AmEagle American Eaglet
| American Eaglet | |
|---|---|
| Role | Ultralight sailplane |
| Manufacturer | AmEagle |
| Designer | Larry Haig |
| First flight | 19 November 1975 |
The AmEagle American Eaglet was a highly unorthodox
propeller
behind the cabin. Its first flight was on 19 November 1975, and by 1978, at least 250 sets of plans had been sold, with 12 aircraft reportedly completed.
Specifications
Data from Jane's All the World's Aircraft 1982-83[1]
General characteristics
- Crew: 1
- Length: 16 ft (4.9 m)
- Wingspan: 36 ft (11 m)
- Height: 3 ft (0.91 m)
- Wing area: 72 sq ft (6.7 m2)
- Aspect ratio: 18
- Empty weight: 160 lb (73 kg)
- Max takeoff weight: 360 lb (163 kg)
- Fuel capacity: 2 litres
- Powerplant: 1 × McCulloch MC-101B two-stroke, single-cylinder engine, 12.2 hp (9.1 kW)
- Propellers: 2-bladed
Performance
- Stall speed: 38 mph (61 km/h, 33 kn)
- g limits: +4.4/-2.2
- Rate of climb: 450 ft/min (2.3 m/s) at sea level
- Wing loading: 5 lb/sq ft (24 kg/m2)
See also
Aircraft of comparable role, configuration, and era
- Birdman TL-1
- Pterodactyl Ascender
- Eipper Quicksilver
- Mitchell U-2 Superwing
- Stanton Sunbird, a motor glider which utlised American Eaglet components
- Ultraflight Lazair
- Zenair Zipper
References
- ^ Taylor, John W. R., ed. (1982). Jane's All the World's Aircraft 1982-83. London: Jane's Publishing Company. p. 618.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- The Rigid Wing Web Site
- Gliding and Motorgliding International
 | This article on an aircraft of the 1970s is a stub. You can help Wikipedia by expanding it. |