Russian light helicopter
Mi-34
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A Mil Mi-34
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Role
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Helicopter Type of aircraft
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National origin
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Soviet Union / Russia
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Manufacturer
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Mil Helicopters
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First flight
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17 November 1986
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Introduction
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1993
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Status
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out of production
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Produced
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1986–2011
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Number built
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27
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The Mil Mi-34 (NATO reporting name: Hermit) 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 on 17 November 1986 and introduced at the Paris Air Show in 1987. The Mi-34 entered production in 1993, and is capable of performing aerobatic manoeuvres, including rolls and loops.
Specifications (Mi-34S)
Data from 'Jane's All The World's Aircraft 2000–2001 [5]
General characteristics
- Crew: 1 or 2
- Capacity: 2 pax
- Length: 11.415 m (37 ft 5 in) overall
- 8.71 m (29 ft) fuselage
- Height: 2.75 m (9 ft 0 in)
- Empty weight: 950 kg (2,094 lb)
- Gross weight: 1,280 kg (2,822 lb) normal
- 1,100 kg (2,425 lb) aerobatic
- Max takeoff weight: 1,450 kg (3,197 lb)
- Fuel capacity: 176 L (46 US gal; 39 imp gal) / 128 kg (282 lb)
- Powerplant: 1 × Vedeneyev M-14V-26V 9-cylinder air-cooled radial piston engine, 239 kW (321 hp)
- Main rotor diameter: 10 m (32 ft 10 in)
- Main rotor area: 78.7 m2 (847 sq ft)
Performance
- Maximum speed: 210 km/h (130 mph, 110 kn)
- Cruise speed: 170 km/h (110 mph, 92 kn)
- Best climb speed: 90 km/h (56 mph; 49 kn)
- Range: 356 km (221 mi, 192 nmi) with maxfuel at 500 m (1,600 ft) and 5% reserve
- Service ceiling: 4,000 m (13,000 ft) *Hover ceiling OGE: 900 m (3,000 ft)
- g limits: +3
- Disk loading: 18.4 kg/m2 (3.8 lb/sq ft)
- Power/mass: 0.165 kW/kg (0.100 hp/lb)