In numbers Through the lens Video
An-26A was developed on the basis of An-24 and is intended only for air-mission landing, in 1971, only one aircraft was converted. An-26Sh is a training aircraft for training cadets - navigators. A total of 36 units were produced.
Technical specifications
| DESIGNER | Antonov |
| COUNTRY | Russia, Ukraine |
| TYPE | Military transport aircraft |
| CREW | 3 |
| POWER-PLANT | Two turboprop engines ΑΙ-24VT |
| Power h.p | 2x2.820 |
| Booster engine | One jet engine (backup system) Tumansky, RU-19A-300 |
| Thrust, kN (kgf) | 7,85 (800) |
| DIMENSIONS | |
| Length, m | 23.80 |
| Height, m | 8,58 |
| Wing span, m | 29,90 |
| Wing area, m2 | 74,98 |
| WEIGHT | |
| Maximum take-off, kg | 23.800 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 15.020 |
| Internal fuel, kg | 2.760 |
| Payload, kg | |
| - student | 10 |
| - instructor | 1 |
| PERFORMANCE | |
| Maximum speed, km/h | - |
| Cruising speed, km/h | 400 |
| Service ceiling, m | 7.500 |
| Range, km | 2.600 |
| Combat range, km | - |
| ARMAMENT | Doesn't have (defensive). |