| Technical data | |
|---|---|
| Type |
AIR-3 'Pionerskaya Pravda' |
| Function | trainer |
| Year | 1929 |
| Crew | 2 |
| Engines | 1*60hp 'Walter' |
| Length | 7.1m |
| Wingspan | 11.0m |
| Wing area | 16.5m2 |
| Empty weight | 392kg |
| Loaded weight | 762kg |
| Wing Load (kg/m2) | 46.3 |
| Power load (kg/hp) | 12.7 |
| Maximum Speed at 0m | 146km/h |
| Cruise Speed | 125km/h |
| Landing Speed | 66km/h |
| Takeoff Roll | 60m |
| Flight Endurance | up to 14h |
| Range | 1835km |
| Ceiling | 4200m |
| Climb | |
| 1000m | 6.0min |
|
Development of the AIR-2 in parasol monoplane configuration. It used fuselage, powerplant, landing gear and tail identical to the predecessor. Money for construction were provided by Osoaviakhim.
Aircraft was ready on Summer 1929. On September 6 same year pilots Filin and Kovalkov (at the time students of the VVA, as well as a designer) flew nonstop from Mineralnye Vody to Moscow covering 1835km with average speed 166.8km/h, setting another International Record for Yakovlev's aircraft.
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Drawing from the Virtual Aircraft Museum, used as a background for this page; |
| Predecessor(s) | Modification(s) |
|---|---|
![]() AIR-2 Ya-2 |
AIR-4 Ya-4 |
| Created April 30, 1995 Modified December 26, 2001 |
|
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