AISA GN
The AISA GN was a prototype four-seat autogyro developed in Spain between 1971 and 1982. it featured an extensively-glazed cabin fitted with a pusher engine and tricycle undercarriage. A separate tail fin was carried at the end of two booms mounted to stub wings. The prototype was developed with a 200 hp engine. The aircraft suffered from an extremely prolonged development, but finally took to the air on 20 July 1982. In September that year, however, it was damaged in an accident, and development was finally abandoned.
Summary from Wikipedia licensed under CC BY-SA.
- Manufacturer
- Aeronáutica Industrial S.A.
- Category
- Helicopters
- Country of origin
- Spain
- First flight
- 1982-07-20
- Length
- 6.5 m
Specifications
- Cruise speed
- 114 kt
- Max speed
- 130 kt
- Range
- 430 nm
- Service ceiling
- 12,000 ft
- Rate of climb
- 60 ft/min
- Max takeoff weight
- 3,086 lb
- Empty weight
- 2,156 lb
- Fuel capacity
- 40 US gal
- Powerplant
- Lycoming IO-540-K1A5
- Engines
- 1
- Seats
- 4
- Length
- 21.3 ft
- Wingspan
- 39 ft
- Height
- 10.5 ft
- Number built
- 1
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.