Technical specifications 
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TECHNICAL SPECIFICATIONS
| DESIGNER | OKB Yakovlev |
| COUNTRY | Russia |
| TYPE | Short-range Bomber |
| CREW | 2-3 |
| POWER-PLANT | Two reciprocating motor M-103 |
| Power, h.p | 2 x 1.100 |
| DIMENSIONS | |
| Length, m | 10,18 |
| Height, m | - |
| Wing span, m | 14,00 |
| Wing area, m2 | 29,40 |
| WEIGHT | |
| Normal take-off, kg | 5.845 |
| Empty aircraft, kg | 4.000 |
| Maximum take-off, kg | - |
| Internal fuel, kg | - |
| PERFORMANCE | |
| Maximum speed, km/h | 574 |
| Cruising speed, km/h | 545 |
| Max speed in low height, km/h | - |
| Rate of climb, m/min | 920 |
| Service ceiling, m | 9.500-10.000 |
| Range, km | 960-1.200 |
| Combat range, km | - |
| ARMAMENT | Two-three 7,62 mm machine-gun ShKAS, up to 400-800 kg bombs. |
