MA-35 R912 Cagolite (Rock) delta-wing aircraft
Number of seats: 2 seats
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MA-35 R912 Cagolite (Rock) delta-wing aircraft
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Product Description
Technical parameters:
Number of seats: 2 seats
Aircraft weight (net weight): 240 kg
Aircraft weight (maximum load): 475 kg
Takeoff distance under maximum load: 31 m (hard surf)
(Takeoff distance under (soft field): 50 m
Climb speed at 43 mph: 8 m/s
Maximum overload at maximum takeoff weight: +6/-3
Maximum fuel carrying capacity: 100 liters
Tires: 15 x 6.0-6
Brakes: Matco hydraulic disc brakes on rear wheels
Aircraft weight: 195 kg
Engine type: Rotax 912
Horsepower: 80
Propeller: Composite 3-blade
Rescue system: BRS-6-1050 parachute (optional)
Aircraft dimensions: 2.6m long, 2.2m wide, 2.8m high
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