Download of a Lifetime - Helicopters International, LLC

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Transcript 
EXPERIENCE
e
m
i
t
e
f
i
of a L
DESCRIPTION
Rotor Brake
Empty weight
265 kg/ 580 lbs
Wheel Brakes
Max. GTOW
560 kg/ 1232 lbs
Rotor RPM Tachometer
Length
4550 mm/ 179 in
Landing Lights
Height
2850 mm/ 112 in
Electric Starter and Trim
Strobe and NAV lights
Prop. diameter
1,75 m/ 67 in
Rotor Diameter
8,5 m/ 29 ft
PERFORMANCE
Chord Diameter
0,21 m/ 8 in
Engine - D-Motor LF 26, 4-cylinder, 2700 cc, water
15l/ h; 4 gal/ h
Fuel consumption
Regular
Fuel Type
cooled
170 km/ h; 105 mph
Full Injection
Fuel System
35 km/ h; 22 mph
2x35 l/ 2x9.2 gal
Fuel Tank Capacity
95 hp
150 km/ h; 95 mph
Airframe Fuselage, landing gear, instrument panel,
tail and wheel pants from carbon
5 m/ s; 980 fpm
Propeller made of composite
3000 m/ 9000 ft
Rotor head produced by Niki
0 -70 m; 230 ft
Pre-rotator Capability
0 -20 m; 65 ft
200 - 220 RPM
4 h with 30 min reserve
12 Volt Power Outlet
Hydraulic System for the main gear
EQUIPMENT
Aluminum Rotor Blades
29”
Composite 4 Blade Propeller
Aircraft tires
Airspeed Indicator
Altimeter
Variometer
1 Year or 200h
Magnetic Compass
Niki Rotor Aviation Inc.
Address: 21, Industrial Area “Praveshki Hanove”
2161, Pravets, Bulgaria
Phone: +359 7133 30 47; Mobile: +359 887 310005
E-mail: [email protected]
www.nikiaviation.com
www.lightningautogyro.com
Helicopters International, LLC
Address: 17673, Marsh Road
Winter Garden, FL 34787
Phone: 407 453 5747
E-mail: [email protected]
www.helicoptersinternational.com
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