Mil Mi-34

The Mil Mi-34 is a light helicopter designed by the Mil Moscow Helicopter Plant in either a two or four seat configuration for utility and training. It was first flown in 1986 and introduced to the world at the Paris Air Show in 1987. The Mi-34 entered production in 1993 and is capable of performing aerobatic maneuvers including rolls and loops.

The Mil Mi-34 is a newer much improved version of the Mil Mi-24 to meet the Russian military's requirement for a more powerful 1

Made by Mil Moscow Helicopter Plant.

The Mil Mi-34 is a light helicopter designed by the Mil Moscow Helicopter Plant in either a two or four seat configuration for utility and training.2
Height Main
2.75 m
Height Alt
9
Length Alt
37
Max Takeoff Weight Main
1450.0
Jet Or Prop
prop
Range Main
356.0
Max Speed Alt
7800.0
Max Speed Main
210.0
Introduction
1993
Capacity
2
Status
in production
Cruise Speed Main
170.0
Max Takeoff Weight Alt
3196.0
Ceiling Main
4
000 m
Type Of Prop
nine-cylinder air-cooled radial engine
Crew
1
Unit Cost
1000000.0
350000.0
US $1 million
US$350
000
Cruise Speed Alt
6360.0
Area Main
78.70 m²
Span Alt
32
Plane Or Copter?
copter
Power Alt
320 hp
Engine(prop)
Vedeneyev M14P
Manufacturer
Mil Moscow Helicopter Plant
Number Of Props
1
First Flight
1986
Origin
Russia
Soviet Union
National Origin
Russia
Soviet Union
Span Main
10.00 m
Power Main
239.0
Production Start Year
1994
Empty Weight Alt
2094.0
Length Main
11.415 m
Area Alt
847.1
Range Alt
13260.0
Similar Aircraft
* Enstrom 280* Robinson R44* Bell Helicopter 206* MD Helicopters MD 500* PZL SW-4* Kazan Ansat
Empty Weight Main
950.0
Ceiling Alt
13120.0
Produced
1994
Category
Helicopters
Mil aircraft
Soviet civil trainer aircraft 1980-1989

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