In numbers Through the lens Video
In 1995, the Mi-26T obtained a IAC Aviaregister certificate under the FAR-29 and was redesignated as Mi-26TC.
Technical specifications
| DESIGNER | OKB Mil |
| COUNTRY | Russia |
| TYPE |
Multipurpose transport helicopter
|
| CREW | 5 |
| POWER-PLANT | Two turboshaft engines Progress D-136 |
| Power, h.p. | 2x11.393 |
| DIMENSIONS | |
| Length, m | 33,73 |
| Main rotor diameter, m | 32,00 |
| Tail rotor diameter, m | 7,61 |
| Height, m | 8,15 |
| WEIGHT | |
| Maximum take-off, kg | 56.000 |
| Normal take-off, kg | 49.600 |
| Empty, kg | 28.200 |
| Internal fuel, kg | - |
| Warload, kg | - |
| Payload, kg | |
| - number of soldiers | up to 70 |
| - VIP | 20 |
| - stretcher | 60 |
| - freight in cabin | 20.000 |
| - with on hook | 18.500 |
| PERFORMANCE | |
| Maximum speed, km/h | 295 |
| Cruising speed, km/h | 255 |
| Range, km | 2.000 |
| Ferry range, km | - |
| Combat range, km | - |
| Service ceiling, m | 6.500 |
| Static ceiling, m | 1.520 |
| Rate of climb, m/s | - |
| Maximum overload, g | - |
| ARMAMENT | Doesn't have (defensive). |
Photos Mi-26TC
Video
Mi-26T © www.Redstar.gr (maximum take-off weight 57.000 kg!).