| Technical data | |
|---|---|
| Type | AIR-5 |
| Function | Passenger |
| Year | 1931 |
| Crew | 1 |
| Engines | 1*200hp Wright |
| Length | 8.0m |
| Wingspan | 12.8m |
| Wing area | 23.0m2 |
| Empty weight | 812kg |
| Loaded weight | 1390kg |
| Wing Load (kg/m2) | 60 |
| Power load (kg/hp) | 6.9 |
| Speed at 0m | 193km/h |
| Landing Speed | 75km/h |
| Landing Roll | 100m |
| Takeoff Roll | 100m |
| Turn time | 13sec |
| Range | 1000km |
| Flight Endurance | 6h |
| Ceiling | 4275m |
| Climb | |
| 1000m | 6.5min |
| 3000m | 27min |
| Payload | |
| Seats | 4 to 5 |
AIR-5, A.S.Yakovlev
 |
High-wing passenger monoplane. Fuselage frame - wielded of steel tubes, front section covered with duralumin, central and tail sections - with fabric. In this aircraft A.S.Yakovlev took all possible of the high wing scheme with struts and fixed landing gear.
AIR-5 passed State Acceptance Trials in April 1932 at NII GVF.
Light aircraft took all possible from its scheme and powerplant. Performance was excellent, but it was not built in series because there were no suitable domestic 200hp engine at the time.
| Predecessor(s) | Modification(s) |
|---|---|
 AIR-4 Ya-4 |
 AIR-6 Ya-6 |
References:
