| Specifications |
|---|
| Country of Origin | Russia
|
| Builder |
|
| Role | ASK mine countermeasures and SAR amphibious helicopter
|
| Variants | - A is ASW
- B is MCm variant(unarmed)
|
| Similar Aircraft | AS 332L1 Super Puma
|
| Rotor diameter | 21.29m (69ft 11in)
|
| Main rotor disc area | 356.0m^2 (3832.1sq ft).
|
| Length overall rotors turning | 25.3m (83ft 0in)
|
| fuselage length | 18.38m (60ft 4in)
|
| Height | 6.93m (22ft 9in)
|
| Empty | 8900kg (19,625lb)
|
| max takeoff | 14,000kg (30,865lb).
|
| Payload | 2000 kg
|
| Engine | Mi-14PL - Two 1397kW (1874shp) Klimov (Isotov) TV3-117MT turboshafts driving a five blade main rotor and three blade tail rotor.
|
| Maximum speed | 230km/h (125kt)
|
| max Cruising speed | 215km/h (116kt)
|
| economical Cruising speed | 205km/h (110kt)
|
| Cruise range | 432 nm
|
| Range with max fuel | 1135km (612nm).
|
| Endurance | 5hr 55min.
|
| Service Ceiling | 3500-5000 m
|
| Max initial rate of climb | 1535ft/min
|
| Time to 3280ft | 2min 18sec.
|
| Armament | E45-75A torpedoes or B-1, Nuclear depth charge in an enclosed weapons bay in the lower hull.
|
| Sensors | MAD, dipping sonar, 20 sonobuoys, Radar type Inicjatywa-2M
|
| Accommodation | . Mi-14PL has a crew of four. The Mi-14PS has a crew of three and can accommodate 10 rescued survivors in the main cabin including two on stretchers.
|
| Cost |
|
| User Countries | Bulgaria, Cuba, Libya, Poland, Romania, Russia, Syria, Yugoslavia
|
