Overview
The Kamov Ka-62 is a twin-engine helicopter developed as a civil derivative of the Ka-60 program. Designed for offshore transport and corporate missions, it incorporates updated avionics and Western engine options. The aircraft represents an effort to compete in the international medium helicopter market.
Live Fleet Activity (KA62)
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Specifications
Units
- Engine
- 2 × Turbomeca Ardiden 3G
- Engine type
- Turboshaft
- Power
- 2 × 1,776 shp · 1,324 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 16
- Crew
- —
- Cabin width
- 5 ft 9 in · 1.75 m
- Cabin height
- 4 ft 3 in · 1.30 m
- Cabin length
- 13 ft 5 in · 4.10 m
- Exterior length
- 51 ft 2 in · 15.60 m
- Tail height
- 15 ft 1 in · 4.60 m
- Fuselage diameter
- 6 ft 3 in · 1.90 m
- Wing span
- 44 ft 3 in · 13.50 m
- Baggage volume
- 76 ft³ · 2.2 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 14,300 lb · 6,500 kg
- Max landing weight
- —
- Max payload
- 5,500 lb · 2,500 kg
- Fuel capacity
- 380 gal · 1,400 L · 1,200 kg (Jet A)
- Max cruise speed
- 160 kt · 184 mph · 296 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 420 nm · 480 mi · 780 km
- Fuel burn
- 0.99 nm/gal · 0.48 km/L
- Ceiling
- 18,700 ft · 5,700 m
- Rate of climb
- 2,300 ft/min · 12 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery
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Live fleet activity details
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