AIR-6A, A.S.Yakovlev
| Technical data | ||||||
|---|---|---|---|---|---|---|---|
| Type | AIR-6A | ||||||
| Function | Floatplane | ||||||
| Year | 1933 | ||||||
| Crew | 1 | ||||||
| Engines | 1*100hp M-11 | ||||||
| Length | 8.0m | ||||||
| Wingspan | 12.0m | ||||||
| Wing area | 19.8m2 | ||||||
| Empty weight | 668kg | ||||||
| Loaded weight | 958kg | ||||||
| Wing load | 48.4kg/m2 | ||||||
| Power load | 9.6kg/hp | ||||||
| Speed at 0m | 150km/h | ||||||
| Landing Speed | 70km/h | ||||||
| Landing Roll | 150m | ||||||
| Takeoff Roll | 10sec | ||||||
| Turn time | 17sec | ||||||
| Range | 600/920km | ||||||
| Flight Endurance | 5h | ||||||
| Ceiling | 3000km | ||||||
| Payload | |||||||
| Seats | 2-3 | ||||||
| Modified February 9, 1998
by Alexandre Savine; |
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