Kazan Mi-17

The transport helicopter built for rugged operations worldwide.

Overview

Kazan Russia ICAO: MI17 2005–Present $17.9 million

The Kazan Mi-17 is a widely used transport helicopter derived from the Mi-8 family. Introduced in the 1970s, it has become one of the most produced helicopters globally. The aircraft is known for durability and payload capacity.

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Specifications

Units
Engine
—
Engine type
-
Power
1,950 hp · 1,454 kW
Avionics
—
Wing tips
No winglets
Seats
36 economy · 26 business · 11 first
Crew
—
Cabin width
7 ft 8 in  ·  2.34 m
Cabin height
5 ft 11 in  ·  1.80 m
Cabin length
17 ft 6 in  ·  5.34 m
Exterior length
60 ft 7 in  ·  18.47 m
Tail height
18 ft 6 in  ·  5.65 m
Fuselage diameter
8 ft 2 in  ·  2.50 m
Wing span
69 ft 11 in  ·  21.30 m
Baggage volume
—
Gross weight
—
Empty weight
—
Max takeoff weight
28,700 lb  ·  13,000 kg
Max landing weight
—
Max payload
8,800 lb  ·  4,000 kg
Fuel capacity
980 gal · 3,700 L · 3,000 kg (Jet A)
Max cruise speed
124 kt  ·  143 mph  ·  230 km/h
Maximum speed
—
Cruise speed
—
Approach speed
—
Range
251 nm  ·  290 mi  ·  460 km
Fuel burn
0.45 nm/gal  ·  0.22 km/L
Ceiling
19,685 ft  ·  6,000 m
Rate of climb
1,575 ft/min  ·  8 m/s
Takeoff distance
—
Landing distance
—
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Afghan Mi-17

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Operational Context

Kazan Mi-17 — medium twin-engine transport helicopter

The Mi-17 first flew in the late 1970s as an export-oriented development of the Mi-8. It features a conventional main rotor and tail rotor configuration. The helicopter is optimized for cargo and troop transport in demanding environments.

Two turboshaft engines producing approximately 1,900 shaft horsepower each power the aircraft. Cruise speed approaches 140 knots (259 km/h). Maximum takeoff weight exceeds 28,000 pounds (12,700 kg), with substantial internal and external load capability.

The Mi-17 has served in military, humanitarian, and commercial roles worldwide. Its ability to operate from austere locations has made it highly adaptable. Production continues in modernized forms.