Falconar AMF-S14
From Wikipedia, the free encyclopedia
| AMF-S14 Maranda | |
|---|---|
| Type | Utility aircraft |
| Manufacturer | Homebuilt |
| Designed by | Chris Falconar |
| Maiden flight | 1961 |
The Falconar AMF-S14 Maranda is a two-seat light aircraft first flown in Canada in 1961 and marketed for homebuilding. Based on the Adam RA-14 Loisirs, it is a conventional high-wing strut-braced monoplane with fixed, tailwheel undercarriage. The pilot and single passenger sit side-by-side in a fully enclosed cabin.
[edit] Specifications (typical Super Maranda)
General characteristics
- Crew: One pilot
- Capacity: 1 passenger
- Length: 6.70 m (22 ft 0 in)
- Wingspan: 9.67 m (31 ft 9 in)
- Wing area: 14.7 m² (158 ft²)
- Empty weight: 500 kg (1,100 lb)
- Gross weight: 840 kg (1,850 lb)
- Powerplant: 1 × Lycoming O-320 four-cylinder horizontally-opposed air-cooled piston engine, 112 kW (150 hp)
Performance
- Cruising speed: 193 km/h (120 mph)
- Range: 770 km (480 miles)
[edit] References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions, 376.
- Plan vendor's website
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