| Technical data | |
|---|---|
| Type | AIR-11 |
| Function | General purpose |
| Year | 1936 |
| Crew | 1 |
| Engines | 120hp Gypsy-Major |
| Length | 7.32m |
| Wingspan | 10.2m |
| Wing area | 16.8m2 |
| Empty weight | 566kg |
| Loaded weight | 891kg |
| Wing Load (kg/m2) | 53.0 |
| Power load (kg/hp) | 7.4 |
| Maximum Speed | 209km/h |
| Landing Speed | 82km/h |
| Landing Roll | 340m 30sec |
| Takeoff Roll | 200m 16sec |
| Range | 720km |
| Flight Endurance | 4.5h |
| Ceiling | 4480m |
| Climb | |
| 1000m | 5.2min |
| 3000m | 21.6min |
| Payload | |
| Fuel + Oil | 80+14kg |
| Seats | 2 |
| Cargo | ?kg |
AIR-11 and AIR-16 by A.S.Yakovlev
AIR-11 was a 3-seat tourist version of AIR-10. Tourist aircraft with enclosed cockpit and 120hp Gypsy-Major engine. Built in 1936 and succeeded in state test flight, but couldn't enter production because of lack of good domestic engine.
S.V.Ilyushin crashed on this a/c flying from Voronezh to Moscow due to a fault of mechanic, who forgot to fill the oil tank. In 1937 almost identical four-seater AIR-16 was built (for 220hp Renault engine). It was rolled out to the airfield, but never flew... Yakovlev failed to acquire the engine.
| Predecessors | Modifications |
|---|---|
 AIR-10 |
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