| Technical data | ||
|---|---|---|
| Type |
AIR-10 Ya-10 |
AIR-10 floatplane |
| Function | Sport | |
| Year | 1935 | 1937 |
| Crew | 2 | |
| Engines | 1*100hp M-11 | |
| Length | 6.80m | 7.65m |
| Wingspan | 10.2m | 10.2m |
| Wing area | 16.87m2 | 16.87m2 |
| Empty weight | 510kg | 624kg |
| Loaded weight | 820kg | 896kg |
| Wing Load (kg/m2) | 48.6 | 53.1kg |
| Power load (kg/hp) | 8.2 | 9.0 |
| Speed at 0m | 217km/h | 200km/h |
| Landing Speed | 70km/h | |
| Landing Roll | 120m 15sec |
- |
| Takeoff Roll | 100m 10sec |
- |
| Turn time | 9sec | - |
| Range | 950km | 700km |
| Flight Endurance | 4h30min | |
| Ceiling | 5700m | 3200m |
| Climb | ||
| 1000m | 4.8min | - |
| 3000m | 16min | - |
AIR-10 (Ya-10) by A.S.Yakovlev
|
Sport aircraft, close derivative of the AIR-9, without Townend ring and with open cockpits. First flight took place on July 11, 1935. Conclusion of the NII VVS was favorable, aircraft was recommended as a monoplane trainer to make a transition from the U-2 biplane to growing park of fast monoplane fighters (mostly the I-16).
Among suggestions of the military expertise were:
- increasing maximum load from 8g to 10g;
- lowering landing speed to 55km/h;
- adding flaps and trimmers;
- improving the pilots protection in case of nose-over;
Aircraft went into production as '20' with yet another major change - its mixed metal/wood construction was replaced by all-wood for easier production launch.
AIR-10 (same airplane) participated in contest of light aircraft in 1935 and 1936 winning the First Price and proving high performance and endurance during 5000km race Moscow - Gorky - Kazan - Sarapul - Perm - Sverdlovsk - Chelabinsk - Magnitogorsk - Kujbyshev - Saratov - Lugansk - Donetsk - Dnepropetrovsk - Kiev - Briansk - Moscow.
| Predecessors | Modifications | ||
|---|---|---|---|
| AIR-9 |
 AIR-12 |
 '20' Ya-20 UT-2 |
AIR-11 |
| References | Links |
|---|---|
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