AIR-3, Ya-3, ' Pionerskaja Pravda' A.S.YakovlevD evelopment 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.
| 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 | 46.3kg/m2 | |||||
| Power load | 12.7kg/hp | |||||
| 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 | |||||
| Modified January 22, 1998
by Alexandre Savine; |
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