Overview
The Mil Mi-38 is a medium-lift helicopter developed as a successor to earlier Mil transport models. Designed for civil and military roles, it incorporates updated engines and avionics. The aircraft entered limited service in the late 2010s.
Live Fleet Activity (MI38)
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Specifications
Units
- Engine
- 2 × Klimov TVA-3000
- Engine type
- Turboshaft
- Power
- 2 × 2,465 shp · 1,838 kW
- Avionics
- Integrated Tactical System (FITS)
- Wing tips
- No winglets
- Seats
- 3
- Crew
- —
- Cabin width
- 7 ft 9 in · 2.36 m
- Cabin height
- 5 ft 11 in · 1.80 m
- Cabin length
- 23 ft 0 in · 7.00 m
- Exterior length
- 65 ft 5 in · 19.95 m
- Tail height
- 22 ft 8 in · 6.90 m
- Fuselage diameter
- 8 ft 8 in · 2.65 m
- Wing span
- 69 ft 3 in · 21.10 m
- Baggage volume
- 1,042 ft³ · 29.5 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 34,400 lb · 15,600 kg
- Max landing weight
- —
- Max payload
- 13,200 lb · 6,000 kg
- Fuel capacity
- 1,040 gal · 3,900 L · 3,100 kg (Jet A)
- Max cruise speed
- 162 kt · 186 mph · 300 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 477 nm · 550 mi · 880 km
- Fuel burn
- —
- Ceiling
- 21,300 ft · 6,500 m
- Rate of climb
- 1,810 ft/min · 9 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery
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Live fleet activity details
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