 15. PAGE NUMBER: 34-17 MMEL REV. NO.: 8 B - 0 Except where en route operations or approach minimums require ite use, may be inoperative provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, and d) Both RFMUs are operative. None required. None required. An Inoperative Placard will be placed adjacent to the CDU and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. One (1) system is required in PRNAV, BRNAV, RNAV 1 and RNAV 2 airspace. 1) Navigation Databases C - - Except where en route operations or approach minimums require a current database, may be out of currency provided: a) Current Aeronautical Charts are used to verify Navigation fixes before dispatch, b) Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight, and c) Approach Navigation Radios are manually tuned and identified. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 16. Navigation *** Management System PAGE NUMBER: 34-18 MMEL REV. NO.: 8 B - 0 Except where en route operations or approach minimums require its use, may be inoperative provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not depend on its use, and d) Both RFMUs are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. One (1) system is required in PRNAV, BRNAV, RNAV 1 and RNAV 2 airspace. 1) Navigation Databases C - - Except where en route operations or approach minimums require a current database, may be out of currency provided: a) Current Aeronautical Charts are used to verify Navigation fixes before dispatch, b) Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight, and c) Approach Navigation Radios are manually tuned and identified. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 34-19 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 17. Lightning Sensor *** Systems (LSS) D - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 18. Stormscope *** D - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 19. B - 0 (M) May be inoperative provided: a) System is deactivated and secured, and b) En route or approach procedures do not require its use. Maintenance or qualified flight crew will ensure system is deactivated by pulling and collaring TCAS Power CB. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C - 0 (M) May be inoperative provided: a) Not required by 14 CFR, b) System is deactivated and secured, and c) En route or approach procedures do not require its use. Maintenance or qualified flight crew will ensure system is deactivated by pulling and collaring TCAS Power CB. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Traffic Alert and Collision Avoidance System (TCAS I) (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 19. PAGE NUMBER: 34-20 MMEL REV. NO.: 8 Traffic Alert and Collision Avoidance System (continued) Traffic Alert and Collision Avoidance System (TCAS II) 1) Combined Traffic Alert (TA) and Resolution Advisory (RA) Dual Display System(s) (continued) B - 0 (M) May be inoperative provided: a) System is deactivated and secured, and b) En route or approach procedures do not require its use. Maintenance or qualified flight crew will ensure system is deactivated by pulling and collaring TCAS Power CB. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C - 0 (M) May be inoperative provided: a) Not required by 14 CFR, b) System is deactivated and secured, and c) En route or approach procedures do not require its use. Maintenance or qualified flight crew will ensure system is deactivated by pulling and collaring TCAS Power CB. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 2 1 May be inoperative on the non-flying pilot None required. side provided: a) TA and RA visual display is operative on the flying pilot side, and b) TA and RA audio function is operative on flying pilot side. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION TCAS II (continued) 2) Resolution Advisory (RA) Display System(s) *** MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 19. PAGE NUMBER: 34-21 MMEL REV. NO.: 8 C 2 1 May be inoperative on non-flying pilot side. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C - 0 (O) May be inoperative provided: a) Traffic Alert (TA) visual display and audio functions are operative, b) TA only mode is selected by the crew, and c) En route or approach procedures do not require its use. None required. Flight crew will verify that the RA Display System is NOT required for the en route and/or approach phase of the proposed flight. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 3) Traffic Alert Display System(s) C - 0 (O) May be inoperative provided: a) RA visual display and audio functions are operative, and b) En route or approach procedures do not require its use. None required. Flight crew will verify that the TA Display System is NOT required for the en route and/or approach phase of the proposed flight. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 4) Audio Functions B 1 0 May be inoperative provided en route or approach procedures do not require use of TCAS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 5) Airspace Selection Function (Above / Normal / Below) C - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 20. Microwave Landing *** Systems (MLS) D 21. C 22. MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS Symbol Generators (GV) PAGE NUMBER: 34-22 MMEL REV. NO.: 8 - - As required by 14 CFR. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (M)(O) May be inoperative provided: a) EFIS displays at pilot’s and copilot's stations are operative from independent Symbol Generators, and b) Both EICAS displays are operative. Maintenance should move inoperative SG to No. 3 position. Refer to AMM Chapter 31-62-00. Flight crew will ensure EFIS Displays at pilot's and copilot's stations are operative from Independent Symbol Generators, and BOTH EICAS Displays (DU 3 and 4) are operative. Crew WILL select ALT for No. 3 SG to power EICAS displays. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Those required by 14 CFR 91.205 [or] 135.161 thru 135.165 are operative. 3 2 Flight crew may accomplish this task if properly qualified and authorized. Guidance Panel Digital Indications and Mode Select Indications 1) Speed Display C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 2) Heading Display C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 22. PAGE NUMBER: 34-23 MMEL REV. NO.: 8 Guidance Panel Digital Indications and Mode Select Indications (continued) 3) VS/FPA Display C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 4) Altitude Select Display C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 5) LNAV C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 6) VNAV C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 7) FLCH C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 22. PAGE NUMBER: 34-24 MMEL REV. NO.: 8 Guidance Panel Digital Indications and Mode Select Indications (continued) 8) Manual Speed C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 9) Bank Select C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 10) BC Select C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 11) Heading Select C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 12) VS/FPA Select C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (continued) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 22. PAGE NUMBER: 34-25 MMEL REV. NO.: 8 Guidance Panel Digital Indications and Mode Select Indications (continued) 13) Alt Hold Select C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 14) Approach C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 15) PFD Command L/R C 1 0 (O) May be inoperative provided the associated value is available in the Primary Flight Display. None required. On initial power up of the airplane, the default is PFD command left PFD. If button is pushed several times, PFD command to the left PFD can be established by pulling and resetting Guidance Panel circuit breakers. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 16) APR Switch C 1 0 May be inoperative provided the associated valve is available in the Primary Flight Display None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION Altitude Alerting System MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 23. PAGE NUMBER: 34-26 MMEL REV. NO.: 8 A - 0 (O) May be inoperative provided: a) Autopilot with altitude hold, and altitude capture operates normally, b) En route operations, i.e. RVSM, do not require its use, c) Airplane does not depart from a designated airport (as listed in the operator’s MEL) where repair or replacement can be made, and d) Repairs are made within three (3) flight days. None required. Flight crew will ensure Autopilot with Altitude Hold is operable. NOTE: Flight into RVSM airspace is not allowed with inoperative Altitude Alerting System. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 1) Aural Alert C - 0 May be inoperative provided: a) Visual alert operates normally, and b) Auto-pilot with altitude hold and altitude capture operates normally. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 2) Visual Alert C - 0 May be inoperative provided: a) Aural alert operates normally, and b) Auto-pilot with altitude hold and altitude capture operates normally. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION (continued) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 24. Display Units *** (GV) PAGE NUMBER: 34-27 MMEL REV. NO.: 8 C 6 5 (M)(O) May be in operative provided: a) Inoperative tube is located in the Copilot's Navigation Display Position (DU #5), b) Standby Attitude Indicator is operative, c) Standby RMI is operative, and d) Alternate procedures are developed for operation without the Copilot's Navigation displays. Maintenance will move the inoperative display unit to the Copilot's Navigation Display Position (DU #5). Refer to AMM Chapter 31-63-03. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will ensure Standby Attitude Indicator and Standby RMI are operative. Alternate Procedures for operation without Copilot's Navigation Display (Pre-Takeoff and PreArrival Crew Briefings) should include crew actions in the event of failure of another DU. Factors concerning abort criteria, takeoff continuance, deviation to alternate airfield and mission continuance should be included in there briefings. For an approach with both copilot's PFD and ND inoperative, it is recommended that Compass Mode be selected on pilot's ND. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 24. PAGE NUMBER: 34-28 MMEL REV. NO.: 8 Display Units (continued) *** Display Units (GV) For DU-885 Equipped Airplanes (continued) C 6 5 (M)(O) May be inoperative provided: a) Inoperative tube is located in the Copilot’s Navigation Display Position (DU #5), b) Standby Attitude Indicator is operative, c) Standby RMI is operative, d) Alternate procedures are developed for operation without the Copilot’s Navigation displays, and e) Terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Maintenance will move the inoperative display unit to the Copilot's Navigation Display Position (DU #5). Refer to AMM Chapter 31-63-03. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will ensure the following: a) Standby Attitude Indicator and Standby RMI are operative, b) Alternate Procedures for operation without Copilot's Navigation Display (PreTakeoff and Pre-Arrival Crew Briefings) should include crew actions in the event of failure of another DU, c) Factors concerning abort criteria, takeoff continuance, deviation to alternate airfield and mission continuance should be included in their briefings, and d) Terminal charts for origin, destination and alternate airports are verified to be current and onboard the aircraft. For an approach with both copilot's PFD and ND inoperative, it is recommended that Compass Mode be selected on pilot's ND. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION Display Units (continued) Display Units (GV-SP, GIV-X) 25. MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 24. PAGE NUMBER: 34-29 MMEL REV. NO.: 8 Standby Magnetic Compass System (Flux Valve) (GV) *** Magnetometer (GV-SP, GIV-X) C 4 3 (M)(O) May be inoperative provided: a) The unit is located in the DU 3 position, and b) The pilot in the left seat flies the airplane. Maintenance will move the inoperative display unit to the DU3 position. Refer to AMM Chapter 3163-03 Flight crew may accomplish this task if properly qualified and authorized. Flight crew will discuss alternate procedures for loss of a second display for all phases of flight including failures during takeoff, approach, landing, and go-around. It is required that the pilot in the left seat fly the airplane. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 1 0 May be inoperative provided all three (3) Heading Reference systems are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 1 0 May be inoperative provided all three (3) IRS’s are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 27. Head Up Display *** System MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 26. Non-Stabilized *** Magnetic Compass PAGE NUMBER: 34-30 MMEL REV. NO.: 8 B 1 0 May be inoperative provided any combination of three (3) Gyro or INS (IRU) Stabilized Compass Systems are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. B 1 0 May be inoperative provided: a) Any combination of two(2) Gyro or INS (IRU) Stabilized Compass Systems are operative, and b) Airplane is operated with Dual Independent Navigation Capability and under Positive Radar Control by ATC on the en route portion of the flight. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. B 1 0 May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two Stabilized Directional Gyro Systems are installed, operative, and used in conjunction with accepted Free Gyro Navigation Techniques. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 May be inoperative provided landing weather minimums or operating procedures do not require its use. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 29. AFIS Printer MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 1) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 28. Airborne Flight *** Information System (AFIS) PAGE NUMBER: 34-31 MMEL REV. NO.: 8 D - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on AFIS Printer and will be noted on ADLS. NOTE: The relief includes the datalink function (GV, GV-SP, GIV-X) and ADSA/ADS-C function (GV-SP, GIV-X). D - 0 Slip-Skid Indicator B 2 1 May be inoperative provided: a) Third attitude indicator is installed and operative, and b) An operative Slip indication is obtained by selecting another IRS source via the Display Controller. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (GV Only) B 2 1 (O) May be inoperative provided electronic slip indicator is replaced by a mechanical slip indicator. None required. Flight crew will ensure mechanical slip indicator is installed. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. B 2 0 May be inoperative provided airplane is operated during day VMC conditions. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 31. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION Data Management Unit (DMU) (GV-SP, GIV-X) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 30. Data Loader *** (GV) PAGE NUMBER: 34-32 MMEL REV. NO.: 8 D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 3 2 Maintenance will pull and collar circuit breaker associated with Micro Air Data Computers. Flight crew will operationally check and assure that the items called out in provisos a) thru d) are operative. An Inoperative Placard will be placed on the instrument panel near the Display Unit affected. Air Data Computers/ Systems 1) Micro Air Data Computers (GV) (M) (O) May be inoperative provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, and e) Airplane is operated in accordance with AFM Limitations. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will comply with all AFM limitations in Section 1-03-30, 1-03-40, and 1-21-10. NOTE: Two systems are required for operation in RVSM airspace. C (continued) 3 2 May be inoperative provided airplane is operated in unpressurized configuration. None required. None required. An Inoperative Placard will be placed on the instrument panel near the Display Unit affected. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 31. PAGE NUMBER: 34-33 MMEL REV. NO.: 8 Air Data Computers/ Systems (continued) 2) Air Data Systems (ADS) (GV-SP, GIV-X) C 3 2 (M) May be inoperative provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, and e) Airplane is operated in accordance with AFM Limitations. Maintenance will pull and collar the ADM circuit breaker associated with the ADS failure. None required. An Inoperative Placard will be placed on Air Data Systems to be seen by flight crew and will be noted on ADLS. None required. An Inoperative Placard will be will be placed on Integrated Avionics Computers (IACs) to be seen by flight crew and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. NOTE 1: Two systems are required for operation in RVSM airspace. NOTE 2: If ADS 2 is failed, the WOW indications on the copilot’s flight control synoptic will be crosshatched. Dispatch is still allowed if the WOW indications on the pilot’s flight control synoptic are shown as valid. 32. Integrated Avionics *** Computers (IACs) (GV) C - 2 May be inoperative provided two bus controllers are operative for dispatch. NOTE: The FMS/PMS/Autothrottle function of the operative IACs may be inoperative as stated elsewhere in this section. The autopilot is addressed in ATA 22. None required. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 34. Airshow Controller *** System MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION Bus Controllers (GV) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 33. PAGE NUMBER: 34-34 MMEL REV. NO.: 8 C - 2 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 1) Cockpit Airshow Display System D - 0 None required. None required. *** An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 2) Cabin Airshow Display System D - 0 None required. None required. *** An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 34-35 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 35. *** Windshear Warning and Flight Guidance System (Reactive) C - 0 (O) May be inoperative provided alternate procedures are established and used. None required. Flight crew will comply with the AFM/AOM guidance on windshear conditions and the recommended procedures for windshear encounters. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 36. *** Windshear Detection and Avoidance System (Predictive) C - 0 (O) May be inoperative provided alternate procedures are established and used. None required. Flight crew will comply with the AFM/AOM guidance on windshear conditions and the recommended procedures for windshear encounters. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 37. *** Cockpit Video Monitors D - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 38. *** Heads Up Checklist D - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 34-36 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 39. *** Enhanced Vision System (EVS) D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** 1) EVS Window Heat D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** 2) Secondary (non-HUD) EVS Display Repeater D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 40. Terrain Server Function/EGPWM Modules (GV-SP, GIV-X) None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 41. *** Electronic Flight Bag May be inoperative provided procedures are not dependent on its use. C Function/EGPWM 2 0 NOTE: Synthetic Vision PFD synthetic terrain will not be available with dual Terrain Server failures, but the full PFD may be used without restriction. Moved to ATA 46 in Rev. 7 GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION Advanced Graphics Modules (AGM) (GV-SP, GIV-X) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 42. PAGE NUMBER: 34-37 MMEL REV. NO.: 8 C Advanced Graphics C Module (AGM) (GV-SP, GIV-X) (ASC 904 - Cert Charlie and ASC 905 – Cert Charlie II and Any later revision to the Operating software) 4 4 3 3 (M)(O) May be inoperative provided: a) The inoperative AGM is located in the AGM 3 position, and b) Crew actions for subsequent failures are established. Maintenance will move the inoperative AGM module to the AGM 3 position. (O) May be inoperative provided: a) The inoperative AGM is electronically switched to the AGM 3 position resulting in DU3 Red Xing, and b) Crew actions for subsequent failures are established. None required. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will discuss the alternate procedures for sharing displays including if a display fails during all phases of flight including takeoff, approach, landing, and go-around. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Flight crew will ensure: a) The failed AGM is electronically switched to the number 3 position, b) Verify that DU 3 is Red X’ed prior to dispatch, c) Dim DU 3 to eliminate the Red X, and d) Discuss alternate procedures for sharing displays in the event a second AGM or DU fails during any phase of flight An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Refer to AFM Sections 2-08-260/261 and Section 3-1611. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 34-38 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 43. Cockpit Printer D 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 44. Cursor Control Devices (GV-SP, GIV-X) C 2 0 May be inoperative provided: None required. a) Both Display Controllers, Weather Radar Controllers, and 2 MCDU’s are operative, and b) Terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** Cursor Control Devices C (GV Only) 2 0 (M)(O) May be inoperative provided: Maintenance will pull and collar the a) Both Display Controllers are circuit breaker for the inoperative operative, and CCD. b) Terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will ensure that terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 45. PAGE NUMBER: 34-39 MMEL REV. NO.: 8 Multifunction Control C Display Units (MCDU) (GV-SP, GIV-X) 3 2 (M) May be inoperative provided: a) The FMS functions and Radio Tuning functions are operative on the remaining MCDU’s, and b) The inoperative MCDU is located in either the No. 1 or the No. 2 position. Maintenance will perform procedures None required. in accordance with AMM Chapter 34-60-03. The inoperative MCDU will be moved to the No. 1 or No. 2 position. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: MCDU 3 has Backup Radio Tuning functions. 1) Flight Management System (FMS) Functions (GV-SP, GIV-X) (continued) B 3 1 Except where en route operations or approach minimums require its use, may be inoperative provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, and c) Procedures do not require its use. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. RNP RNAV including PRNAV and BRNAV only require a single FMS. None required. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 45. PAGE NUMBER: 34-40 MMEL REV. NO.: 8 Multifunction Control Display Units (MCDU) (GV-SP, GIV-X) (continued) 2) a) Navigation Database C - - Except where en route operations or None required. minimums require a current database, may be out of currency provided: a) Current Aeronautical Charts are used to verify Navigation fixes before dispatch, b) Procedures are established and used to verify status and suitability of Navigation Facilities used to define the route of flight, and c) Approach Navigation Radios are manually tuned. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Radio Tuning Functions (GV-SP, GIV-X) B 3 2 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 34-41 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 46. Advanced Graphics Module (AGM) Databases (GV-SP, GIV-X) C - 0 May be out of currency provided: a) Current IFR/VFR Aeronautical Charts or appropriate airport information charts are used to verify the information before dispatch, b) Procedures are established and used to verify the status and suitability of Navigation Facilities used to define the route of flight, and c) Approach Navigation Radios are manually tuned and identified. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 47. Charts Function (GV-SP, GIV-X) D 2 0 May be inoperative provided current None required. aeronautical charts are carried onboard the airplane and available to the flight crew. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 1) C 4 0 May be out of currency provided the terminal charts for the origin, destination and alternate airports are verified to be current. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 4 0 May be out of currency provided the terminal charts for the origin, destination and alternate airports are verified to be current and on board. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D 1 0 May be inoperative provided alternate procedures are established for the use of the Enhanced Vision System (EVS) display function. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 48. Charts Database Video Function (GV-SP, GIV-X) GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION *** MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 49. *** PAGE NUMBER: 34-42 MMEL REV. NO.: 8 Automatic Dependent Surveillance-Broadcast (ADS-B) System D 1) Cockpit Display and Traffic Information (CDTI) D - 0 May be inoperative provided it is not required by 14 CFR. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: If ADS-B is installed in lieu of or as a replacement for 14 CFR required equipment, the repair category in the operator’s MEL will be the same as that of the 14 CFR required equipment. - 0 NOTE: Cockpit Display Traffic Information (CDTI) display of data from other airplane systems may be used. *** 2) CDTI Control Panel D - 0 *** 3) Date Link Transmitter(s) D - 0 May be inoperative provided: a) Flight ID can be set, and b) Screen display is acceptable to the flight crew. NOTE: In some airplanes the Data Link Transmission is an integral part of the transponder and relief is provided in that section. *** 4) Data Link Receivers D - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. *** 5) ADS-B Applications D - 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION Right Side Display Controller (GV Only) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 50. PAGE NUMBER: 34-43 MMEL REV. NO.: 8 A 1 0 (M) (O) May be inoperative provided: a) The weather at the destination is forecast to be VFR (1,000 ft ceiling and three (3) miles visibility), b) An alternate airport is specified in the flight plan which has VFR weather forecast (1,000 ft ceiling and three (3) miles visibility), c) Both VOR and ADF navigation receivers are operative, d) Flight is conduncted based on short range navigation sources only being available, e) Navigation sufix in the IFR flight plan clearly indicates that the airplane is not capable of any RNP required navigation capability, f) Flight is conducted in airspace where the availability of navigation by short range navigation receivers (VOR/ADF) is assured, g) One DBDI or Standby RMI or Secondary Navigation Display is operative, h) Associated Display Controller circuit breaker is pulled and collared. i) Alternate procedures are established and used, and j) Repairs are made within one (1) flight day. Maintenance will ensure associated Display Controller circuit breaker for the failed Display Controller is pulled and collared. The flight crew shall prepare and display a TOLD (Takeoff and Landing Data) card pror to takeoff and prior to approach and landing. An Inoperative Placard will be placed on the Right Side Display Controller and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION Right Side Display Controller (GV-SP/GIV-X Only) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 50. PAGE NUMBER: 34-44 MMEL REV. NO.: 8 A 1 0 (M)(O) May be inoperative provided: Maintenance will pull and collar a) FMS is the navigation source on associated Display Control circuit both PFD’s, breaker. b) Destination and alternate airports have either LPV, GPS or FMS overlay approaches available without NOTAM restrictions for airplanes not equipped with Enhanced Navigation Package, c) Destination and alternate airports have either LPV, GPS, FMS overlay, or ILS approach available without NOTAM restrictions for airplanes equipped with Enhanced Navigation Package, d) No other display system failures exist, e) Associated Display Controller circuit breaker is pulled and collared, f) Alternate procedures are established and used, and g) Repairs are made within two (2) flight days. Flight crew will verify the required approaches are available at the destination and alternate airports without being NOTAMed out of service or unusable. When weather conditions exist at the destination or alternate airport during the approach, the PNF will be prepared to announce approach minimums in the event the operative Display Controller fails en route. An Inoperative Placard will be placed on the Right Side Display Controller and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 34-45 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 34. NAVIGATION 51. *** Synthetic Vision Primary Flight Display (SV-PFD) Functions D 2 0 None required. None required. 52. *** DDA (Digital to Discrete Adapter) (GV only) D 2 0 53. *** GNSSU WAAS (Wide Area Augmentation System or SBAS – Space Based Augmentation System) Function D 2 *** 1) LPV Enable Switches (GV Only) C 54. CAS Scroll Switches D An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. May be inoperative provided approach minimums do not require its use. None required. None required. 0 WAAS function may be inoperative provided en route and approach procedures do not require its use. None required. None required. 2 0 May be inoperative provided approach procedures do not require its use. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 2 0 May be inoperative provided both CCD’s are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 35. OXYGEN 2. MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 35-1 MMEL REV. NO.: 8 Passenger Oxygen System and Supply B - - As required by 14 CFR. Cabin Oxygen ON Warning System C 1 0 May be inoperative provided: a) Cabin Altitude and Differential Pressure Indicators are operative, and b) Cabin Altitude Pressure Warning System is operative. None required. None required. An Inoperative Placard will be placed above "ON" position on Oxygen Control Panel and will be noted on ADLS. C 1 0 (O) May be inoperative provide airplane is operated in unpressurized configuration. None required. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM Air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard will be placed above "ON" position on Oxygen Control Panel and will be noted on ADLS. None required. None required. NOTE: Minimum oxygen supply for dispatch will be computed from data in the applicable AFM Supplement for the Oxygen System STC with reference to the requirements of 14 CFR 91.211. An Inoperative Placard will be placed on affected Oxygen Control Panel or Mask Unit and will be noted on ADLS. Additionally, affected seats shall be blocked and placarded. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MMEL REV. NO.: 8 PAGE NUMBER: 35-2 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL PROCEDURE 7. PLACARDING PROCEDURE 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 3. 35. OXYGEN NUMBER REQ’D FOR DISPATCH 4. MMEL REMARKS OR EXCEPTIONS 5. MAINTENANCE PROCEDURE NOTE: Information regarding the oxygen system capabilities for each airplane can be found in the Airplane Flight Manual Supplement for Oxygen Systems. The following document number, G450/G350 – GC41453M000, G550/G500 – GC51453M004 or GV – GC52712M001 are associated with the Oxygen Flight Manual Supplements however, each operator must verify that the document number is applicable to the particular airplane. EXAMPLE OF G550 OXYGEN SYSTEM: OXYGEN REQUIRED FOR DE-PRESSURIZATION AND CONTINUED CRUISE REQUIRED BOTTLE PRESSURE AT DISPATCH TIME NUMBER OF PASSENGERS (HR:MIN) 0 1 2 4 6 8 10 15 19 1:00 413 447 482 551 621 690 759 932 1071 1:30 508 560 613 717 822 927 1031 1293 1502 2:00 603 673 743 883 1023 1163 1303 1653 1933 2:30 699 786 874 1049 1225 1400 1575 2014 25000 3:00 794 899 1005 1215 1426 1637 1847 3:30 890 1013 1136 1382 1628 1874 4:00 985 1126 1266 1548 1829 4:30 1080 1239 1397 1714 2030 5:00 1176 1352 1528 1880 1:00 369 397 424 479 534 589 644 782 892 1:30 440 481 522 605 687 770 852 1058 1223 2:00 510 565 620 730 840 950 1060 1334 1554 2:30 581 650 718 855 993 1130 1267 1611 1885 20000 3:00 651 734 816 981 1146 1310 1475 1887 3:30 722 818 914 1106 1298 1491 1683 2163 4:00 792 902 1012 1232 1451 1671 1890 4:30 863 986 1110 1357 1604 1851 5:00 933 1070 1208 1482 1757 2031 1:00 342 355 369 397 425 453 481 550 606 1:30 396 416 436 476 517 557 597 698 778 2:00 450 477 503 556 608 661 713 845 950 2:30 505 537 570 635 700 765 830 992 1122 15000 3:00 559 598 637 714 791 869 946 1140 1295 3:30 614 659 703 793 883 973 1063 1287 1467 4:00 668 719 770 873 975 1077 1179 1435 1639 4:30 722 780 837 952 1066 1181 1296 1582 1811 5:00 777 840 904 1031 1158 1285 1412 1730 1984 CRUISE ALTITUDE (FT) Based on pressure reading at 70ºF. Includes oxygen for three crewmembers breathing 100% oxygen for emergency descent plus two minutes. Normal dillution for remainder of flight. Increase oxygen required by 37 PSIG for each crewmember on oxygen at/above FL410 for each 60 minutes. Maximum system pressure is 1800 PSIG. Values in excess of 1800 are shown for interpolation purposes only. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 4. Portable Oxygen *** Dispensing Units (Bottle and Mask) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE D 2 0 May be inoperative provided the associated cockpit gauge is operative and monitored. None required. None required. An Inoperative Placard will be placed on Oxygen Service Panel Gauges and will be noted on ADLS. B - - Any in excess of those required by 14 CFR may be inoperative or missing provided required distribution is maintained throughout airplane. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Any bottle not properly serviced is considered inoperative and should be removed. 5. Oxygen Supply Warning Systems PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 35. OXYGEN Oxygen Service Panel Pressure Gauges MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 3. PAGE NUMBER: 35-3 MMEL REV. NO.: 8 C 2 0 May be inoperative provided associated cockpit gauge is operative and monitored. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 35-4 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 35. OXYGEN 6. Protective Breathing *** Equipment (PBE) D - - Any in excess of those required by 14 CFR may be inoperative or removed provided location placarding is removed or obscured. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 7. Electronic Equipment *** Rack Oxygen Pressure Gauges D - 0 May be inoperative provided cockpit gauges are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 8. Cockpit Oxygen Pressure Indications C - 0 May be inoperative provided: a) Oxygen Service Panel Pressure Gauges are operative and checked before every takeoff, and b) Crew Oxygen Off and Passenger Oxygen Off messages are not displayed on the CAS prior to every takeoff. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 9. Therapeutic Oxygen C - - As required by 14 CFR. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 35-5 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 35. OXYGEN 10. High Landing Field *** Elevation Passenger Oxygen Controller High Altitude Switch (GV-SP/GIV-X) D 1 0 May be inoperative provided the maximum Landing Field Elevation does not exceed 14,500 feet. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 1) High Altitude Switch *** Light (GV-SP/GIV-X) D 1 0 May be inoperative provided the switch position is verified to be depressed in whenever the Landing Field Elevation exceeds 14,500 feet. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 36. PNEUMATIC 1. PAGE NUMBER: 36-1 MMEL REV. NO.: 8 Bleed Air Systems (GV, GV-SP) 1) Pressurized Configuration C 2 1 (M) Except for ER operations, may be inoperative provided: a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF, b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, and d) Airplane is operated in accordance with AFM Limitations. NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN. Maintenance will CLOSE None required. inoperative Bleed Control Valve and electrically deactivate affected system. If failure occurs with 1) Right Bleed Air Control Valve: Select Right Bleed Air Valve OFF utilizing R Eng Bleed Air Switch and Pull R Bleed CONT Circuit Breaker (CB). 2) Left Bleed Air Control Valve: Select Left Bleed Air Valve OFF utilizing L Eng Bleed Air Switch and Pull Left Bleed CONT Circuit Breaker (CB). In addition, opposite Engine Bleed Air System and Isolation Valve will be verified operative and Isolation Valve selected OPEN. Refer to AMM Chapter 36-12-00. Flight crew may accomplish this task if properly qualified and authorized. (continued) An Inoperative Placard will be placed above the affected Bleed Air Control Switch and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 36. PNEUMATIC 1. PAGE NUMBER: 36-2 MMEL REV. NO.: 8 Bleed Air Systems (GV, GV-SP) (continued) 2) Unpressurized Configration (continued) C 2 0 (M)(O) Except for ER operations, may be inoperative provided: a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF, b) Airplane is not operated in forecast or known icing conditions, and c) Airplane is operated in accordance with AFM Limitations. Maintenance will ensure both Bleed Air Valves are CLOSED and deactivated electrically. Flight crew may accomplish this task if properly qualified and authorized. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM Air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard will be placed above the affected Bleed Air Control Switch(es) and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 36. PNEUMATIC 1. PAGE NUMBER: 36-3 MMEL REV. NO.: 8 Bleed Air Systems (continued) (GIV-X only) 1) Pressurized Configuration C 2 1 (M) Except for ER operations, may be inoperative provided: a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF, b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, d) Airplane is not operated in forecast or known icing conditions, and e) Airplane is operated in accordance with AFM Limitations. Maintenance will CLOSE associated Bleed Control Valve and electrically deactivate system. In addition, opposite Engine Bleed Air System and Isolation Valve will be verified operative and Isolation Valve selected OPEN. Refer to AMM Chapter 36-12-00. None required. An Inoperative Placard will be placed above both Bleed Air Control Switches and will be noted on ADLS. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM Air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard will be placed on affected Valve(s) and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN. 2) Unpressurized Configuration C 2 0 (M)(O) Except for ER operations, may be inoperative provided: a) Affected Valve(s) is verified CLOSED, b) Airplane is not operated in known or forecast icing conditions, and c) Airplane is operated in accordance with AFM Limitations. NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN. Maintenance will ensure all affected Valve(s) are verified CLOSED. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 36. PNEUMATIC 2. PAGE NUMBER: 36-4 MMEL REV. NO.: 8 Bleed Air Hot Warning Systems 1) Pressurized Configuration C 2 1 (M) Except for ER operations, may be inoperative provided: a) Associated Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF, b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, d) Airplane is not operated in known or forecast icing conditions, and e) Airplane is operated in accordance with AFM Limitations. NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN. (continued) Maintenance will CLOSE associated Bleed Control Valve and electrically deactivate system. In addition, opposite Engine Bleed Air System and Isolation Valve will be verified operative and Isolation Valve selected OPEN. Refer to AMM Chapter 36-12-00. Flight crew may accomplish this task if properly qualified and authorized. None required. An Inoperative Placard will be placed above both Bleed Air Control Switches and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 36. PNEUMATIC 2. PAGE NUMBER: 36-5 MMEL REV. NO.: 8 Bleed Air Hot Warning System (continued) 2) Unpressurized Configuration C 2 0 (M)(O) Except for ER operations, may be inoperative provided: a) Associated Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF, b) Airplane is not operated in forecast or known icing conditions, and c) Airplane is operated in accordance with AFM Limitations. Maintenance will ensure both Bleed Air Valves are CLOSED and deactivated electrically by verifying the capsules indicate OFF. Flight crew may accomplish this task if properly qualified and authorized. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full OPEN position with RAM Air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight. An Inoperative Placard will be placed above both Bleed Air Control Switches and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 36. PNEUMATIC Isolation Valve MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 3. PAGE NUMBER: 36-6 MMEL REV. NO.: 8 C 1 0 (M) May be inoperative provided: a) Both Bleed Air Systems are operative, b) Both Environmental Control Systems (ECS) Packs are operative, c) Isolation Valve is electrically deactivated, d) Isolation Valve is verified CLOSED, and e) Airplane is operated in accordance with AFM Limitations. Maintenance will ensure BOTH None required. Bleed Air System and Environmental Control System (ECS) Packs are operative. In addition, Isolation Valve is to be electrically deactivated and verified "CLOSED". Refer to AMM Chapters 21-51-00 and 36-1200. An Inoperative Placard will be placed on Isolation Valve Switch and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. NOTE: Valve must be OPENED manually during left engine start. 4. Bleed Air System Switch Capsule Lights C 4 0 May be inoperative provided Bleed Air System indications are available on the Synoptic display. None required. None required. An Inoperative Placard will be placed on Bleed Air System Switch Capsule Lights and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 38. WATER/WASTE Potable Water Systems MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 38-1 MMEL REV. NO.: 8 C - - (M) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, b) Associated system components are verified not to have leaks, and c) Passengers are advised of the inoperative water system. Maintenance will ensure appropriate procedures are established to deactivate applicable system components and verify that components do not have leaks. None required. An Inoperative Placard will be placed on Portable Water System and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. NOTE: Any portion of system which operates normally may be used. 2. Lavatory Waste Systems (Including Wheelchair Accessible Lavatories) C - - (M) May be inoperative provided: Maintenance will drain the system a) System is drained, and and placard the access door to b) Procedures are established to ensure prohibit servicing. that system is not serviced. Flight crew may accomplish this task if properly qualified and authorized. None required. An Inoperative Placard will be placed on Portable Water System and will be noted on ADLS. C - - (M) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have leaks. None required. An Inoperative Placard will be placed on Lavatory Waste System and will be noted on ADLS. NOTE: Any portion of system which operates normally may be used. (continued) Maintenance will ensure appropriate procedures are established to deactivate applicable system components and verify that components do not have leaks. If maintenance is not available, flight crew may perform the procedure. Flight crew may accomplish this task if properly qualified and authorized. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 38. WATER/WASTE 2. PAGE NUMBER: 38-2 MMEL REV. NO.: 8 Lavatory Waste Systems (Including Wheelchair Accessible Lavatories) (continued) C - - (M) Associated lavatory system(s) may be inoperative provided: a) Associated components are deactivated or isolated to prevent leaks, and b) Associated lavatory door(s) is secured CLOSED and placarded “INOPERATIVE - DO NOT ENTER. Maintenance will ensure appropriate procedures are established to deactivate applicable system components. If maintenance is not available, flight crew may perform the procedure. None required. An Inoperative Placard will be placed on Lavatory Waste System and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. NOTE: These provisos are not intended to prohibit inspections by crewmembers. 3. Lavatory Dump/Drain System C - - May be inoperative provided: a) Dump valve is secured in the CLOSED and LOCKED position, and b) System is checked for leaks before every flight. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 4. Vacuum Toilet Holding Tank Indicator D 1 0 May be inoperative provided: a) Tank is verified to be serviced prior to the first flight of the day, and b) Tank is serviced after the last flight of the day. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. SYSTEM & SEQUENCE NUMBERS 45. CENTRAL MAINTENANCE COMPUTER 1) Maintenance Data D Acquisition Unit (MDAU) (GV) 2) Central Maintenance Computer (CMC) (GV-SP, GIV-X) PAGE NUMBER: 45-1 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 1 0 C 1 0 C 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. May be inoperative provided all faults are recorded after each flight. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. (M) May be inoperative or missing provided: a) All faults are recorded after each flight, and b) The CMC module is replaced with an Airflow Blockage Module (ABM) if the CMC module is removed from the MAU. Maintenance will ensure CMC module is removed for maintenance and is replaced with an Air Blockage Module (ABM). Refer to AMM Chapter 31-43-13. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 46-1 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 46. NEW TECHNOLOGY 1. Electronic Flight Bag *** Systems (EFBs) *** 1) Class 3 EFBs C - - (O) May be inoperative provided alternate procedures are established and used. None required. Flight crew will establish alternate procedures to ensure required information normally provided by the EFB is available. These alternate procedures include using other means to acquire data through datalink, SATCOM or FliteFone, or over the VHF radio through either a FSS or Flight Watch. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Any function, program or document which operates normally may be used. D (continued) - 0 May be inoperative or missing provided procedures do not require its use. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 46-2 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 46. NEW TECHNOLOGY 1. Electronic Flight Bag *** Systems (EFBs) (continued) *** *** 2) Data Connectivity (Class 2) 3) Power Connection (Class 1 & 2) (continued) C - - (O) May be inoperative provided alternate procedures are established and used. None required. Flight crew will establish alternate procedures to ensure required information normally provided by the EFB is available. These alternate procedures include using other means to acquire data through datalink, SATCOM or FliteFone, or over the VHF radio through either a FSS or Flight Watch. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - 0 May be inoperative provided procedures do not require its use. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C - - (O) May be inoperative provided alternate procedures are established and used. None required. Flight crew will establish alternate procedures to ensure required information normally provided by the EFB is available. These alternate procedures include using other means to acquire data through datalink, SATCOM or FliteFone, or over the VHF radio through either a FSS or Flight Watch. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 46-3 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 46. NEW TECHNOLOGY 1. Electronic Flight Bag *** Systems (EFBs) (continued) *** 4) Mounting Device (Class 2) D - - May be inoperative provided procedures do not require its use. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C - 0 (M) (O) May be inoperative provided: a) Associated EFB and hardware is secured by an alternate means or removed from airplane, and b) Alternate procedures are established and used. Maintenance will ensure EFB and hardware is secured by an alternate means or removed from airplane, and procedures do not require its use. Flight crew will use other means to retrieve information provided by data connectivity, e.g., datalink to obtain current weather, uplink weather for graphical weather etc. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. D - 0 (M) May be inoperative provided: a) Associated EFB and hardware is secured by an alternate means or removed from airplane, and b) Procedures do not require its use. Maintenance will ensure EFB and hardware is secured by an alternate means or removed from airplane, and procedures do not require its use. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 49. AIRBORNE AUXILIARY POWER 1. Auxiliary Power Unit (APU) C 1 0 2. APU EGT Indicators (EICAS and Overhead) C 2 1 C 2 0 C 2 1 C 2 0 APU Tachometers (EICAS and Overhead) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 3. PAGE NUMBER: 49-1 MMEL REV. NO.: 8 (O) Except for ER operations, may be inoperative provided: a) Both Engine Driven generators are operative, and b) Standby Electrical System is operative. Except for ER operations, may be inoperative provided: a) APU is not operated, b) Both Engine Driven generators are operative, and c) Standby Electrical System is operative. Except for ER operations, may be inoperative provided : a) APU is not operated, b) Both Engine driven generators are operative, and c) Standby Electrical System is operative. None required. Flight crew will ensure: a) BOTH Engine Driven Generators are operative. AFM, Section 2, Normal Procedure, After Starting Engines. b) Standby Electrical System is operative. (Same as a). An Inoperative Placard will be placed on APU "MASTER" Switch and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on inoperative APU EGT indicator and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on inoperative APU EGT indicator and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on inoperative APU Tachometer indicator and will be noted on ADLS. None required. None required. An Inoperative Placard will be placed on inoperative APU Tachometer indicator and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 49-2 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 49. AIRBORNE AUXILIARY POWER 4. APU "READY" Light System C 1 0 May be inoperative provided APU is operated in accordance with AFM Limitations. None required. None required. An Inoperative Placard will be placed on APU "READY" Light and will be noted on ADLS. 5. APU Remote Oil Quantity/Servicing System C 1 0 May be inoperative provided oil is checked before every flight. None required. None required. An Inoperative Placard will be placed on APU Oil Quantity Indication System and will be noted on ADLS. 6. APU Oil Pressure *** Gauges D - 0 None required. None required. An Inoperative Placard will be placed on APU Oil Pressure Gauges and will be noted on ADLS. 7. APU Oil Temperature *** Gauges D - 0 None required. None required. An Inoperative Placard will be placed on APU Oil Temperature Gauges and will be noted on ADLS. 8. APU Fuel Pressure *** Gauges D - 0 None required. None required. An Inoperative Placard will be placed on APU Fuel Pressure Gauges and will be noted on ADLS. 9. C 1 0 None required. None required. An Inoperative Placard will be placed on APU Start Indicator Light and will be noted on ADLS. APU Start Indicator Light GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 49. AIRBORNE AUXILIARY POWER APU Air Load Control Valve MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 10. PAGE NUMBER: 49-3 MMEL REV. NO.: 8 C 1 0 (M) May be inoperative provided valve is verified in CLOSED position. Maintenance will ensure APU Air Load Valve is verified in a CLOSED position by Butterfly Plate Shaft Indicator. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. 11. APU External Fire Warning Alarm (Fire Warning Bell) C 1 0 May be inoperative provided APU operation is monitored in cockpit. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 12. APU Air Inlet Door System C 1 0 (M) Except for ER operations, may be inoperative provided: a) APU Air Inlet door is secured fully CLOSED, b) APU is not operated, c) Both Engine Driven Generators are operative, and d) Standby Electrical System is operative. Maintenance will ensure Air Intake Door is secured fully CLOSED by visually verifying door is CLOSED and pulling and collaring the APU door actuator circuit breaker. Flight crew may accomplish this task if properly qualified and authorized. None required. An Inoperative Placard will be placed on APU Control Panel and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 49-4 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 49. AIRBORNE AUXILIARY POWER 13. Bleed Air Augmentation Valve (GV, GV-SP) C 1 0 (O) May be inoperative provided: a) APU startng is not attempted above FL 350, and b) APU is operated in accordance with AFM Limitations. None required. Flight crew will ensure APU will be operated in accordance with AFM, Section 1, Limitations, APU Operation. Successful airstart only below 35,000 ft. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 14. Surge Control Valve (GV, GV-SP) C 1 0 (O) Except for ER operations, may be inoperative provided: a) APU is restricted to ground use only at pressure altitude of 8000 ft. or below, b) Both Engine Generators are operative, and c) Standby Electrical System is operative. None required. Flight crew will ensure APU is restricted to ground use only at P.A. < 8000 ft. An Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on ADLS. 15. Ignition System Channels (GV, GV-SP) C 2 1 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 16. EGT Thermocouple System (GV, GV-SP) C 2 1 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 49-5 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 49. AIRBORNE AUXILIARY POWER 17. Temperature Resistance Bulb (T2) C 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 18. Inlet Pressure Transmitter (P2) (GV, GV-SP) C 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 19. RPM Speed Sensor Channels (GV, GV-SP) C 2 1 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 20. APU Hour Meter C 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 21. Oil Temperature (GV, GV-SP) C 1 0 None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. May be inoperative provided airplane is operated in accordance with AFM Limitations. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 49. AIRBORNE AUXILIARY POWER Deprime Solenoid (GV, GV-SP) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 22. PAGE NUMBER: 49-6 MMEL REV. NO.: 8 C 1 0 (M) May be inoperative provided airplane is operated in accordance with AFM Limitations. Maintenance will verify Deprime None required. Solenoid is inoperative by reference to MDAU. Maintenance will visually check APU oil level and perform APU start, run and shutdown per AFM procedures. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. 23. Oil Heater (GV, GV-SP) 24. APU Start/Engine *** Cowl Interrupt System C 1 0 D 1 0 May be inoperative provided airplane is operated in accordance with AFM Limitations. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 2. Cargo Door Operating *** System NUMBER REQ’D FOR DISPATCH PROCEDURE MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE C 1 0 May be inoperative provided a crewmember verifies by visual inspection before each departure that the associated door is CLOSED and LOCKED. None required. Flight crew will visually inspect Door(s) to ensure they are CLOSED and LOCKED prior to departure. AFM, Section 2, Normal Procedures, After Starting Engines. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. C 1 0 May be inoperative provided a crewmember verifies by visual inspection before each departure that the associated door is CLOSED and LOCKED. Maintenance will OPEN and CLOSE doors for each flight from outside airplane. Flight crew will ensure by visual inspection associated Door is CLOSED and LOCKED before each departure. In addition, flight crew will ensure door is OPENED and CLOSED by maintenance ground crew. An Inoperative Placard will be placed Externally and Internally near door operating handles and will be noted on ADLS. Flight crew will ensure by visual inspection associated Door is CLOSED and LOCKED before each departure. In addition, flight crew will ensure Door is OPENED and CLOSED by maintenance ground crew. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Flight crew may accomplish this task if properly qualified and authorized. 3. Cargo Door Warning *** Light System MMEL DATE: 11/07/2014 4. MMEL REMARKS OR EXCEPTIONS 52. DOORS Door Warning Light System MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 52-1 MMEL REV. NO.: 8 C 1 0 May be inoperative provided a crewmember verifies by visual inspection before each departure that the associated door is CLOSED and LOCKED. Maintenance will OPEN and CLOSE doors for each flight from outside airplane. Flight crew may accomplish this task if properly qualified and authorized. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 52-2 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 52. DOORS 4. Door Seal Pressure *** Indicator D 1 0 5. Main Entry Door Normal Operating System C 1 0 6. Main Entry Door Acoustic Curtain/ Door System D - - (O) May be inoperative provided: a) Alternate system is operative, and b) Main door is not CLOSED manually. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. Flight crew will select the AUX Hydraulic Pump ON, manually OPEN the door control valve, CLOSE and LOCK the main door, and manually CLOSE the door control valve. Refer to AOM Volume 3 Handling and Servicing Procedures, Section 9 item 09-03-20. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 52. DOORS Lavatory Door MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 7. PAGE NUMBER: 52-3 MMEL REV. NO.: 8 D - - May be inoperative provided the affected door is secured OPEN or CLOSED for taxi, takeoff and landing. None required. None required. An Inoperative Placard will be placed on the Lavatory Door and will be noted on ADLS. NOTE: Includes pop-up panels, latches, locks and handles. 8. Baggage Door Warning System C 1 0 May be inoperative provided a crewmember verifies by visual inspection before each departure that the baggage door is CLOSED and LOCKED. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 9. Main Entry Door Warning System C 1 0 May be inoperative provided a crewmember verifies by visual inspection before each departure that the Main Entry Door is CLOSED and LOCKED. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Internal Baggage Door Warning System (GV, GV-SP) C 1 0 (O) May be inoperative provided: a) Door is confirmed to be CLOSED and LOCKED by a crewmember after each use, and b) Door is placarded “DO NOT ENTER” above 40,000 ft. None required. The flight crew advises the passengers when the airplane is at or above 40,000 ft and that access to the baggage compartment is not allowed. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 10. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 52-4 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 52. DOORS 11. Internal Pocket Doors D - - May be inoperative provided the affected None required. door is secured OPEN for taxi, takeoff and landing. NOTE: Includes pop-up panels, latches, locks and handles. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 12. Cabin Over Wing Exit Window Warning System D 1 0 May be inoperative provided a crewmember verifies by visual inspection before each departure that the cabin exit window internal and external locking (T) handles in the over wing access panels are engaged in their LOCKED position. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 71. POWERPLANT EPA Tank Ejector Pump MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 71-1 MMEL REV. NO.: 8 D 2 0 (M) May be inoperative provided maintenance procedures are established to drain tank: a) Before the first flight of each day, b) After three normal shutdowns, and c) After two false (wet) starts. Maintenance will perform procedures None required. in accordance with AMM Chapter 71-71-02. If maintenance is not available, flight crew may perform the procedure. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 73. ENGINE FUEL & CONTROL 2. MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 73-1 MMEL REV. NO.: 8 Fuel Flow Indication Systems 1) EICAS C 2 1 May be inoperative provided: a) Associated EPR, LP and HP indicating systems are operative, and b) Fuel Quantity indicating systems are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 2) RFMU (GV) / MCDU (GV-SP)/ (GIV-X) C 2 1 May be inoperative provided: a) Associated EPR, LP and HP indicating systems are operative, and b) Fuel Quantity indicating systems are operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Fuel Low Pressure Warning Systems (EICAS) C 2 1 May be inoperative provided: a) Associated Fuel Boost Pumps are operative, and b) Airplane is operated at or below FL 250. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH A 2 0 (M) (O) Airplane may be dispatched with Blue “Engine Maintenance STD (###)” and/or “Engine Maintenance LTD” messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), chapter 5 or BR 710C4 Time Limits Manual (GV-SP), chapter 5 (no extensions are authorized), and b) FADEC faults are reviewed by flight crew before each takeoff. NOTE: GV, GV-SP Blue “Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue “Engine Maintenance LTD” messages required maintenance action within 500 hours. PROCEDURE Maintenance will ensure repairs are made in accordance with times (hours) established by the BR710 Type Certificate Data Sheet. The times (hours) established for Engine Maintenance LTD (Long Term Dispatch) message is 500 engine hours. The times (hours) established for Engine Maintenance ### STD (Short Term Dispatch where ### is the number of hours remaining) is 150 engine hours when the fault is first logged. The hours remaining to affect the repair are automatically decreased by the system as engine time is accumulated. When the time remaining is zero, the fault automatically becomes a DND (Do Not Dispatch) fault. Flight crew may accomplish this task if properly qualified and authorized. (continued) MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 73. ENGINE FUEL & CONTROL Engine FADEC Systems (GV, GV-SP) MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 3. PAGE NUMBER: 73-2 MMEL REV. NO.: 8 Flight crew will review the FADEC faults prior to each takeoff. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 73. ENGINE FUEL & CONTROL 3. PAGE NUMBER: 73-3 MMEL REV. NO.: 8 Engine FADEC Systems (continued) Engine FADEC System (GIV-X) A 2 0 (M) (O) Airplane may be dispatched with Blue “Engine Maintenance STD (###)” and/or “Engine Maintenance LTD” messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the Tay 611-8C Time Limits Manual, chapter 5 (no extensions are authorized), and b) FADEC faults are reviewed by flight crew before each takeoff. Maintenance will ensure repairs are made in accordance with times (hours) established by the Tay 6118C Time Limits Manual, chapter 5. The times (hours) established for Engine Maintenance LTD (Long Term Dispatch) message is 500 engine hours. The times (hours) established for Engine Maintenance ### STD (Short Term Dispatch where ### is the number of hours remaining) is 150 engine hours when NOTE: GIV-X “Blue Engine Maintenance the fault is first logged. The hours STD” (###) message require maintenance remaining to effect the repair are action within 150 hours and “Blue Engine automatically decreased by the Maintenance LTD” messages required system as engine time is maintenance action within 500 hours. accumulated. When the time remaining is zero, the fault automatically becomes a DND (Do Not Dispatch) fault. Flight crew may accomplish this task if properly qualified and authorized. Flight crew will review FADEC faults prior to each takeoff. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 74. IGNITION 1. PAGE NUMBER: 74-1 MMEL REV. NO.: 8 Ignition Systems 1) 2) No. 1 Igniters No. 2 Igniters A 2 1 May be inoperative provided: a) Both No. 2 Igniters are operative, b) Takeoff runway does not have standing water, slush, or snow, and c) Repairs are made within 150 flight hours. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. A 2 0 May be inoperative provided: a) Both No. 2 Igniters are operative, b) Takeoff runway does not have standing water, slush, or snow, and c) Repairs are made within 10 flight days. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. A 2 1 May be inoperative provided: a) Both No. 1 Igniters are operative, b) Takeoff runway does not have standing water, slush, or snow, and c) Repairs are made within 150 flight hours. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. A 2 0 May be inoperative provided: a) Both No. 1 Igniters are operative, b) Takeoff runway does not have standing water, slush, or snow, and c) Repairs are made within 10 flight days. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 74. IGNITION Ignition ON Indicator Systems MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 2. PAGE NUMBER: 74-2 MMEL REV. NO.: 8 C 2 0 (M) May be inoperative provided both airstart systems are verified to be operative before each flight. To check the igniters: Pull the IGN None required. L/R #2 breaker. Select L & R airstart ignition switches ON. Verify igniters firing at the engines. Reset breakers. Pull IGN L/R #1 breaker. Select L & R airstart ignition switches ON. Verify igniters firing at the engines. Reset breaker when complete. An Inoperative Placard will be placed near affected Ignition "ON" Light and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 77. ENGINE INDICATING HP Tachometer Indications EICAS MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 77-1 MMEL REV. NO.: 8 C 2 1 May be inoperative on either engine None required. provided associated LP, EPR and Fuel Flow Indicating Systems (EICAS or Standby) are operative for affected engine. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Standby HP Indication may also be inoperative on both engines. 2. Engine Vibration Monitor Systems Sensors 1) Primary Sensors C 2 0 May be inoperative provided associated secondary sensor system is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 2) Secondary Sensors C 2 0 May be inoperative provided associated primary sensor system is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 77. ENGINE INDICATING 3. PAGE NUMBER: 77-2 MMEL REV. NO.: 8 Standby Engine Instruments Indicating System (RFMU) (GV) C 1 4. Standby Engine Instruments on Multifunction Control Display (MCDU) (GV-SP, GIV-X) C 1 5. Engine Vibration Monitoring System B 1 0 May be inoperative provided: a) Associated EICAS indication is operative, and b) All channels of both DAUs are operative. None required. None required. 0 May be inoperative provided associated EICAS indication is operative. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 0 May be inoperative provided: a) Both Ice Detection Systems are operative, b) Operations are not conducted in known or forecast icing conditions, and c) Crew reviews the Abnormal Procedures for engine vibration before each takeoff. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: Individual standby indications may be inoperative provided associated EICAS indication is operative. See individual indications for other authorized configurations. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 78. ENGINE EXHAUST Thrust Reversers MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 78-1 MMEL REV. NO.: 8 C 2 0 (M) May be inoperative provided: a) Affected Thrust Reverser is deactivated, stowed and LOCKED in forward thrust position, and b) Airplane is operated in accordance with AFM Limitations and Procedures. May be inoperative provided: a) Affected Thrust Reverser is deactivated, stowed, and LOCKED in forward thrust position. Refer to AMM Chapter 78-30-00. b) Airplane is operated IAW AFM Limitations and Procedures. NOTE: AFM Landing Distances are not impacted for dry runway, refer to AFM 01-78-10, but is affected in wet/contaminated runway conditions, refer to AOM 13-03-00. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 79-1 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 79. ENGINE OIL 1. Low Oil Pressure Warning System C 2 1 2. Engine Oil Replenishment System D 1 0 3. Impending Oil Filter Bypass Indications A 2 1 May be inoperative provided oil pressure indication for both engines are operative. (M) May be inoperative provided: a) Associated oil filter bypass pop up indicator is verified in normal (recessed) position before each engine start, b) The oil filter is changed every flight day or every 15 flight hours, whichever occurs first, c) The Magnetic Chip Detectors are checked and verified to be free of all debris, d) Procedures are in place to ensure all other DND (Do Not Dispatch) messages are addressed before dispatch, and e) Repairs are made within three (3) flight days. NOTE: An amber “Engine Maintenance Required” message will still be displayed on the Crew Alerting System. Dispatch is allowed with this message displayed after complying with the required (M) procedure. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. Maintenance will ensure: a) Associated oil filter bypass pop up indicator is verified in normal (recessed) position before each engine start b) Affected engine’s oil filter is replaced per AMM, c) Fault is confirmed to be on the indication system, and d) Procedures are in place to ensure all other DND (Do Not Dispatch) messages are addressed before dispatch. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. PAGE NUMBER: 79-2 MMEL REV. NO.: 8 MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 79. ENGINE OIL 4. Oil Quantity Indication Systems (EICAS / Ground Service Control Panel) C 2 0 May be inoperative provided the engine oil quantity is verified on the engine oil quantity gauge before each engine start. None required. None required. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. 5. Oil Filter Pressure Switch Fault Indications C 2 0 (M) May be inoperative provided: a) Associated oil filter bypass pop up indicator is verified in normal (recessed) position before each engine start, b) Oil filter fault is not displayed in MDAU (GV) or CMC (GV-SP, GIV-X), c) Fault is confirmed to be on the indication system, and d) Procedures are in place to ensure all other DND (Do Not Dispatch) messages are addressed before dispatch. Maintenance will ensure associated None required. oil filter bypass pop up indicator is verified in normal (recessed) position before each engine start. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. NOTE: An amber “Engine Maintenance Required” message will still be displayed on the Crew Alerting System. Dispatch is allowed with this message displayed after complying with the required (M) procedure. Flight crew may accomplish this task if properly qualified and authorized. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. 2. Auto Start System MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 80. STARTING Engine Starting Systems MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 1. PAGE NUMBER: 80-1 MMEL REV. NO.: 8 C C 2 2 0 0 (M) (O) May be inoperative provided: a) Airstart Ignition System is operative, b) Start Valve has not failed in OPEN position, c) Start Valve is manually OPENED and CLOSED for engine starting, d) Airstart Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached selfsustaining speed, and e) Engine start is accomplished in accordance with AFM Engine Start Valve Fails To Open Procedure. Maintenance will ensure: a) Start Valve has not failed in OPEN position, b) Start Valve is manually OPENED and CLOSED for engine starting, c) Airstart (Continuous) Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached self sustaining speed, and d) The Airstart Ignition System is operative. May be inoperative provided: a) Alternate start system is operative, and b) AFM procedures for alternate engine start are used to start engines. None required. The flight crew may perform this task if properly qualified and authorized. Flight crew will ensure: a) Start Valve has not failed in OPEN position. b) Start Valve is manually OPENED and CLOSED for engine starting. c) Airstart (Continuous) Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached selfsustaining speed. d) Engine Start is accomplished in accordance with AFM, Section 3, Abnormal Procedures, Engine Starting System. An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS. None required. An Inoperative Placard will be displayed in a prominent position to be seen by the flight crew and will be noted on the ADLS. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. 5. MAINTENANCE 3. MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 NUMBER REQ’D FOR DISPATCH PROCEDURE 6. OPERATIONAL 7. PLACARDING PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 80. STARTING Start Valve Position Indication MOP REV. NO.: 8 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 3. PAGE NUMBER: 80-2 MMEL REV. NO.: 8 C C 2 2 0 0 (M) May be inoperative provided: a) Start Valve has not failed in OPEN position as verified by visual means through an access panel, b) Ignition ON indication is operative during engine start, and c) Start Valve is verified CLOSED following engine start by visual means. Maintenance will ensure: a) Start Valve has not failed in OPEN position, b) Airstart ignition is operative, c) Start Valve is manually OPENED and CLOSED for engine starting. (M) (O) May be inoperative provided: a) Airstart Ignition System is operative, b) Start Valve has not failed in OPEN position, c) Start Valve is manually OPENED and CLOSED for engine starting, d) Airstart Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached selfsustaining speed, and e) Engine start is accomplished in accordance with AFM Engine Start Valve Fails To Open Procedure. Maintenance will ensure: a) Start Valve has not failed in OPEN position, b) Start Valve is manually OPENED and CLOSED for engine starting, c) Airstart (Continuous) Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached self sustaining speed, and d) The Airstart Ignition System is operative. None required. An Inoperative Placard will be placed on Start Valve Position Indicator and will be noted on ADLS. Flight crew will comply with QRH procedures for Manually Overriding Starter Air Valve OM-09-03-40 found under Alternate Normal Procedures tab. An Inoperative Placard will be placed on Start Valve Position Indicator and will be noted on ADLS. The flight crew may perform this task if properly qualified and authorized. The flight crew may perform this task if properly qualified and authorized. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL 1. MOP REV. NO.: 8 MMEL DATE: 11/07/2014 MOP DATE: 11/07/2014 6. OPERATIONAL 7. PLACARDING 2. NUMBER INSTALLED SYSTEM & SEQUENCE NUMBERS 5. MAINTENANCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURE PROCEDURE PROCEDURE 4. MMEL REMARKS OR EXCEPTIONS 80. STARTING 4. Start Valve *** Position Indicator Lights PAGE NUMBER: 80-3 MMEL REV. NO.: 8 C 2 0 (M) May be inoperative provided: a) Start Valve has not failed in OPEN position as verified by visual means through an access panel, b) Start Valve is manually OPENED and CLOSED for engine starting in accordance with AFM Start Valve Failure procedures, and c) Airstart Ignition, Engine Selector and Start switches are switched to the OFF position when engine has reached self-sustaining speed. Maintenance will ensure a) Start Valve has not failed in OPEN position, b) Start Valve is manually OPENED and CLOSED for engine starting, c) Airstart (Continuous) Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached self sustaining speed, and d) The Airstart Ignition System is operative. The flight crew may perform this task if properly qualified and authorized. None Required. An Inoperative Placard will be placed on Start Valve Position Indicator Lights and will be noted on ADLS. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 PAGE NO: 2-1 SECTION TWO CREW ALERTING SYSTEM (CAS) MESSAGE RELIEF GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 PAGE NO: 2-2 STATEMENT PAGE 1. Section Two of the MMEL will list only Crew Alerting system (CAS) messages meeting the following requirements: a. Equipment failure indications(s) that can be used to determine the airworthiness status of the airplane. b. Messages that the crew can act upon with simple troubleshooting procedures without the assistance of a mechanic, and for which the crew has been trained. c. Messages using the new self-diagnostic technology (virtual) actions for which the crew has been trained. 2. CAS message relief items not meeting these requirements will be listed in Section One of the MMEL. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message A/P TRIM PWR FAIL (O) Airplane may be dispatched with one (1) elevator trim servo inoperative provided the inoperative trim servo circuit breaker(s) is pulled and collared. B (O) Airplane may be dispatched provided affected A/T system is confirmed disengaged. B (O) Airplane may be dispatched provided affected A/T system is confirmed disengaged. Flight crew will confirm affected A/T system is disengaged. C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. (Blue – Advisory) (GV-SP/GIV-X) ACS Default Mode, L-R Operational Procedures B (Blue – Advisory) A/T 1-2 TQA Power Fail 2-3 3. Limitations and/or Procedures (Blue – Advisory) (GV) A/T 1-2 FAIL PAGE NO: Flight crew will ensure inoperative A/P SERVO #1: POP, D-4 or A/P SERVO #2: CPOP, D-4 servo circuit breaker is pulled and collared. Flight crew will confirm affected A/T system is disengaged. (Blue – Advisory) (GV-SP/GIV-X) ACS DEFLT MODE, L-R (Blue – Advisory) (GV) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message ACS Fail, L-R 2. PAGE NO: 2-4 3. Limitations and/or Procedures Operational Procedures B Except for ER operations, airplane may be dispatched in the pressurized configuration with a single pack inoperative provided: a) Inoperative ECS Pack is selected OFF, b) Bleed Air Isolation Valve is CLOSED and OPERATIVE, c) Right Main TRU is operative, d) Airplane is operated in accordance with AFM Limitations, e) Airplane is operated at or below FL410, and f) Autothrottles must be operative and engaged at or above FL400. None required. B Except for ER operations, airplane may be dispatched in the unpressurized configuration with both packs inoperative provided the outflow valve is operative. None required. (Amber – Caution) (GV-SP/GIV-X) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message ACS FAIL, L-R 2. PAGE NO: 2-5 3. Limitations and/or Procedures Operational Procedures B Except for ER operations, airplane may be dispatched in the pressurized configuration with a single pack inoperative provided: a) Inoperative ECS Pack is selected OFF, b) Bleed Air Isolation Valve is CLOSED and OPERATIVE, c) Right Main TRU is operative, d) Airplane is operated in accordance with AFM Limitations, e) Airplane is operated at or below FL410, and f) Autothrottles must be operative and engaged at or above FL400. None required. B Except for ER operations, airplane may be dispatched in the unpressurized configuration with both packs inoperative provided the outflow valve is operative. None required. (Amber – Caution) (GV) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message ACS Maintenance, L-R (Blue – Advisory) (GV-SP/GIV-X) Operational Procedures C (O) Except for ER operations, airplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, and d) Autopilot is operative. Flight crew will ensure: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, and d) Autopilot is operative. C (O) Except for ER operations, airplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, and d) Autopilot is operative. Flight crew will ensure: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, and d) Autopilot is operative. Airplane may be dispatched provided system is not required by 14 CFR. None required. (Blue – Advisory) (GV) ADF 1-2 Fail 2-6 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) ACS MAINT REQD, L-R PAGE NO: B GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message ADM1-3 Probe Heat Fail (Blue – Advisory) (GV-SP) 2-7 3. Limitations and/or Procedures Operational Procedures A (O) Except for ER operations, airplane may be dispatched with one (1) probe heater inoperative provided: a) Airplane is not operated in visible moisture or known or forecast icing conditions, b) Flight crew select ADS sources that are different and not associated with failed pitot heater element, and c) Repairs are made within two (2) flight days. Flight crew will select ADS sources that are different and not associated with failed pitot heater element and transfer transponder to an operable ADM. A (O) Except for ER operations, airplane may be dispatched with one (1) probe heater inoperative provided: a) Airplane is not operated in visible moisture or known or forecast icing conditions, b) Flight crew select ADS sources that are different and not associated with failed pitot heater element, and c) Repairs are made within two (2) flight days. Flight crew will select ADS sources that are different and not associated with failed pitot heater element. (Blue – Advisory) (GV-SP) ADM2 Stby Probe Heat Fail PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message ADS 1-2 Probe Heat Fail (Blue – Advisory) (GIV-X) (O) 2-8 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched with one (1) probe heater inoperative provided: a) Airplane is not operated in visible moisture or known or forecast icing conditions, b) Flight crew select ADS sources that are different and not associated with failed pitot heater element, and c) Repairs are made within two (2) flight days. Operational Procedures Flight crew will select ADS sources that are different and not associated with failed pitot heater element. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message ADS 1-2-3 Fail (Blue – Advisory) (GV-SP/GIV-X) (O) 2-9 3. Limitations and/or Procedures B PAGE NO: Operational Procedures Airplane may be dispatched with a single Flight crew will pull and collar air data system inoperative provided: ADM #1: POP B-8, ADM #2: a) Manual Pressurization Control System CPOP B-8 and ADM #3: POP Bis operative, 9 circuit breakers associated with b) Cabin Altitude and Differential the ADS failure. Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Airplane is operated in accordance with AFM Limitations, f) ADM #1: POP B-8, ADM #2: CPOP B8 and ADM #3: POP B-9 circuit breakers associated with ADS failure is pulled and collared, and g) Flight crew selects operative and different ADS sources prior to departure. NOTE 1: Two systems are required for operation in RVSM airspace. NOTE 2: Transponder and Flight Director / Autopilot must use same ADC data for RVSM. NOTE 3: For ADS 1 Fail, expect the L Engine Backup Air Data advisory and associated Engine Maintenance message to post. NOTE 4: For ADS 2 Fail, expect the R Engine Backup Air Data advisory and associated Engine Maintenance message to post. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message ADS 3 Stby Probe Heat Fail A (O) 2 - 10 3. Limitations and/or Procedures (Blue – Advisory) (GIV-X) PAGE NO: Except for ER operations, airplane may be dispatched with one (1) probe heater inoperative provided: a) Airplane is not operated in visible moisture or known or forecast icing conditions, b) Flight crew selects ADS sources that are different and not associated with failed pitot heater element, and c) Repairs are made within two (2) flight days. Operational Procedures Flight crew will select ADS sources that are different and not associated with failed pitot heater element. NOTE: Standby instruments and ADS 3 may be unreliable. ADS-B Fail (Blue – Advisory) (GV-SP/GIV-X) A Airplane may be dispatched provided: a) Operations do not require its use, and b) Repairs are made before completion of next heavy maintenance visit. None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Aft Cabin Temp Fan Fail (Blue – Advisory) (GV-SP/GIV-X) (O) 2 - 11 3. Limitations and/or Procedures C PAGE NO: Airplane may be dispatched provided: a) None of the following CAS messages are also posted: Forward Cabin Temp Fan Fail; Cockpit Temp Fan Fail; b) Aft Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) AFT CABIN SENSOR FAN, LEER E9, is pulled and collared, and e) Flight crew monitor aft cabin temperature and aft cabin duct temperature. Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: Forward Cabin Temp Fan Fail; Cockpit Temp Fan Fail, b) Aft Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) AFT CABIN SENSOR FAN circuit breaker: LEER E-9 is pulled and collared, and e) Aft cabin temperature and aft cabin duct temperature are monitored. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message AFT CABIN TMP FAN FL C AGM 1-2-3-4 DMU Charts Fail (Blue – Advisory) (GV-SP/GIV-X) C (O) 2 - 12 3. Limitations and/or Procedures (Blue – Advisory) (GV) PAGE NO: Airplane may be dispatched provided: a) None of the following CAS messages are also posted: Forward Cabin Temp Fan Fail; Cockpit Temp Fan Fail; b) Aft Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) AFT CABIN SENSOR FAN, LEER E9, is pulled and collared, and e) Flight crew monitor aft cabin temperature and aft cabin duct temperature. Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: Forward Cabin Temp Fan Fail; Cockpit Temp Fan Fail, b) Aft Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) AFT CABIN SENSOR FAN circuit breaker: LEER E-9 is pulled and collared, and e) Aft cabin temperature and aft cabin duct temperature are monitored. Airplane may be dispatched provided: None required. a) Current aeronautical charts are carried onboard the airplane and available to the flight crew, and b) Airplane is operated in accordance with AFM Limitations. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message AGM 1-2-3-4 Fail B AIU 1-2 FAIL (Blue – Advisory) (GV) A (O) 2 - 13 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) PAGE NO: Operational Procedures Airplane may be dispatched with one AGM Flight crew will ensure: inoperative provided: a) The inoperative AGM is a) The inoperative AGM is electronically electronically switched to the switched to the AGM 3 position number 3 position resulting resulting in DU3 red Xing, in DU3 red Xing, b) DU3 is dimmed to eliminate the Red X, b) DU 3 is dimmed to eliminate and the Red X, c) Crew actions for subsequent failures c) Crew actions for are established. subsequent failures are established, and d) Crew will discuss the alternate procedures for sharing displays including if a display fails during any phase of flight especially takeoff, approach, landing and go-around. Airplane may be dispatched with one AIU inoperative provided: a) Operations do not require use of HF radio, and b) Repairs are made within two (2) flight days. None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Alternate Pump Fail, L-R (Amber – Caution) (GIV-X) 2 - 14 3. Limitations and/or Procedures Operational Procedures B (O) Except for ER operations, airplane may be dispatched with a single pump inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, d) Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, and e) Airplane is operated in accordance with AFM Limitations. Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative, b) BOTH Fuel Low Quantity Warning Systems are operative, and c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure. B (O) Except for ER operations, airplane may be dispatched with a single pump inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, d) Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, and e) Airplane is operated in accordance with AFM Limitations. Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative, b) BOTH Fuel Low Quantity Warning Systems are operative, and c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure (Amber – Caution) (GV-SP) Alt FuelPump Fail, L-R PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message ALT PUMP FAIL, L-R (Amber – Caution) (GV) (O) 2 - 15 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched with a single pump inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, d) Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, and e) Airplane is operated in accordance with AFM Limitations. Operational Procedures Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative, b) BOTH Fuel Low Quantity Warning Systems are operative, and c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Antiskid Fail (Amber – Caution) (GV-SP/GIV-X) (O) 2 - 16 3. Limitations and/or Procedures B PAGE NO: Airplane may be dispatched provided: a) ANTI-SKID is selected “OFF”, b) Anti-skid off braking procedures, AFM Section 3, Abnormal Procedures, AntiSkid Failure are followed, c) No WOW Power Faults exist, d) If Auto mode of the AUX Hydraulic Pump is inoperative, AUX pump is selected ON for takeoff and landing, and e) Airplane is operated in accordance with AFM Limitations. NOTE: Anti-Skid inoperative AFM performance penalties must be applied. Refer to AFM, Section 5, Performance, Reference Accelerate-Stop Distance. Operational Procedures Flight crew will ensure airplane is operated in accordance with AFM, Limitations. Flight crew will select ANTI-SKID “OFF” and follow Anti-Skid Off Braking Procedures. AFM, Section 3, Abnormal Procedures, Anti-Skid Failure. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message ANTISKID FAIL (Amber – Caution) (GV) (O) 2 - 17 3. Limitations and/or Procedures B PAGE NO: Airplane may be dispatched provided: a) ANTI-SKID is selected “OFF”, b) Anti-skid off braking procedures, AFM Section 3, Abnormal Procedures, AntiSkid Failure are followed, c) No WOW Power Faults exist, d) If Auto mode of the AUX Hydraulic Pump is inoperative, AUX pump is selected ON for takeoff and landing, and e) Airplane is operated in accordance with AFM Limitations. NOTE: Anti-Skid inoperative AFM performance penalties must be applied. Refer to AFM, Section 5, Performance, Reference Accelerate-Stop Distance. Operational Procedures Flight crew will ensure airplane is operated in accordance with AFM, Limitations. Flight crew will select ANTI-SKID “OFF” and follow Anti-Skid Off Braking Procedures. AFM, Section 3, Abnormal Procedures, Anti-Skid Failure. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message AP 1-2 Fail B (O) 2 - 18 3. Limitations and/or Procedures (Amber – Caution) (GV-SP/GIV-X) PAGE NO: Except for ER operations or where en route operations or approach minimums require its use, Airplane may be dispatched with one (1) Autopilot inoperative provided the airplane is operated in accordance with AFM Limitations in the event operative FGC fails and Yaw Damper is inoperative. Operational Procedures Flight crew will operate the airplane in accordance AFM limitations in the event the operative FGC fails and the Yaw Damper is inoperative. NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations. AP 1-2 Power Fail (Blue – Advisory) (GV-SP/GIV-X) B (O) Except for ER operations or where en route operations or approach minimums require its use, Airplane may be dispatched with one (1) inoperative provided airplane is operated in accordance with AFM Limitations in the event operative FGC fails and Yaw Damper is inoperative. NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations. Flight crew will operate airplane in accordance with AFM limitations in the event the FGC fails and the Yaw Damper is inoperative. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message AP/Trim Fail B APM 1-2-3-4 Fail (Blue – Advisory) (GV-SP/GIV-X) B (O) 2 - 19 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) PAGE NO: Operational Procedures Airplane may be dispatched with one (1) elevator trim servo inoperative provided the inoperative trim servo circuit breaker(s) is pulled and collared. G550: Flight crew will ensure inoperative PITCH TRIM SERVO #1: POP, E-2 or PITCH TRIM SERVO #2: CPOP, E-1 servo circuit breaker is pulled and collared. G450: Flight crew will ensure inoperative PITCH TRIM SERVO #1: POP, E-2 or PITCH TRIM SERVO #2: CPOP, E-1 servo circuit breaker is pulled and collared. Airplane may be dispatched with one (1) APM inoperative. None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message APU Fail (Amber – Caution) (GV-SP/GIV-X) Operational Procedures B (O) Except for ER operations, airplane may be dispatched provided: a) Both Engine Driven generators are operative, and b) Standby Electrical System is operative. Flight crew will ensure: a) BOTH Engine Driven Generators are operative. b) Standby Electrical system is operative. B (O) Except for ER operations, airplane may be dispatched provided: a) Both Engine Driven generators are operative, and b) Standby Electrical System is operative. Flight crew will ensure: a) BOTH Engine Driven Generators are operativ b) Standby Electrical system is operative. B (O) Except for ER operations, airplane may be dispatched provided: a) APU is considered inoperative, b) Both engine driven generators are operative, c) Standby electrical system is operative, and d) APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. Flight crew will pull and collar APU CONT #1 and APU CONT #2 circuit breakers. Flight crew will ensure: a) Both Engine Generators are operative. b) Standby Electrical Power System is operative. (Amber – Caution) (GV) APU Fire Bottle Discharge 2 - 20 3. Limitations and/or Procedures (Amber – Caution) (GV-SP/GIV-X) APU FAIL PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message APU Fire Detector Fail (Amber – Caution) (GV) 2 - 21 3. Limitations and/or Procedures Operational Procedures B (O) Except for ER operations, airplane may be dispatched provided: a) APU is not used, and b) APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. Flight crew will ensure APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. B (O) Except for ER operations, airplane may be dispatched provided: a) APU is not used, and b) APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. Flight crew will ensure APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. (Amber – Caution) (GV-SP/GIV-X) APU FIRE DET FAIL PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message APU GCU Fail (Blue – Advisory) (GV) 2 - 22 3. Limitations and/or Procedures Operational Procedures A (O) Except for ER operations, airplane may be dispatched provided: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. Flight crew will ensure: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and c) Standby Electrical System is operative. A (O) Except for ER operations, airplane may be dispatched provided: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. Flight crew will ensure: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and c) Standby Electrical System is operative. (Blue – Advisory) (GV-SP/GIV-X) APU GCU FAIL PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message APU Generator Fail A APU Generator Maint Reqd (Blue – Advisory) (GV-SP/GIV-X) C (O) 2 - 23 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) PAGE NO: Operational Procedures Except for ER operations, airplane may be dispatched provided: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS, and c) Standby Electrical System is operative. Flight crew will ensure: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and c) Standby Electrical System is operative. Airplane may be dispatched. None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message APU GEN FAIL APU GEN MAINT REQD Operational Procedures Except for ER operations, airplane may be dispatched provided: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS, and c) Standby Electrical System is operative. Flight crew will ensure: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and c) Standby Electrical System is operative. C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. (Blue – Advisory) (GV) (O) 2 - 24 3. Limitations and/or Procedures A PAGE NO: (Blue – Advisory) (GV) APU Maintenance Required (Blue – Advisory) (GV-SP/GIV-X) APU MAINT REQD (Blue – Advisory) (GV) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message APU Shutoff Valve Fail B ATC 1-2 Fail (Blue – Advisory) (GV-SP/GIV-X) C (O) 2 - 25 3. Limitations and/or Procedures (Amber – Caution) (GV-SP/GIV-X) PAGE NO: Operational Procedures Except for ER operations, may be inoperative provided: a) Both Engine Driven generators are operative, b) Standby Electrical System is operative, and c) APU is not used. Flight crew will ensure: a) BOTH Engine Driven Generators are operative. b) Standby Electrical system is operative. Airplane may be dispatched with any in excess of those required by 14 CFR inoperative. None required. NOTE 1: Flight Director, Autopilot, and Transponder must use the same Air Data source for flight into RVSM airspace. NOTE 2: Transponder and altitude reporting capability must be operative for flight into RVSM airspace. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message BAROSET 1 Fail (Blue – Advisory) (GV-SP/GIV-X) (O) 2 - 26 3. Limitations and/or Procedures C PAGE NO: Airplane may be dispatched provided: a) None of the following CAS messages are also posted: 1. ADS 2 Fail 2. ADS 3 Fail 3. BAROSET 2 Fail 4. BAROSET 3 Fail b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and g) Airplane is operated in accordance with AFM Limitations. Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: 1. ADS 2 Fail 2. ADS 3 Fail 3. BAROSET 2 FAIL 4. BAROSET 3 FAIL b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and NOTE 1: Two systems are required for g) Airplane is operated in operation in RVSM airspace. accordance with AFM NOTE 2: Transponder and Flight Limitations. Director/Autopilot must use same ADC data for RVSM. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message BAROSET 2 Fail (Blue – Advisory) (GV-SP/GIV-X) (O) 2 - 27 3. Limitations and/or Procedures C PAGE NO: Airplane may be dispatched provided: a) None of the following CAS messages are also posted: 1. ADS 1 Fail 2. ADS 3 Fail 3. BAROSET 1 Fail 4. BAROSET 3 Fail b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and g) Airplane is operated in accordance with AFM Limitations. Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: 1. ADS 1 Fail 2. ADS 3 Fail 3. BAROSET 1 FAIL 4. BAROSET 3 FAIL b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and NOTE 1: Two systems are required for g) Airplane is operated in operation in RVSM airspace. accordance with AFM NOTE 2: Transponder and Flight Limitations. Director/Autopilot must use same ADC data for RVSM. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message BAROSET 3 Fail (Blue – Advisory) (GV-SP/GIV-X) (O) 2 - 28 3. Limitations and/or Procedures C PAGE NO: Airplane may be dispatched provided: a) None of the following CAS messages are also posted: 1. ADS 1 Fail 2. ADS 2 Fail 3. BAROSET 1 Fail 4. BAROSET 2 Fail b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and g) Airplane is operated in accordance with AFM Limitations. Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: 1. ADS 1 Fail 2. ADS 2 Fail 3. BAROSET 1 FAIL 4. BAROSET 2 FAIL b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and NOTE 1: Two systems are required for g) Airplane is operated in operation in RVSM airspace. accordance with AFM NOTE 2: Transponder and Flight Limitations. Director/Autopilot must use same ADC data for RVSM. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message BAS Default Mode, L-R 2. PAGE NO: 2 - 29 3. Limitations and/or Procedures Operational Procedures C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. (Blue – Advisory) (GV-SP/GIV-X) BAS DEFLT MODE, L-R (Blue – Advisory) (GV) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message BAS Fail, L-R (Amber – Caution) (GV-SP/GIV-X) (continued) (O) 2 - 30 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched in the pressurized configuration with one Bleed Air System inoperative provided (GV-SP): a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows: 1. Affected Bleed Air Valve is selected OFF 2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTIICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, and d) Airplane is operated in accordance with AFM Limitations. NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN. Operational Procedures GV-SP pressurized configuration: Flight crew will CLOSE inoperative Bleed Control Valve and electrically deactivate affected system. If failure occurs with 1) Right Bleed Air Control Valve: Select Right Bleed Air Valve OFF utilizing R Eng Bleed Air Switch and Pull R Bleed CONT Circuit Breaker (CB). 2) Left Bleed Air Control Valve: Select Left Bleed Air Valve OFF utilizing L Eng Bleed Air Switch and Pull Left Bleed CONT Circuit Breaker (CB). In addition, opposite Engine Bleed Air Sytem will be verified operative and Isolation Valve will be selected OPEN. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message BAS Fail, L-R (Amber – Caution) (GV-SP/GIV-X) (O) (GIV-X): a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows: 1. Affected Bleed Air Valve is selected OFF 2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTIICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, d) Airplane is not operated in forecast or known icing conditions, and e) Airplane is operated in accordance with AFM Limitations. NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN. (continued) 2 - 31 3. Limitations and/or Procedures B PAGE NO: Operational Procedures GIV-X pressurized configuration: Flight crew will CLOSE associated Bleed Control Valve and electrically deactivate affected system. In addition, opposite Engine Bleed Air Sytem and Isolation Valve will be verified operative and Isolation Valve selected OPEN GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message BAS Fail, L-R (Amber – Caution) (GV-SP/GIV-X) (continued) (O) 2 - 32 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched in the unpressurized configuration with both Bleed Air Systems inoperative provided (GV-SP): a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows: 1. Affected Bleed Air Valve is selected OFF 2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. b) Manual pressurization control is selected, c) Outflow valve is slewed to the full OPEN position, d) RAM Air is selected ON, e) Cabin differential pressure is monitored to be nominally zero psid during the flight, f) Airplane is not operated in known or forecast icing conditions, and g) Airplane is operated in accordance with AFM Limitations. Operational Procedures For GV-SP unpressurized configuration: Flight crew will ensure inoperative Bleed Control Valve is CLOSED and deactivated electrically. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message BAS Fail, L-R (Amber – Caution) (GV-SP/GIV-X) (O) 2 - 33 3. Limitations and/or Procedures B PAGE NO: (GIV-X): a) Affected Valve(s) are verified CLOSED, b) Manual pressurization control is selected, c) Outflow valve is slewed to the full OPEN position, d) RAM Air is selected ON, e) Cabin differential pressure is monitored to be nominally zero psid during the flight, f) Airplane is not operated in forecast or known icing conditions, and g) Airplane is operated in accordance with AFM Limitations. Operational Procedures For GIV-X unpressurized configuration: Flight crew will ensure all affected Valve(s) are verified CLOSED. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message BAS FAIL, L-R (Amber – Caution) (GV) (continued) (O) 2 - 34 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched in the pressurized configuration with one Bleed Air System inoperative provided (GV): a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows: 1. Affected Bleed Air Valve is selected OFF 2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTIICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, and d) Airplane is operated in accordance with AFM Limitations. NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN. Operational Procedures GV pressurized configuration: Flight crew will CLOSE inoperative Bleed Control Valve and electrically deactivate affected system. If failure occurs with 1) Right Bleed Air Control Valve: Select Right Bleed Air Valve OFF utilizing R Eng Bleed Air Switch and Pull R Bleed CONT Circuit Breaker (CB). 2) Left Bleed Air Control Valve: Select Left Bleed Air Valve OFF utilizing L Eng Bleed Air Switch and Pull Left Bleed CONT Circuit Breaker (CB). In addition, opposite Engine Bleed Air Sytem will be verified operative and Isolation Valve will be selected OPEN. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message BAS FAIL, L-R (Amber – Caution) (GV) (O) 2 - 35 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched in the unpressurized configuration with both Bleed Air Systems inoperative provided (GV): a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows: 1. Affected Bleed Air Valve is selected OFF 2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. b) Manual pressurization control is selected, c) Outflow valve is slewed to the full OPEN position, d) RAM Air is selected ON, e) Cabin differential pressure is monitored to be nominally zero psid during the flight, f) Airplane is not operated in known or forecast icing conditions, and g) Airplane is operated in accordance with AFM Limitations. Operational Procedures For GV unpressurized configuration: Flight crew will ensure both Bleed Air Valves are CLOSED and deactivated electrically. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message BAS Maintenance Reqd, L-R PAGE NO: 2 - 36 3. Limitations and/or Procedures Operational Procedures C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. (Blue – Advisory) (GV-SP/GIV-X) BAS MAINT REQD, L-R (Blue – Advisory) (GV) BATT CHGR FAIL, L-R (Amber – Caution) (GV) A (O) Airplane may be dispatched with one Flight crew will pull and collar inoperative battery charger provided: associated “BATT CHGR” CB. a) Both Engine Generators are operative, b) APU Generator is operative, c) Associated L BATT CHGR: Left PDB, Left Main AC section or R BATT CHGR: Right PDB, Right Main AC section circuit breaker on the Power Distribution Box is pulled and collared, d) Standby Electrical System is operative, e) Affected Battery is selected OFF, and f) Repairs are made within two (2) flight days. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message Battery Charger Fail, L-R 2 - 37 3. Limitations and/or Procedures Operational Procedures A Airplane may be dispatched with one None required. ( inoperative battery charger provided: O )a) Both Engine Generators are operative, b) APU Generator is operative, c) Associated L BATT CHGR: Left PDB, Left Main AC section or R BATT CHGR: Right PDB, Right Main AC section circuit breaker on the Power Distribution Box is pulled and collared, d) Standby Electrical System is operative, e) Affected Battery is selected OFF, and f) Repairs are made within two (2) flight days. C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. (Amber – Caution) (GV-SP/GIV-X) Brake Maintenance Reqd 2. PAGE NO: (Blue – Advisory) (GV-SP/GIV-X) BRAKE MAINT REQD (Blue – Advisory) (GV) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CAB PRESS SEMIAUTO (Blue – Advisory) (GV-SP/GIV-X) Operational Procedures C Airplane may be dispatched provided airplane is operated in accordance with AFM Limitations. None required. C Airplane may be dispatched provided airplane is operated in accordance with AFM Limitations. None required. Airplane may be dispatched provided: a) Both Display Controllers, Weather Radar Controllers, and 2 MCDU’s are operative, and b) Current terminal charts for the origin, destination and alternate airports are carried, or EFB’s are carried, onboard the airplane and available to the flight crew. Flight crew will ensure: a) Both Display Controllers, Weather Radar Controllers and two MCDUs are operative, and b) Current terminal charts for the origin, destination and alternate airports are carried, or EFB’s are carried, onboard the airplane and available to the flight crew. (Blue – Advisory) (GV-SP/GIV-X) CCD 1-2 Fail 2 - 38 3. Limitations and/or Procedures (Blue – Advisory) (GV) Cabin Pressure Semi-auto PAGE NO: B (O) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message CDU 1-2-3 FAIL (Blue – Advisory) (GV) 2. 2 - 39 3. Limitations and/or Procedures A PAGE NO: Operational Procedures Except where en route operations or None required. approach minimums require its use, airplane may be dispatched provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, d) Both RFMUs are operative, and e) Repairs are made within two (2) flight days. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. One (1) system is required in PRNAV, BRNAV, RNAV 1 and RNAV 2 airspace. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CHECKLIST MISMATCH (Blue – Advisory) (GV) 2 - 40 3. Limitations and/or Procedures Operational Procedures B (O) Airplane may be dispatched provided: a) The checklist module in Fault Warning Computer (FWC) 1 is operative, and b) Current paper checklists are utilized. Flight crew will ensure: a) The checklist module in Fault Warning Computer (FWC) 1 is operative, and b) Utilize current paper checklists. C (O) Airplane may be dispatched provided: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Forward Cabin Temp Fan Fail; b) Cockpit Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) CKPT SENSOR FAN, REER D-10, is pulled and collared, and e) Flight crew monitor cockpit temperature and cockpit duct temperature. Flight crew will ensure: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Forward Cabin Temp Fan Fail, b) Cockpit Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) CKPT SENSOR FAN cirucuit breaker: REER D-10 is pulled and collared, and e) Cockpit temperature and cockpit duct temperature are monitored. (Blue – Advisory) (GV) CKPT TEMP FAN FAIL PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CMC Fail B CMF 1-2 Fail Airplane may be dispatched provided all faults are recorded after each flight. (Blue – Advisory) (GV-SP/GIV-X) Operational Procedures None required. B (O) Airplane may be dispatched provided: Flight crew will ensure: a) Alternate procedures are established a) Alternate procedures are and used, and established and used, and b) Flight crew utilizes voice over b) Voice over VHF/HF is used VHF/HF to relay pertinent to relay pertinent information information to the air traffic to the air traffic management management system. system. B (O) Airplane may be dispatch provided routine procedures do not require its use. Flight crew will ensure routine procedures do not require its use. Airplane may be dispatched with one (1) system inoperative. None required. (Blue – Advisory) (GV-SP/GIV-X) CMS 1-2 Fail 2 - 41 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) PAGE NO: B GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Cockpit Temp Fan Fail (Blue – Advisory) (GV-SP/GIV-X) (O) 2 - 42 3. Limitations and/or Procedures C PAGE NO: Airplane may be dispatched provided: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Forward Cabin Temp Fan Fail; b) Cockpit Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) CKPT SENSOR FAN, REER D-10, is pulled and collared, and e) Flight crew monitor cockpit temperature and cockpit duct temperature. Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Forward Cabin Temp Fan Fail, b) Cockpit Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) CKPT SENSOR FAN cirucuit breaker: REER D-10 is pulled and collared, and e) Cockpit temperature and cockpit duct temperature are monitored. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message Cockpit Voice Recorder Fail 2. A without FDR installed not Air Carrier or Commercial 2 - 43 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) PAGE NO: Operational Procedures Airplane may be dispatched provided: a) Flight Data Recorder (FDR) is operative, and b) Repairs are made within three (3) flight days. None required. Airplane may be dispatched provided repairs are made within three (3) flight days. None required. Airplane may be dispatched provided repairs are made in accordance with applicable 14 CFRs. None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Cowl Valve Fail Open, L-R (Amber – Caution) (GV-SP/GIV-X) (O) 2 - 44 3. Limitations and/or Procedures B PAGE NO: Airplane may be dispatched with one (1) inoperative provided: a) Affected Valve is verified OPEN, b) All components of both HP Bleed Air Systems are operative, c) Both Environmental Control Systems (ECS) Packs are operative, d) Affected Cowl Anti-Ice switch is ON, e) Affected L COWL ANTI-ICE: LEER, D3 or R COWL ANTI-ICE: REER, D-14 valve circuit breaker is pulled or in the OPEN position, f) Performance Computer is initialized with COWL ANTI ICE selected ON for either takeoff or landing when COWL ANTI-ICE valve is pressurized, and g) Airplane is operated in accordance with AFM Limitations and Performance. Operational Procedures Flight crew will ensure: a) BOTH HP Bleed Air Systems and BOTH Environmental Control System (ECS) Packs are operative. b) Select the affected Cowl Anti-Ice switch ON and ensure that the affected valve circuit breaker is pulled or in the OPEN position. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message COWL VLV FL OP, L-R CPAM Fail Flight crew will ensure: a) BOTH HP Bleed Air Systems and BOTH Environmental Control System (ECS) Packs are operative. b) Select the affected Cowl Anti-Ice switch ON and ensure that the affected valve circuit breaker is pulled or in the OPEN position. B Airplane may be dispatched provided both auto systems are operative. None required. B Airplane may be dispatched provided both auto systems are operative. None required. (Amber – Caution) (GV-SP/GIV-X) CPAM FAIL (Amber – Caution) (GV) Operational Procedures Airplane may be dispatched with one (1) inoperative provided: a) Affected Valve is verified OPEN, b) All components of both HP Bleed Air Systems are operative, c) Both Environmental Control Systems (ECS) Packs are operative, d) Affected Cowl Anti-Ice switch is ON, e) Affected L COWL ANTI-ICE: LEER, D3 or R COWL ANTI-ICE: REER, D-14 valve circuit breaker is pulled or in the OPEN position, f) Performance Computer is initialized with COWL ANTI ICE selected ON for either takeoff or landing when COWL ANTI-ICE valve is pressurized, and g) Airplane is operated in accordance with AFM Limitations and Performance. (Amber – Caution) (GV) (O) 2 - 45 3. Limitations and/or Procedures B PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS 1-2 Fail (Blue – Advisory) (GV-SP/GIV-X) (continued) (O) 2 - 46 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Airplane is operated in accordance with AFM Limitations and Abnormal Procedures (for Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Section 1, Limitations, and Section 3, Abnormal Procedures. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS 1-2 Fail (Blue – Advisory) (GV-SP/GIV-X) (cont’d) (O) 2 - 47 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Section 1, Limitations, and Section 3, Abnormal Procedures. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS 1-2 FAIL (Blue – Advisory) (GV) (continued) (O) 2 - 48 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Airplane is operated in accordance with AFM Limitations and Abnormal Procedures (for Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Section 1, Limitations, and Section 3, Abnormal Procedures. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS 1-2 FAIL (Blue – Advisory) (GV) (cont’d) (O) 2 - 49 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Section 1, Limitations, and Section 3, Abnormal Procedures. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS Channel 1-2 Fail (Blue – Advisory) (GV-SP/GIV-X) (continued) (O) 2 - 50 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Airplane is operated in accordance with AFM Limitations and Abnormal Procedures (for Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Limitations, and Abnormal Procedures. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS Channel 1-2 Fail (Blue – Advisory) (GV-SP/GIV-X) (cont’d) (O) 2 - 51 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Limitations, and Abnormal Procedures. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS CHNL 1-2 FAIL (Blue – Advisory) (GV) (continued) (O) 2 - 52 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Airplane is operated in accordance with AFM Limitations and Abnormal Procedures (for Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Limitations, and Abnormal Procedures. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS CHNL 1-2 FAIL (Blue – Advisory) (GV) (cont’d) (O) 2 - 53 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Limitations, and Abnormal Procedures. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS Control Panel Fail (Amber – Caution) (GV-SP/GIV-X) (continued) (O) 2 - 54 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Airplane is operated in accordance with AFM Limitations (for Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS Control Panel Fail (Amber – Caution) (GV-SP/GIV-X) (cont’d) (O) 2 - 55 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS CONT PNL FAIL (Amber – Caution) (GV) (continued) (O) 2 - 56 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Airplane is operated in accordance with AFM Limitations (for Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS CONT PNL FAIL (Amber – Caution) (GV) (cont’d) (O) 2 - 57 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS Fail - Select Manual (Amber – Caution) (GV-SP/GIV-X) (continued) (O) 2 - 58 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Airplane is operated in accordance with AFM Limitations (for Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS Fail - Select Manual (Amber – Caution) (GV-SP/GIV-X) (cont’d) (O) 2 - 59 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS FAIL-SEL MAN (Amber – Caution) (GV) (continued) (O) 2 - 60 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Airplane is operated in accordance with AFM Limitations (for Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message CPCS FAIL-SEL MAN (Amber – Caution) (GV) (cont’d) (O) 2 - 61 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings – Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message CPCS LAND ELEV FL Operational Procedures B Airplane may be dispatched provided pressurization system is operated in the Semi mode. None required. B Airplane may be dispatched provided pressurization system is operated in the Semi mode. None required. C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. A Airplane may be dispatched provided: a) Auto system (Cabin Pressure Control Panel) is operative, b) Semi-auto mode is considered inoperative, and c) Repairs are made within two (2) flight days. None required. (Blue – Advisory) (GV-SP/GIV-X) CPCS Maintenance Required 2 - 62 3. Limitations and/or Procedures (Blue – Advisory) (GV) CPCS Landing Elevation Fail 2. PAGE NO: (Blue – Advisory) (GV-SP/GIV-X) CPCS MAINT REQD (Blue – Advisory) (GV) CPCS Select Panel Fault (Blue – Advisory) (GV-SP/GIV-X) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message (Blue – Advisory) (GV) A (Blue – Advisory) (GV) without FDR installed not Air Carrier or Commercial 2 - 63 3. Limitations and/or Procedures CPCS SEL PNL FAULT A CVR FAIL 2. PAGE NO: Operational Procedures Airplane may be dispatched provided: a) Auto system (Cabin Pressure Control Panel) is operative, b) Semi-auto mode is considered inoperative, and c) Repairs are made within two (2) flight days. None required. Airplane may be dispatched provided: a) Flight Data Recorder (FDR) is operative, and b) Repairs are made within three (3) flight days. None required. Airplane may be dispatched provided repairs are made within three (3) flight days. None required. Airplane may be dispatched provided repairs are made in accordance with applicable 14 CFRs. None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Database Config B DAU 1A FL DAU 1B FL DAU 2A FL DAU 2B FL (Blue – Advisory) (GV) A (O) 2 - 64 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) PAGE NO: Operational Procedures Except where en route operations or minimums require a current database, airplane may be dispatched with charts out of currency provided: a) Current Aeronautical Charts are used to verify Navigation fixes before dispatch, b) Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight, and c) Approach Navigation Radios are manually tuned and identified. None required. Airplane may be dispatched with one (1) failed DAU channel provided: a) Flight crew selects operative channel via the display controller, and b) Repairs are made within two (2) flight days. Flight crew will select operative channel via the display controller. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message DISP CTRL 2 FAIL (Blue – Advisory) (GV) (continued) (O) 2 - 65 3. Limitations and/or Procedures A PAGE NO: Aircraft may be dispatched provided: a) The weather at the destination is forecast to be VFR (1,000 ft ceiling and three (3) miles visibility), b) An alternate airport is specified in the flight plan which has VFR weather forecast (1,000 ft ceiling and three (3) miles visibility), c) Both VOR and ADF navigation receivers are operative, d) Flight is conducted based on short range navigation sources only being available, e) Navigation suffix in the IFR flight plan clearly indicates that the airplane is not capable of any RNP required navigation capability, f) Flight is conducted in airspace where the availability of navigation by short range navigation receivers (VOR/ADF) is assured, g) One DBDI or Standby RMI or Secondary Navigation Display is operative, h) Alternate procedures are established and used, Operational Procedures Flight crew will ensure associated Display Controller circuit breaker for the failed Display Controller is pulled and collared. The flight crew shall prepare and display a TOLD (Takeoff and Landing Data) card prior to takeoff and prior to approach and landing. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message 2. PAGE NO: 2 - 66 3. Limitations and/or Procedures i) j) k) l) m) Flight crew pull and collar associated Display Controller circuit breaker, Flight crew prepare and display a TOLD (Takeoff and Landing Data) card prior to takeoff and prior to approach and landing (GV only), Flight crew verify required approaches are available at the destination and alternate airports without being NOTAMed out of service or unusable, Pilot-Not-Flying (PNF) is prepared to announce approach minimums in the event the operative Display Controller fails enroute, and Repairs are made within one (1) flight day. Operational Procedures GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Display Controller 2 Fail (Blue – Advisory) (GV-SP/GIV-X) (continued) (O) 2 - 67 3. Limitations and/or Procedures A PAGE NO: Aircraft may be dispatched provided: a) The weather at the destination is forecast to be VFR (1,000 ft ceiling and three (3) miles visibility), b) An alternate airport is specified in the flight plan which has VFR weather forecast (1,000 ft ceiling and three (3) miles visibility), c) Both VOR and ADF navigation receivers are operative, d) Flight is conducted based on short range navigation sources only being available, e) Navigation suffix in the IFR flight plan clearly indicates that the airplane is not capable of any RNP required navigation capability, f) Flight is conducted in airspace where the availability of navigation by short range navigation receivers (VOR/ADF) is assured, g) One DBDI or Standby RMI or Secondary Navigation Display is operative, h) Alternate procedures are established and used, Operational Procedures Flight crew will pull and collar associated Display Controller circuit breaker. Flight crew will verify the required approaches are available at the destination and alternate airports without being NOTAMed out of service or unusable. When weather conditions exist at the destination or alternate airport during the approach, the PNF will be prepared to announce approach minimums in the event the operative Display Controller fails en route. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message 2. PAGE NO: 2 - 68 3. Limitations and/or Procedures i) j) k) l) m) Flight crew pull and collar associated Display Controller circuit breaker, Flight crew prepare and display a TOLD (Takeoff and Landing Data) card prior to takeoff and prior to approach and landing (GV only), Flight crew verify required approaches are available at the destination and alternate airports without being NOTAMed out of service or unusable, Pilot-Not-Flying (PNF) is prepared to announce approach minimums in the event the operative Display Controller fails en route, and Repairs are made within one (1) flight day. Operational Procedures GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message DME 1-2 Fail (Amber – Caution) (GV-SP/GIV-X) Operational Procedures C Airplane may be dispatched except where en route operations or approach minimums require its use. Any in excess of those required by 14 CFR may be inoperative. None required. B Airplane may be dispatched. None required. (Blue – Advisory) (GV-SP/GIV-X) Elevator Trim 1-2 Fail 2 - 69 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) EGPWM SYS 1-2 Fail PAGE NO: NOTE: Synthetic Vision PFD synthetic terrain will not be available with dual Terrain Server failures, but the full PFD may be used without restriction. B (O) Airplane may be dispatched with electric elevator trim inoperative provided: a) Electric Elevator Trim remains OFF, b) Both Flap/Stabilizer Control Channels are operative (no messages on CAS), and c) Airplane is operated in accordance with AFM Limitations (Maximum Operating Limit Speed 0.80 Mach). Flight crew will ensure electronic Pitch Trim remains “OFF”, both Flap/Stabilizer Control Channels are operative (no messages on CAS), and airplane is operated in accordance with AFM Limitations (Maximum Operating Limit Speed is 0.80 Mach). GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message ELEV TRIM INOP B (O) Engine Maintenance ###, L-R (Blue – Advisory) (GV-SP/GIV-X) A (O) 2 - 70 3. Limitations and/or Procedures (Amber – Caution) (GV) PAGE NO: Airplane may be dispatched with electric elevator trim inoperative provided: a) Electric Elevator Trim remains OFF, b) Both Flap/Stabilizer Control Channels are operative (no messages on CAS), and c) Airplane is operated in accordance with AFM Limitations (Maximum Operating Limit Speed 0.80 Mach). Airplane may be dispatched with Blue “Engine Maintenance STD (###)” and/or “Engine Maintenance LTD” messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and b) FADEC faults are reviewed by flight crew before each takeoff. NOTE: Blue “Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue “Engine Maintenance LTD” messages required maintenance action within 500 hours. Operational Procedures Flight crew will ensure electronic Pitch Trim remains “OFF”, both Flap/Stabilizer Control Channels are operative (no messages on CAS), and airplane is operated in accordance with AFM Limitations (Maximum Operating Limit Speed is 0.80 Mach). Flight crew will ensure repairs are made in accordance with times (hours) established. Flight crew will review FADEC faults prior to each takeoff. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Engine Maintenance LTD, L-R A (Blue – Advisory) (GV-SP/GIV-X) 2 - 71 3. Limitations and/or Procedures (O) PAGE NO: Airplane may be dispatched with Blue “Engine Maintenance STD (###)” and/or “Engine Maintenance LTD” messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and b) FADEC faults are reviewed by flight crew before each takeoff. NOTE: Blue “Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue “Engine Maintenance LTD” messages required maintenance action within 500 hours. Operational Procedures Flight crew will ensure repairs are made in accordance with times (hours) established. Flight crew will review FADEC faults prior to each takeoff. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message ENG MAINT ###, L-R (Blue – Advisory) (GV) (O) 2 - 72 3. Limitations and/or Procedures A PAGE NO: Airplane may be dispatched with Blue “Engine Maintenance STD (###)” and/or “Engine Maintenance LTD” messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and b) FADEC faults are reviewed by flight crew before each takeoff. NOTE: Blue “Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue “Engine Maintenance LTD” messages required maintenance action within 500 hours. Operational Procedures Flight crew will ensure repairs are made in accordance with times (hours) established. Flight crew will review FADEC faults prior to each takeoff. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message ENG MAINT LTD, L-R (Blue – Advisory) (GV) (O) 2 - 73 3. Limitations and/or Procedures A PAGE NO: Airplane may be dispatched with Blue “Engine Maintenance STD (###)” and/or “Engine Maintenance LTD” messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and b) FADEC faults are reviewed by flight crew before each takeoff. NOTE: Blue “Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue “Engine Maintenance LTD” messages required maintenance action within 500 hours. Operational Procedures Flight crew will ensure repairs are made in accordance with times (hours) established. Flight crew will review FADEC faults prior to each takeoff. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message EPS Maintenance Reqd, L-R 2. PAGE NO: 2 - 74 3. Limitations and/or Procedures Operational Procedures C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. (Blue – Advisory) (GV-SP/GIV-X) EPS MAINT REQD, L-R (Blue – Advisory) (GV) EVS Fail (Amber – Caution) (GV-SP/GIV-X) EVS FAIL (Amber – Caution) (GV) EVS Maintenance Required (Blue – Advisory) (GV-SP/GIV-X) EVS MAINT REQD (Blue – Advisory) (GV) EVS Window Heat Fail (Amber – Caution) (GV-SP/GIV-X) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message EVS WINDOW HEAT FAIL 2. PAGE NO: 2 - 75 3. Limitations and/or Procedures Operational Procedures C Airplane may be dispatched. None required. A Airplane may be dispatched provided: a) Cockpit Voice Recorder (CVR) is operative, b) Airplane is not dispatched from a designated airport as listed in the operator’s MEL unless the FDR failure occurs after pushback but before takeoff, and c) Repairs are made within three (3) flight days. None required. (Amber – Caution) (GV) FDAU FAIL (Blue – Advisory) (GV) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message FDR SYS FAIL (Blue – Advisory) (GV-SP/GIV-X) 2 - 76 3. Limitations and/or Procedures Operational Procedures A Airplane may be dispatched provided: a) Cockpit Voice Recorder (CVR) is operative, b) Airplane is not dispatched from a designated airport as listed in the operator’s MEL unless the FDR failure occurs after pushback but before takeoff, and c) Repairs are made within three (3) flight days. None required. A Airplane may be dispatched provided: a) Cockpit Voice Recorder (CVR) is operative, b) Airplane is not dispatched from a designated airport as listed in the operator’s MEL unless the FDR failure occurs after pushback but before takeoff, and c) Repairs are made within three (3) flight days. None required. (Blue – Advisory) (GV) FDR System Fail 2. PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message FGC 1-2 FAIL B (O) 2 - 77 3. Limitations and/or Procedures (Amber – Caution) (GV) PAGE NO: Except for ER operations or where en route operations or approach minimums require its use, airplane may be dispatched with one (1) failed provided airplane is operated in accordance with AFM Limitations in the event the operative FGC fails and the Yaw Damper is inoperative. Operational Procedures Flight crew will observe AFM limitations in the event the operative FGC fails and the Yaw Damper is inoperative. NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations. Fire Detection Loop Fault B Except for ER operations, airplane may be None required. dispatched with one (1) complete loop (A or B) inoperative provided the Fault Switch/Light is pressed to isolate the faulty loop and illuminate the OFF portion of the switch light. B Except for ER operations, airplane may be None required. dispatched with one (1) complete loop (A or B) inoperative provided the Fault Switch/Light is pressed to isolate the faulty loop and illuminate the OFF portion of the switch light. (Amber – Caution) (GV-SP/GIV-X) FIRE DET LOOP FALT (Amber – Caution) (GV) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message Flap/Stab Maint Reqd A-B 2. PAGE NO: 2 - 78 3. Limitations and/or Procedures Operational Procedures C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. A Airplane may be dispatched with one (1) channel inoperative provided: a) Electric Pitch Trim System is operative, b) Alternate control is verified to be operative before each departure, and c) Repairs are made within two (2) flight days. None required. C Airplane may be dispatched. None required. (Blue – Advisory) (GV-SP) Flap/Stab Maint Reqd (Blue – Advisory) (GIV-X) Flap/Stab System Fail A-B (Blue – Advisory) (GV-SP) FLP/STB MX RQD A-B (Blue – Advisory) (GV) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message FLP/STB SYS FL A-B A FMS/GPS Pos Monitor Unavail B (Blue – Advisory) (GV-SP/GIV-X) (O) 2 - 79 3. Limitations and/or Procedures (Blue – Advisory) (GV) PAGE NO: Operational Procedures Airplane may be dispatched with one (1) channel inoperative provided: a) Electric Pitch Trim System is operative, d) Alternate control is verified to be operative before each departure, and e) Repairs are made within two (2) flight days. None required. Airplane may be dispatched provided: a) FMS position is checked against available sensors, and b) If errors encountered, affected GPS is de-selected as a position sensor and FMS position is updated. Check FMS position against available sensors. De-select GPS as a position sensor and update FMS position if errors encountered. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message FMS 1-2-3 Fail (Blue – Advisory) (GV-SP/GIV-X) 2. 2 - 80 3. Limitations and/or Procedures A PAGE NO: Operational Procedures Airplane may be dispatched with two (2) None required. inoperative except where en route operations or approach minimums require its use provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, d) Both RFMU’s are operative (GV), and e) Repairs are made within two (2) flight days. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. RNP RNAV including PRNAV and BRNAV only require a single FMS. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message FMS 1-2 FAIL (Blue – Advisory) (GV) 2. 2 - 81 3. Limitations and/or Procedures A PAGE NO: Operational Procedures Airplane may be dispatched with two (2) None required. inoperative except where en route operations or approach minimums require its use provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, d) Both RFMU’s are operative (GV), and e) Repairs are made within two (2) flight days. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. RNP RNAV including PRNAV and BRNAV only require a single FMS. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message FQMS Maintenance Required Operational Procedures Airplane may be dispatched provided: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Cockpit Temp Fan Fail; b) Forward Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) FWD CABIN SENSOR FAN, LEER D9, is pulled and collared, and e) Flight crew monitor forward cabin temperature and forward cabin duct temperature. Flight crew will ensure: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Cockpit Temp Fan Fail, b) Forward Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) FWD CABIN SENSOR FAN cirucuit breaker: LEER D-9 is pulled and collared, and e) Forward cabin temperature and Forward cabin duct temperature are monitored. C Airplane may be dispatched. None required. C Airplane may be dispatched. None required. (Blue – Advisory) (GV-SP/GIV-X) (O) 2 - 82 3. Limitations and/or Procedures Forward Cabin Temp Fan Fail C PAGE NO: (Blue – Advisory) (GV-SP/GIV-X) FQMS MAINT REQD (Blue – Advisory) (GV) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message FQSC Channel Fail, L-R (Blue – Advisory) (GV-SP/GIV-X) (O) 2 - 83 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched with one (1) channel inoperative provided: a) Both tanks are completely filled using overwing refueling, b) Both Fuel Flow Indicating Systems are operative, c) After takeoff, power is set by matching fuel flow indications on both engines, and d) Flight crew maintains a log of fuel burned. NOTE: Total Fuel indications will be INVALID with inoperative indicator. Operational Procedures Flight crew will ensure BOTH tanks are completely filled using overwing method of fueling. NOTE: Do not pull Quel Qty circuit breaker as this disables Fuel Level Low caution message. Flight crew will ensure: a) B oth Fuel Flow Indicating Systems are operative. b) After takeoff, power is set by matching Fuel Flow indications on both engines. c) A log of fuel burned is maintained. NOTE: Total Fuel indication will be INVALID with inoperative indicator. (continued) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message FQSC Channel Fail, L-R (Blue – Advisory) (GV-SP/GIV-X) (cont’d) (O) 2 - 84 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched with one (1) channel inoperative provided: a) Affected tank is defueled before each refueling, b) Affected tank is fueled with a known quantity of fuel, c) Both fuel flow meters are operative, d) After takeoff, power is set by matching fuel flow indications on both engines, and e) Flight crew maintains a log of fuel burned. NOTE: Total Fuel indications will be INVALID with inoperative indicator. Operational Procedures Flight crew will Defuel affected tank before each refueling and refuel it with a Known quantity of fuel. Flight crew will ensure: a) Both fuel flow meters are operative. b) After takeoff, power is set by matching Fuel Flow indications on both engines. c) A log of fuel burned is maintained. NOTE: Total Fuel indication will be INVALID with inoperative indicator. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message FQSC CH FAIL, L-R (Blue – Advisory) (GV) (O) 2 - 85 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched with one (1) channel inoperative provided: a) Both tanks are completely filled using overwing refueling, b) Both Fuel Flow Indicating Systems are operative, c) After takeoff, power is set by matching fuel flow indications on both engines, and d) Flight crew maintains a log of fuel burned. NOTE: Total Fuel indications will be INVALID with inoperative indicator. Operational Procedures Flight crew will ensure BOTH tanks are completely filled using overwing method of fueling. NOTE: Do not pull Quel Qty circuit breaker as this disables Fuel Level Low caution message. Flight crew will ensure: a) B oth Fuel Flow Indicating Systems are operative. b) After takeoff, power is set by matching Fuel Flow indications on both engines. c) A log of fuel burned is maintained. NOTE: Total Fuel indication will be INVALID with inoperative indicator. (continued) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message FQSC CH FAIL, L-R (Blue – Advisory) (GV) (cont’d) (O) 2 - 86 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched with one (1) channel inoperative provided: a) Affected tank is defueled before each refueling, b) Affected tank is fueled with a known quantity of fuel, c) Both fuel flow meters are operative, d) After takeoff, power is set by matching fuel flow indications on both engines, and e) Flight crew maintains a log of fuel burned. NOTE: Total Fuel indications will be INVALID with inoperative indicator. Operational Procedures Flight crew will Defuel affected tank before each refueling and refuel it with a Known quantity of fuel. Flight crew will ensure: a) Both fuel flow meters are operative. b) After takeoff, power is set by matching Fuel Flow indications on both engines. c) A log of fuel burned is maintained. NOTE: Total Fuel indication will be INVALID with inoperative indicator. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Front Windshield Fail, L-R (Amber – Caution) (GV-SP/GIV-X) Operational Procedures B Except for ER operations, airplane may be dispatched with one (1) inoperative provided airplane is not operated in known or forecast icing conditions. None required. C Airplane may be dispatched with one inoperative sensor in each Windshield Heat System. None required. Except for ER operations, airplane may be dispatched with inoperative crossflow valve provided: a) All Fuel Boost Pumps are operative, b) Fuel Intertank Valve is operative, c) Fuel Quantity Indicating System is operative, d) Fuel Tank Temperature System is operative, and e) Airplane is operated in accordance with AFM Limitations. Flight crew will ensure: a) All Fuel boost Pumps are operative, b) Fuel Intertank Valve is operative, c) Fuel Quantity Indicating System is operative, d) Fuel tank temperature system is operative. (Blue – Advisory) (GV-SP/GIV-X) Fuel Crossflow Valve Open 2 - 87 3. Limitations and/or Procedures (Amber – Caution) (GV-SP/GIV-X) Front Windshield Fault, L-R PAGE NO: B (O) NOTE: Avoid uncoordinated maneuvers when Fuel Intertank Valve is OPEN. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message Fuel Return Fail, L-R (Blue – Advisory) (GV) 2 - 88 3. Limitations and/or Procedures Operational Procedures B Airplane may be dispatched provided: a) Flight crew monitors fuel tank temperature, and b) Airplane is operated in accordance with AFM Limitations. None required. B Airplane may be dispatched provided: a) Flight crew monitors fuel tank temperature, and b) Airplane is operated in accordance with AFM Limitations. None required. (Blue – Advisory) (GV-SP) FUEL RETURN FL, L-R 2. PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message FWD CAB TMP FAN FL C F WSHLD FAIL, L-R (Amber – Caution) (GV) B (O) 2 - 89 3. Limitations and/or Procedures (Blue – Advisory) (GV) PAGE NO: Operational Procedures Airplane may be dispatched provided: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Cockpit Temp Fan Fail; b) Forward Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) FWD CABIN SENSOR FAN, LEER D-9, is pulled and collared, and e) Flight crew monitor forward cabin temperature and forward cabin duct temperature. Flight crew will ensure: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Cockpit Temp Fan Fail, b) Forward Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) FWD CABIN SENSOR FAN cirucuit breaker: LEER D-9 is pulled and collared, and e) Forward cabin temperature and Forward cabin duct temperature are monitored. Except for ER operations, airplane may be dispatched with one (1) inoperative provided airplane is not operated in known or forecast icing conditions. None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message GCU Fail, L-R (Blue – Advisory) (GV) 2 - 90 3. Limitations and/or Procedures Operational Procedures A Except for ER Operations, airplane may be dispatched with one Engine Generator Control Unit (GCU) inoperative provided: a) APU Generator is used for all phases of flight, b) Airplane is operated at or below FL450, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. None required. A Except for ER operations, airplane may be dispatched with one Engine Generator Control Unit (GCU) inoperative provided: a) APU Generator is used for all phases of flight, b) Airplane is operated at or below FL450, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. None required. (Blue – Advisory) (GV-SP/GIV-X) GCU FAIL, L-R 2. PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message Generator Fail, L-R (Blue – Advisory) (GV) 2 - 91 3. Limitations and/or Procedures Operational Procedures A Except for ER operations, airplane may be dispatched with one Engine Generator Control Unit (GCU) inoperative provided: a) APU Generator is used for all phases of flight, b) Airplane is operated at or below FL450, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. None required. A Except for ER operations, airplane may be dispatched with one Engine Generator Control Unit (GCU) inoperative provided: a) APU Generator is used for all phases of flight, b) Airplane is operated at or below FL450, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. None required. (Blue – Advisory) (GV-SP/GIV-X) GEN FAIL, L-R 2. PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message GPS 1-2 Fail (Blue – Advisory) (GV-SP/GIV-X) Operational Procedures B Airplane may be dispatched except where en route operations or approach minimums require the use of GPS or GNSSU. None required. B Airplane may be dispatched except where en route operations or approach minimums require the use of GPS or GNSSU. None required. Airplane may be dispatched provided: a) Alternate procedures are established and used, b) Pilot-Not-Flying (PNF) monitors flight progress with reference to radio altimeter data and situational awareness, c) PNF advises Pilot-Flying (PF) of adverse situations, d) Airplane is operated in accordance with AFM Limitations, and e) Repairs are made within two (2) flight days. Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. (Blue – Advisory) (GV) GPWS 1-2 Fail 2 - 92 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) GPS 1-2 FAIL PAGE NO: A (O) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message GPWS FAIL HUD COMP Fan Fail Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. C Airplane may be dispatched provided extended ground operations are avoided. None required. C Airplane may be dispatched provided: a) Extended ground operations are avoided, and b) Pilot selected HUD brightness is reduced. None required. (Blue – Advisory) (GV-SP/GIV-X) HUD OHU Fan Fail (Blue – Advisory) (GV-SP/GIV-X) Operational Procedures Airplane may be dispatched provided: a) Alternate procedures are established and used, b) Pilot-Not-Flying (PNF) monitors flight progress with reference to radio altimeter data and situational awareness, c) PNF advises Pilot-Flying (PF) of adverse situations, d) Airplane is operated in accordance with AFM Limitations, and e) Repairs are made within two (2) flight days. (Blue – Advisory) (GV) (O) 2 - 93 3. Limitations and/or Procedures A PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message Hydraulic Temp Sen Fail, L-R B (Blue – Advisory) (GV) 2 - 94 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) HYD TMP SEN FL, L-R 2. PAGE NO: Airplane may be dispatched. Operational Procedures None required. NOTE: Accuracy of hydraulic quantity indication will be degraded during long flights in cold soak conditions. If Right Hydraulic System (R SYS) sensor has failed in flight, there is no protection against overheating R SYS pumps during Power Transfer Unit (PTU) operation. In flight, with either or both sensors failed, there is no warning of hot hydraulic system temperatures. B Airplane may be dispatched. NOTE: Accuracy of hydraulic quantity indication will be degraded during long flights in cold soak conditions. If Right Hydraulic System (R SYS) sensor has failed in flight, there is no protection against overheating R SYS pumps during Power Transfer Unit (PTU) operation. In flight, with either or both sensors failed, there is no warning of hot hydraulic system temperatures. None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Ice Detect Fail, L-R (Amber – Caution) (GV-SP/GIV-X) (O) 2 - 95 3. Limitations and/or Procedures B PAGE NO: Airplane may be dispatched provided: a) Airplane is operated in accordance with alternate AFM procedures, b) Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and SAT is +10 deg C or less, and c) Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges. NOTE: With Ice Detection Systems inoperative, automatic anti-ice is not available. Operational Procedures Flight crew shall operate airplane in accordance with Alternate AFM procedures. Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and the SAT is +10 deg C or less. Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message ICE DETECT FL, L-R (Amber – Caution) (GV) (O) 2 - 96 3. Limitations and/or Procedures B PAGE NO: Airplane may be dispatched provided: a) Airplane is operated in accordance with alternate AFM procedures, b) Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and SAT is +10 deg C or less, and c) Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges. NOTE: With Ice Detection Systems inoperative, automatic anti-ice is not available. Operational Procedures Flight crew shall operate airplane in accordance with Alternate AFM procedures. Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and the SAT is +10 deg C or less. Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message IRS 1-2-3 Fail (Blue – Advisory) (GV) 2 - 97 3. Limitations and/or Procedures Operational Procedures A (O) Airplane may be dispatched with one (1) Flight crew will ensure the same IRS inoperative provided: IRS is NOT used as attitude a) Both PFD attitude indicating systems source for both pilots. operate independently, b) Flight crew ensure same IRS is NOT used as attitude source for both pilots, c) Standby Attitude Indicator is operative, and d) Repairs are made within two (2) flight days. A (O) Airplane may be dispatched with one (1) Flight crew will ensure the same IRS inoperative provided: IRS is NOT used as attitude a) Both PFD attitude indicating systems source for both pilots. operate independently, b) Flight crew ensure same IRS is NOT used as attitude source for both pilots, c) Standby Attitude Indicator is operative, and d) Repairs are made within two (2) flight days. (Blue – Advisory) (GV-SP/GIV-X) IRS 1-2-3 FAIL PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message IRS 1-2-3 ON DC (Blue – Advisory) (GV-SP/GIV-X) 2 - 98 3. Limitations and/or Procedures Operational Procedures A Airplane may be dispatched provided only one (1) IRU / IRS is on Secondary Power provided repairs are made within one (1) flight day. None required. A Airplane may be dispatched provided only one (1) IRU / IRS is on Secondary Power provided repairs are made within one (1) flight day. None required. (Blue – Advisory) (GV) IRU On Sec Pwr 2. PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message IRU Sec Pwr 1-2-3 Fail (Blue – Advisory) (GV) 2 - 99 3. Limitations and/or Procedures Operational Procedures A Airplane may be dispatched with both back- None required. up batteries inoperative provided: a) The affected battery is located in the #2 or #3 IRU back up battery position, and b) Repairs are made within one (1) flight day. A Airplane may be dispatched with both back- None required. up batteries inoperative provided: a) Airplane is operated in day VMC conditions, and b) Repairs are made within one (1) flight day. A Airplane may be dispatched with both back- None required. up batteries inoperative provided: a) All other components of the Electrical Power system are operative, and b) Repairs are made within one (1) flight day. B Airplane may be dispatched provided at least one Flight Management System is operative. (Blue – Advisory) (GV-SP/GIV-X) LASERTRAK FAIL 2. PAGE NO: None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message L PSU Fan Fail B LX Fail (O) 2 - 100 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) PAGE NO: Operational Procedures Airplane may be dispatched provided: Flight crew will: a) Ambient Temperature is 95 degrees F a) Minimize ground operation (35 degrees C) or cooler, time, espescially during hot b) TRU electrical loads are 50% or less, weather, c) Right main TRU is operative, b) During Ground operation, d) Both Environmental Control System monitor TRU load – limit (ECS) Packs are operative, load to 50%, e) Flight crew minimize ground operation c) For ground operation longer time, and than 15 minutes ensure f) For ground operations longer than 15 main and baggage doors minutes, flight crew ensure main and are closed. APU air is baggage doors are closed, APU air is selected “ON” and outflow selected “ON” and outflow valve is fully valve is fully OPEN. OPEN. C Airplane may be dispatched. None required. B Airplane may be dispatched with one (1) Mach Trim System inoperative. None required. (Blue – Advisory) (GV-SP/GIV-X) Mach Trim 1-2 Fail (Blue – Advisory) (GV-SP/GIV-X) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message MADC 1-2-3 FAIL (Blue – Advisory) (GV) (O) 2 - 101 3. Limitations and/or Procedures B PAGE NO: Airplane may be dispatched with a one (1) micro air data computer inoperative provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Airplane is operated in accordance with AFM limitations, f) MADC 1: POP A-9, MADC 2: CPOP A-9, and MADC 3: POP A-10 circuit breakers associated with the failed Micro Air Data Computer (MADC) are pulled and collared, and g) Flight crew selects operative and different MADC sources prior to departure. NOTE 1: Two systems are required for operation in RVSM airspace. NOTE 2: For MADC 1 FAIL, expect the L Engine Backup Air Data advisory and associated Engine Maintenance message to post. NOTE 3: For MADC 2 FAIL, expect the R Engine Backup Air Data advisory and associated Engine Maintenance message to post. Operational Procedures Flight crew will pull and collar MADC 1: POP A-9, MADC 2: CPOP A-9, and MADC 3: POP A-10 circuit breaker associated with Micro Air Data Computers. Flight crew will operationally check and assure that the items called out in provisos a) thru d) are operative. Flight crew will comply with all AFM limitations in section 1-0330, 1-03-40, and 1-21-10. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message MADC 1-2-3 FAIL (Blue – Advisory) (GV) 2 - 102 3. Limitations and/or Procedures Operational Procedures B (O) Airplane may be dispatched with one (1) micro air data computer inoperative provided airplane is operated in unpressurized configuration. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight. A (O) Except for ER operations, airplane may be dispatched with one (1) probe heater inoperative provided: a) Airplane is not operated in visible moisture or known or forecast icing conditions, b) L LWR PITOT HTR: CPOP A-5 and R LWR PITOT HTR: CPOP A-5 circuit breakers are pulled and collared, c) Flight crew select MADC sources that are different and not associated with failed pitot heater element, and d) Repairs are made within two (2) flight days. Flight crew will pull and collar L LWR PITOT HTR: CPOP A-5 and R LWR PITOT HTR: CPOP A-5 circuit breakers and select MADC sources that are different and not associated with failed pitot heater element. (Blue – Advisory) (GV) (cont’d) MADC 1-3 PROBE FL PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message MADC 2-SBY PROBE FL (Blue – Advisory) (GV) (O) 2 - 103 3. Limitations and/or Procedures A PAGE NO: Except for ER operations, airplane may be dispatched with one (1) probe heater inoperative provided: a) Airplane is not operated in visible moisture or known or forecast icing conditions, b) L UPR PITOT HTR: CPOP A-6 and R UPR PITOT HTR: CPOP A-6 circuit breakers are pulled and collared, c) Flight crew select MADC sources that are different and not associated with failed pitot heater element, and d) Repairs are made within two (2) flight days. Operational Procedures Flight crew will pull and collar L UPR PITOT HTR: CPOP A-6 and R UPR PITOT HTR: CPOP A-6 circuit breakers and select MADC sources that are different and not associated with failed pitot heater element. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Main Fuel Pump Fail, L-R (Amber – Caution) (GV-SP/GIV-X) (O) 2 - 104 3. Limitations and/or Procedures B PAGE NO: Except for ER operations, airplane may be dispatched with one (1) pump inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, d) Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, and e) Airplane is operated in accordance with AFM Limitations. Operational Procedures Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative, b) BOTH Fuel Low Quantity Warning Systems are operative, c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message MAIN PUMP FAIL, L-R B MAINT REQUIRED (Blue – Advisory) (GV) C (O) 2 - 105 3. Limitations and/or Procedures (Amber – Caution) (GV) PAGE NO: Operational Procedures Except for ER operations, airplane may be dispatched with one (1) pump inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, d) Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, and e) Airplane is operated in accordance with AFM Limitations. Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative, b) BOTH Fuel Low Quantity Warning Systems are operative, c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure. Airplane may be dispatched. None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Main TRU Fault, L-R A MAU 1-2-3 Fan Fail (Blue – Advisory) (GV-SP/GIV-X) B (O) 2 - 106 3. Limitations and/or Procedures (Amber – Caution) (GV-SP/GIV-X) PAGE NO: Airplane may be dispatched with one (1) main TRU inoperative provided: a) Both Generators are operative, b) Both essential TRU’s are operative, c) Auxiliary TRU is operative, d) APU Generator is operative, e) Both Battery chargers are operative, f) Both Main Airplane Batteries are operative, g) Inoperative L MAIN TRU: LPDB, Left Main AC section or R MAIN TRU: RPDB, Right Main AC section TRU circuit breaker on the Power Distribution Box is pulled and collared, and h) Repairs are made within two (2) flight days. Airplane may be dispatched: a) With one (1) failed fan provided performance of items affected by the indicated MAU are monitored during the flight, and b) Flight crew references the appropriate matrix in AFM Section 03-16-80. Operational Procedures Flight crew will pull and collar inoperative TRU circuit breaker on Power Distribution Box. Flight crew will ensure AUX TRU is operative and both essential TRUs are operative. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message MAU 1B-2A-3A-3B Fail (Amber – Caution) (GV-SP/GIV-X) (O) 2 - 107 3. Limitations and/or Procedures A PAGE NO: Airplane may be dispatched with one (1) channel inoperative provided: a) Failed channel is not MAU 1A or MAU 2B, b) No other failures exist in the Avionics System, c) Associated MAU circuit breakers: MAU 1A PRI: POP, A-10 MAU 1A SEC: CPOP, A-10 MAU 1B PRI: CPOP, A-9 MAU 1B SEC: POP, A-9 MAU 2A PRI: CPOP, A-8 MAU 2A SEC: POP, A-8 MAU 2B PRI: CPOP, A-7 MAU 2B SEC: POP, A-7 MAU 3A PRI: POP, A-6 MAU 3A SEC: CPOP, A-6 MAU 3B PRI: POP, A-5 MAU 3B SEC: CPOP, A-5 are pulled and collared, d) Alternate procedures are established and used, e) Flight crew discusses contingency procedures for next worse failures as described in GAC-OIS-09 Dispatch with MAU Channels Inoperative, and f) Repairs are made within two (2) flight days. Operational Procedures Flight crew will pull and collar the associated MAU circuit breakers. Flight crew will review the next worse failures as described in the GAC-OIS-09 Dispatch with MAU Channels Inoperative. Flight crew will discuss contingency procedures should the next worse failure occur and plan accordingly for the flight. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message MDAU FAIL (Amber – Caution) (GV) Operational Procedures B Airplane may be dispatched provided all faults are recorded after each flight. None required. B Airplane may be dispatched provided all faults are recorded after each flight. None required. Airplane may be dispatched with one (1) main TRU inoperative provided: a) Both Generators are operative, b) Both essential TRU’s are operative, c) Auxiliary TRU is operative, d) APU Generator is operative, e) Both Battery chargers are operative, f) Both Main Airplane Batteries are operative, g) Inoperative L MAIN TRU: LPDB, Left Main AC section or R MAIN TRU: RPDB, Right Main AC section TRU circuit breaker on the Power Distribution Box is pulled and collared, and h) Repairs are made within two (2) flight days. Flight crew will pull and collar inoperative TRU circuit breaker on Power Distribution Box. (Blue – Advisory) (GV) MN TRU FAULT, L-R 2 - 108 3. Limitations and/or Procedures (Blue – Advisory) (GV) MDAU MEM 90% FULL PAGE NO: A (O) Flight crew will ensure AUX TRU is operative and both essential TRUs are operative. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message MRC 1 Fail 2. A 2 - 109 3. Limitations and/or Procedures (Amber – Caution) (GV-SP/GIV-X) PAGE NO: Airplane may be dispatched with one (1) MRC failed, provided: a) Associated Comm and Nav radios and opposite ATC are operative, and b) Repairs are made within one (1) flight day. Operational Procedures None required. NOTE: EICAS blue messages “APM FAIL” and “ASCB FAIL” displayed. “ASCB FAIL” is only displayed in flight. MRC 2 Fail (Blue – Advisory) (GV-SP/GIV-X) A Airplane may be dispatched provided: a) Associated Comm and Nav radios and opposite ATC are operative, and b) Repairs are made within one (1) flight day. NOTE: With MRC 2 Fail, expect EICAS blue messages “APM FAIL” and “ASCB FAIL” displayed. “ASCB FAIL” will display inflight only. None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message NAV 2 Fail (Blue – Advisory) (GV) Operational Procedures B Airplane may be dispatched as required by 14 CFR. None required. B Airplane may be dispatched provided operations do not require its use. None required. A Except where en route operations or None required. approach minimums require its use, airplane may be dispatched provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, d) Both RFMUs are operative, and e) Repairs are made within two (2) flight days. (Blue – Advisory) (GV-SP/GIV-X) NMS 1-2 FAIL 2 - 110 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) NAVCOM Fail 2. PAGE NO: NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. One (1) system is required in PRNAV, BRNAV, RNAV 1 and RNAV 2 airspace. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message NMS FAIL 2. A 2 - 111 3. Limitations and/or Procedures (Blue – Advisory) (GV) PAGE NO: Operational Procedures Except where en route operations or None required. approach minimums require its use, airplane may be dispatched provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, d) Both RFMUs are operative, and e) Repairs are made within two (2) flight days. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. One (1) system is required in PRNAV, BRNAV, RNAV 1 and RNAV 2 airspace. NWS Fixed Gain B Airplane may be dispatched provided Nose Wheel Tiller Steering System is operative. None required. B Airplane may be dispatched provided Nose Wheel Tiller Steering System is operative. None required. (Blue – Advisory) (GV-SP/GIV-X) NWS FIXED GAIN (Blue – Advisory) (GV) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Outflow Valve Fault Airplane may be dispatched provided: a) DC motor is operative, and b) Airplane is operated in accordance with AFM Limitations. None required. B Airplane may be dispatched provided: a) DC motor is operative, and b) Airplane is operated in accordance with AFM Limitations. None required. Airplane may be dispatched with one (1) inoperative Autopilot Pitch Trim Servo provided PITCH TRIM SERVO #1: POP, E2 or PITCH TRIM SERVO #2, CPOP, E-1 circuit breaker is pulled and collared. Flight crew will ensure inoperative servo circuit breaker is pulled and collared. B (Blue – Advisory) (GV-SP/GIV-X) RAAS 1-2 Fail (Blue – Advisory) (GV-SP/GIV-X) Operational Procedures B (Blue – Advisory) (GV) Pitch Trim 1-2 Power Fail 2 - 112 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) OUTFLOW VLV FAULT PAGE NO: B (O) None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message RAD ALT 1-2 FAIL (Blue – Advisory) (GV-SP/GIV-X) 2 - 113 3. Limitations and/or Procedures Operational Procedures B Airplane may be dispatched provided: None required. a) Landing weather minimums or operating procedures do not require its use, and b) Other systems affected (E/GPWS, TCAS, Flight Director, Autopilot, Autothrottle, Altimeter Ground Awareness Display, Synthetic Vision Primary Flight Display, HUD Flare Cue) are considered. B Airplane may be dispatched provided: None required. a) Landing weather minimums or operating procedures do not require its use, and b) Other systems affected (E/GPWS, TCAS, Flight Director, Autopilot, Autothrottle, Altimeter Ground Awareness Display, Synthetic Vision Primary Flight Display, HUD Flare Cue) are considered. (Blue – Advisory) (GV) Radio Altimeter 1-2 Fail 2. PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message Rudder Steering Fail (Blue – Advisory) (GIV-X/GV-SP) Operational Procedures B Airplane may be dispatched provided: a) Nose Wheel Tiller Steering System is operative, and b) Left seat pilot performs the takeoff and landing task. None required. B Airplane may be dispatched provided: a) Nose Wheel Tiller Steering System is operative, and b) Left seat pilot performs the takeoff and landing task. None required. C Airplane may be dispatched provided procedures do not require their use. None required. (Amber – Caution) (GV) SATCOM Call 2 - 114 3. Limitations and/or Procedures (Amber – Caution) (GV-SP/GIV-X) RUDDER STRG FAIL 2. PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Service Door (Amber – Caution) (GV-SP/GIV-X) Operational Procedures B (O) Airplane may be dispatched provided a crewmember verifies by visual inspection before each departure that the associated door is CLOSED and LOCKED. Flight crew will visually inspect door(s) to ensure it is CLOSED and LOCKED prior to departure. B (O) Airplane may be dispatched provided a crewmember verifies by visual inspection before each departure that the associated door is CLOSED and LOCKED. Flight crew will visually inspect door(s) to ensure it is CLOSED and LOCKED prior to departure. Airplane may be dispatched. None required. (Blue – Advisory) (GV) Side Windshield Fail, L-R 2 - 115 3. Limitations and/or Procedures (Blue – Advisory) (GV-SP/GIV-X) SERVICE DOOR PAGE NO: B GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message STCK PUSH 1-2 FAULT (Amber – Caution) (GV) (O) 2 - 116 3. Limitations and/or Procedures A PAGE NO: Airplane may be dispatched with one (1) system inoperative provided: a) Angle of Attack indication is available on both PFD’s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled by pulling and collaring the Stall Barrier Valve and Stick Shaker associated with the failed system, d) Crew procedures in the event the remaining stall barrier fails are discussed, e) If the remaining stall barrier fails the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight (this minimum speed shall be cross referenced to a normalized AOA value of 0.59 as displayed on the PFD), f) Weather at departure and destination is considered, g) Consideration is given to delaying takeoff or approach and landing, if windshear is forecast until such conditions cease, or consideration is given to proceeding to alternate, and h) Repairs are made within two (2) flight days. Operational Procedures Flight crew will pull and collar the circuit breakers for the Stall Barrier Valve and Stick Shaker associated with the failed system. Prior to dispatch, the flight crew will discuss the dispatch situation with the stall barrier inoperative and crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be cross-referenced to Normalized Angle of Attack of 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear conditions at the departure or destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist, or consider deviation to an alternate airport in the approach and landing case. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message STCK PUSH 1-2 FL (Amber – Caution) (GV) (O) 2 - 117 3. Limitations and/or Procedures A PAGE NO: Airplane may be dispatched with one (1) system inoperative provided: a) Angle of Attack indication is available on both PFD’s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled by pulling and collaring the Stall Barrier Valve and Stick Shaker associated with the failed system, d) Crew procedures in the event the remaining stall barrier fails are discussed, e) If the remaining stall barrier fails the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight (this minimum speed shall be cross referenced to a normalized AOA value of 0.59 as displayed on the PFD), f) Weather at departure and destination is considered, g) Consideration is given to delaying takeoff or approach and landing, if windshear is forecast until such conditions cease, or consideration is given to proceeding to alternate, and h) Repairs are made within two (2) flight days. Operational Procedures Flight crew will pull and collar the circuit breakers for the Stall Barrier Valve and Stick Shaker associated with the failed system. Prior to dispatch, the flight crew will discuss the dispatch situation with the stall barrier inoperative and crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be cross-referenced to Normalized Angle of Attack of 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear conditions at the departure or destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist, or consider deviation to an alternate airport in the approach and landing case. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Stick Push 1-2 Fail (Amber – Caution) (GV-SP/GIV-X) (O) 2 - 118 3. Limitations and/or Procedures A PAGE NO: Airplane may be dispatched with one (1) system inoperative provided: a) Angle of Attack indication is available on both PFD’s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled by pulling and collaring the Stall Barrier Valve and Stick Shaker associated with the failed system, d) Crew procedures in the event the remaining stall barrier fails are discussed, e) If the remaining stall barrier fails the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight (this minimum speed shall be cross referenced to a normalized AOA value of 0.59 as displayed on the PFD), f) Weather at departure and destination is considered, g) Consideration is given to delaying takeoff or approach and landing, if windshear is forecast until such conditions cease, or consideration is given to proceeding to alternate, and h) Repairs are made within two (2) flight days. Operational Procedures Flight crew will pull and collar the circuit breakers for the Stall Barrier Valve and Stick Shaker associated with the failed system. Flight crew will discuss crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be crossreferenced to Normalized Angle of Attack of 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear conditions at the departure or destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist, or consider deviation to an alternate airport in the approach and landing case. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Stick Push 1-2 Fault (Amber – Caution) (GV-SP/GIV-X) (O) 2 - 119 3. Limitations and/or Procedures A PAGE NO: Airplane may be dispatched with one (1) system inoperative provided: a) Angle of Attack indication is available on both PFD’s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled by pulling and collaring the Stall Barrier Valve and Stick Shaker associated with the failed system, d) Crew procedures in the event the remaining stall barrier fails are discussed, e) If the remaining stall barrier fails the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight (this minimum speed shall be cross referenced to a normalized AOA value of 0.59 as displayed on the PFD), f) Weather at departure and destination is considered, g) Consideration is given to delaying takeoff or approach and landing, if windshear is forecast until such conditions cease, or consideration is given to proceeding to alternate, and h) Repairs are made within two (2) flight days. Operational Procedures Flight crew will pull and collar the circuit breakers for the Stall Barrier Valve and Stick Shaker associated with the failed system. Prior to dispatch, the flight crew will discuss the dispatch situation with the stall barrier inoperative and crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be cross-referenced to Normalized Angle of Attack of 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear conditions at the departure or destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist, or consider deviation to an alternate airport in the approach and landing case. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message STICK PUSH UNAVAIL (Amber – Caution) (GV) (O) 2 - 120 3. Limitations and/or Procedures A PAGE NO: Airplane may be dispatched with one (1) system inoperative provided: a) Angle of Attack indication is available on both PFD’s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled by pulling and collaring the Stall Barrier Valve and Stick Shaker associated with the failed system, d) Crew procedures in the event the remaining stall barrier fails are discussed, e) If the remaining stall barrier fails the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight (this minimum speed shall be cross referenced to a normalized AOA value of 0.59 as displayed on the PFD), f) Weather at departure and destination is considered, g) Consideration is given to delaying takeoff or approach and landing, if windshear is forecast until such conditions cease, or consideration is given to proceeding to alternate, and h) Repairs are made within two (2) flight days. Operational Procedures Flight crew will pull and collar the SHAKER #1: POP E-6, SHAKER #2: CPOP E-6, STALL BARR VALVE #1: POP E-5, STALL BARR VALVE #2: CPOP E-5, FLAP/STAB LEFT DC: POP C-6 or FLAP / STAB RIGHT DC: CPOP C-6 circuit breakers for the Stall Barrier Valve and Stick Shaker associated with the failed system. Prior to dispatch, the flight crew will discuss the dispatch situation with the stall barrier inoperative and crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be cross-referenced to Normalized Angle of Attack of 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear conditions at the departure or destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist, or consider deviation to an alternate airport in the approach and landing case. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Stick Push Unavailable (Amber – Caution) (GV-SP/GIV-X) (O) 2 - 121 3. Limitations and/or Procedures A PAGE NO: Airplane may be dispatched with one (1) system inoperative provided: a) Angle of Attack indication is available on both PFD’s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled by pulling and collaring the Stall Barrier Valve and Stick Shaker associated with the failed system, d) Crew procedures in the event the remaining stall barrier fails are discussed, e) If the remaining stall barrier fails the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight (this minimum speed shall be cross referenced to a normalized AOA value of 0.59 as displayed on the PFD), f) Weather at departure and destination is considered, g) Consideration is given to delaying takeoff or approach and landing, if windshear is forecast until such conditions cease, or consideration is given to proceeding to alternate, and h) Repairs are made within two (2) flight days. Operational Procedures Flight crew will pull and collar the SHAKER #1: POP E-6, SHAKER #2: CPOP E-6, STALL BARR VALVE #1: POP E-5, STALL BARR VALVE #2: CPOP E-5, FLAP/STAB LEFT DC: POP C-6 or FLAP / STAB RIGHT DC: CPOP C-6 circuit breakers for the Stall Barrier Valve and Stick Shaker associated with the failed system. Prior to dispatch, the flight crew will discuss the dispatch situation with the stall barrier inoperative and crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be cross-referenced to Normalized Angle of Attack of 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear conditions at the departure or destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist, or consider deviation to an alternate airport in the approach and landing case. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message Stick Shake 1-2 Fail (Blue – Advisory) (GV) 2 - 122 3. Limitations and/or Procedures Operational Procedures A Airplane may be dispatched with a single None required. control column shaker inoperative provided: a) Angle of Attack indication is available on both PFD’s, b) Both stall barrier systems are operative, and c) Repairs are made within two (2) flight days. A Airplane may be dispatched with a single None required. control column shaker inoperative provided: a) Angle of Attack indication is available on both PFD’s, b) Both stall barrier systems are operative, and c) Repairs are made within two (2) flight days. (Blue – Advisory) (GV-SP/GIV-X) STICK SHAKE 1-2 FL 2. PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Stuck MIC ACP 3 (Blue – Advisory) (GV-SP/GIV-X) (continued) (O) 2 - 123 3. Limitations and/or Procedures A PAGE NO: Airplane may be dispatched with ACP 3 indicating stuck MIC provided: a) Pilot and Copilot ACP’s are operative, b) OBSERVER ACP: REER, D-7, is pulled and collared, c) Affected ACP is not required as determined by the Pilot-in-Command, d) Flight Deck to cabin communication is operative, e) A passenger seat in the passenger cabin is made available to an FAA inspector for the performance of official duties, f) Alternate procedures are established and used, g) Required minimum safety equipment (safety belt and oxygen) is available, h) Seat is acceptable to the FAA inspector for performance of official duties, and i) Repairs are made within two (2) flight days. Operational Procedures Flight crew will ensure: a) Pilot and Copilot ACP’s are operative, b) OBSERVER ACP: REER D7, is pulled and collared, c) Affected ACP is not required as determined by the Pilotin-Command, d) Flight Deck to cabin communication is operative, and e) Alternate procedures are established and used. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Stuck MIC ACP 3 2 - 124 3. Limitations and/or Procedures A PAGE NO: Operational Procedures NOTE 1: These provisos are intended to provide for occupancy of the above seats by an FAA inspector when the minimum safety equipment (oxygen and safety belt) is functional and the inspector determines the condition to be acceptable. (Blue – Advisory) (GV-SP/GIV-X) (cont’d) NOTE 2: The pilot-in-command will determine if the minimum safety equipment is functional for other persons authorized to occupy any observer seat(s). S WSHLD FAIL, L-R B Airplane may be dispatched. None required. Airplane may be dispatched provided: a) System is deactivated and secured by pulling and collaring TCAS: POP, F-2 circuit breaker, b) En route or approach procedures do not require its use, and c) Repairs are made within two (2) flight days. Flight crew will ensure: a) System is deactivated and secured by pulling and collaring TCAS Power CB, and b) En route or approach procedures do not require its use. (Amber – Caution) (GV) TCAS Fail (Blue – Advisory) (GV-SP/GIV-X) A (O) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message TCAS FAIL A Terrain 1-2 Fail B (Blue – Advisory) (GV-SP/GIV-X) Terrain Bus Fail (Blue – Advisory) (GV-SP/GIV-X) (O) 2 - 125 3. Limitations and/or Procedures (Blue – Advisory) (GV) PAGE NO: Operational Procedures Airplane may be dispatched provided: a) System is deactivated and secured by pulling and collaring TCAS: POP, F-2 circuit breaker, b) En route or approach procedures do not require its use, and c) Repairs are made within two (2) flight days. Flight crew will ensure: a) System is deactivated and secured by pulling and collarin TCAS Power CB, and b) En route or approach procedures do not require its use. Airplane may be dispatched. None required. NOTE: Synthetic Vision PFD synthetic terrain will not be available with dual Terrain Server failures, but the full PFD may be used without restriction. B Airplane may be dispatched. NOTE: Synthetic Vision PFD synthetic terrain will not be available with dual Terrain Server failures, but the full PFD may be used without restriction. None required. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. CAS Message THROT QUAD 1-2 FL B B (Blue – Advisory) (GV) None required. Airplane may be dispatched. None required. NOTE: With both Channel 1 and Channel 2 failed, the autothrottle system will be inoperative. C Airplane may be dispatched with any in excess of those required by 14 CFR. None required. C Airplane may be dispatched with any in excess of those required by 14 CFR. None required. (Blue – Advisory) (GV-SP/GIV-X) VHF COMM 1-2 FAIL Airplane may be dispatched. Operational Procedures NOTE: With both Channel 1 and Channel 2 failed, the autothrottle system will be inoperative. (Blue – Advisory) (GV-SP/GIV-X) VHF COM 1-2 Fail 2 - 126 3. Limitations and/or Procedures (Blue – Advisory) (GV) Throttle Quadrant 1-2 Fail 2. PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message WG A/I SYS FL, L-R B 2 - 127 3. Limitations and/or Procedures Except for ER operations, airplane may be dispatched with wing anti-ice system inoperative provided airplane is not operated in known or forecast icing conditions. (Amber – Caution) (GV) PAGE NO: Operational Procedures None required. NOTE: Do not select affected side Wing Anti-Ice to ON. Windshear 1-2 Fail (Blue – Advisory) (GV-SP/GIV-X) A (O) Airplane may be dispatched provided: a) At least one (1) radio altimeter is operative, b) Alternate procedures are established and used, c) Flight crew comply with AFM/AOM guidance in windshear situations and recommend procedures when encountering windshear, and d) Repairs are made within two (2) flight days. NOTE: Operator’s alternate procedures should include reviewing windshear avoidance and windshear recovery procedures. Flight crew will comply with AFM/AOM guidance in windshear situations and recommend procedures when encountering windshear and verify both radio altimeters are valid. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message WINDSHEAR FAIL (Blue – Advisory) (GV) (O) 2 - 128 3. Limitations and/or Procedures A PAGE NO: Airplane may be dispatched provided: a) At least one (1) radio altimeter is operative, b) Alternate procedures are established and used, c) Flight crew comply with AFM/AOM guidance in windshear situations and recommend procedures when encountering windshear, and d) Repairs are made within two (2) flight days. NOTE: Operator’s alternate procedures should include reviewing windshear avoidance and windshear recovery procedures. Operational Procedures Flight crew will comply with AFM/AOM guidance in windshear situations and recommend procedures when encountering windshear and verify both radio altimeters are valid. GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message Wing Anti-Ice Sys Fail, L-R B 2 - 129 3. Limitations and/or Procedures Except for ER operations, airplane may be dispatched with wing anti-ice system inoperative provided airplane is not operated in known or forecast icing conditions. (Amber – Caution) (GV-SP/GIV-X) PAGE NO: Operational Procedures None required. NOTE: Do not select affected side Wing Anti-Ice to ON. Yaw Damper 1-2 Fail B (O) Except for ER operations, airplane may be dispatched with one (1) channel inoperative provided airplane is operated in accordance with AFM Limitations in the event the operative Yaw Damper fails. Flight crew will ensure airplane is operated in accordance with AFM Limitations in the event the operative Yaw Damper fails. B (O) Except for ER operations, airplane may be dispatched with one (1) channel inoperative provided airplane is operated in accordance with AFM Limitations in the event the operative Yaw Damper fails. Flight crew will ensure airplane is operated in accordance with AFM Limitations in the event the operative Yaw Damper fails. (Amber – Caution) (GV-SP/GIV-X) YD 1-2 FAIL (Amber – Caution) (GV) GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message YD 1-2 Fail (Blue – Advisory) (GV-SP/GIV-X) 2 - 130 3. Limitations and/or Procedures Operational Procedures B (O) Airplane may be dispatched with one inoperative yaw damper system provided the inoperative YAW DAMPER SERVO #1: POP, D-6 or YAW DAMPER SERVO #2: CPOP, D-6 circuit breaker is pulled and collared. Flight crew will ensure inoperative servo circuit breaker is pulled and collared. C (O) Airplane may be dispatched provided: a) L FREQ CONV: Left PDB or R FREQ CONV: Right PDB circuit breaker is pulled and collared, b) Flight crew brief passengers on items that are inoperative with the failure of the power source for cabin entertainment, and c) Backup battery is available if EFB is used. Flight crew will pull and collar affected circuit breaker. Flight crew will brief the passengers on the items that are inoperative with the failure of the power source for cabin entertainment. (Blue – Advisory) (GV-SP/GIV-X) 50 HZ Power Fail, L-R PAGE NO: GULFSTREAM AEROSPACE CORPORATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) REVISION NO: 8 DATE: 11/07/2014 1. 2. CAS Message 60 HZ Power Fail, L-R (Blue – Advisory) (GV) 2 - 131 3. Limitations and/or Procedures Operational Procedures C (O) Airplane may be dispatched provided: a) Affected L FREQ CONV: Left PDB or R FREQ CONV: Right PDB circuit breaker is pulled and collared, b) Flight crew brief passengers on items that are inoperative with the failure of the power source for cabin entertainment, and c) Backup battery is available if EFB is used. Flight crew will pull and collar affected circuit breaker. Flight crew will brief the passengers on the items that are inoperative with the failure of the power source for cabin entertainment. C (O) Airplane may be dispatched provided: a) Affected L FREQ CONV: Left PDB or R FREQ CONV: Right PDB circuit breaker is pulled and collared, b) Flight crew brief passengers on items that are inoperative with the failure of the power source for cabin entertainment, and c) Backup battery is available if EFB is used. Flight crew will pull and collar affected circuit breaker. Flight crew will brief the passengers on the items that are inoperative with the failure of the power source for cabin entertainment. (Blue – Advisory) (GV-SP/GIV-X) 60HZ PWR FAIL, L-R PAGE NO: GULFSTREAM AEROSPACE CORPORATION P.O. Box 2206, Savannah, Georgia 31402-2206 Telephone (912) 965-3000 Telex 3772775
