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Mi-17

Mi-17P is a single-rotor helicopter with five-lobed three-hinged main rotor and three-lobed steering rotor. Unlike in Mi-8P, the steering rotor is mounted on the left side to act as a pusher. The tricycle landing gear is non-retractable, and is equipped with castor nose wheel locked in-flight. The steering rotor is protected by a tail crutch. The power unit consists of 2 turboprop engines TV3-117VM with VR-14 and VSU AI-9V main rotor transmission. The power unit is equipped with automatic main rotor revolution regulation system and engine synchronizing system. Engine air inlets are equipped with dust protectors. 26 soft passenger seats are available in Mi-17P cabin.

 

Specification

Maximum takeoff gross weight

13000 kg

Service ceiling

6000 m

Crew

2 persons

Power units

2 х TV3-117VM

Takeoff power

2 х 2000

Speed

Peak speed on the deck

250 km/h

Cruising speed

230 km/h

Dimensions

Overall length

25.31 m

Overall height

5.54 m

Main rotor diameter

21.29 m

Passenger compartment width

2.34 m

Passenger compartment height

1.8 m


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