In numbers Through the lens Video
Trainer helicopter Mi-24D. Without firearm. This modification had a dual (parallel) flight control and navigation system.
Technical specifications
| DESIGNER | OKB Mil |
| COUNTRY | Russia |
| TYPE |
Multipurpose assault helicopter
|
| CREW | 2 + 1 (optionally) |
| POWER-PLANT | Two turboshaft engines Klimov TV3-117 |
| Power, h.p. | 2x2.200 |
| DIMENSIONS | |
| Length, m | 21,50 |
| Main rotor diameter, m | 17,30 |
| Tail rotor diameter, m | 3,91 |
| Height, m | - |
| Wing span, m | 6,66 |
| WEIGHT | |
| Maximum take-off, kg | 11.500 |
| Normal take-off, kg | 11.100 |
| Empty, kg | 8.340 |
| Internal fuel, l | - |
| Weight of transported fuel with external tanks, l | - |
| Warload, kg | up to 2.400 |
| Payload, kg | |
| - soldier | 8 |
| - stretcher | 4 |
| - freight in cabin | 1.500 |
| - with on hook | 2.000 |
| PERFORMANCE | |
| Maximum speed, km/h | 320 |
| Cruising speed, km/h | 270 |
| Range, km | - |
| Ferry range, km | 1.125 |
| Combat range, km | 595 |
| Service ceiling, m | 4.500 |
| Static ceiling, m | 1.300 |
| Rate of climb, m/s | - |
| Maximum overload, g | - |
| ARMAMENT | Number external hardpoints: 6. Transportation of weapons: up to 4x Anti-tank missile 9Μ17P Falanga-PV, 4 launcher UB-32A-24 (unguided missiles S-5M1, S-5MO, S-5KBP, S-5KO or S-5-0), 8xOFAB-100, 4xOFAB-250, 4xRBK-250, 2xRBK-500, 2xKMGU-2, 2xODAB-500, 2x3B-500. |