Overview
The Kamov Ka-32A is a civil utility helicopter derived from the Ka-27 naval platform. Introduced in the 1980s, it features a distinctive coaxial rotor system. The aircraft serves in firefighting and heavy-lift roles.
Live Fleet Activity (KA32)
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Specifications
- Engine
- 2 × Klimov TV3-117V turboshafts
- Engine type
- Turboshaft
- Power
- 2 × 2,190 shp · 1,633 kW
- Avionics
- Israel Aerospace Industries.
- Wing tips
- No winglets
- Seats
- 13
- Crew
- —
- Cabin width
- 4 ft 3 in · 1.30 m
- Cabin height
- 4 ft 1 in · 1.24 m
- Cabin length
- 14 ft 10 in · 4.52 m
- Exterior length
- 37 ft 1 in · 11.30 m
- Tail height
- 18 ft 1 in · 5.50 m
- Fuselage diameter
- 5 ft 3 in · 1.60 m
- Wing span
- 52 ft 2 in · 15.90 m
- Baggage volume
- 35 ft³ · 1.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 28,000 lb · 12,700 kg
- Max landing weight
- —
- Max payload
- 11,000 lb · 5,000 kg
- Fuel capacity
- 700 gal · 2,600 L · 2,100 kg (Jet A)
- Max cruise speed
- 124 kt · 143 mph · 230 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 530 nm · 610 mi · 980 km
- Fuel burn
- 0.70 nm/gal · 0.34 km/L
- Ceiling
- 16,405 ft · 5,000 m
- Rate of climb
- 2,460 ft/min · 12 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery
Live fleet activity details
Operational Context
Kamov Ka-32A — twin-engine utility helicopter
The Ka-32 first flew in 1973, with civil variants entering service in the 1980s. It employs coaxial counter-rotating rotors for stability and lift efficiency. The design eliminates the need for a tail rotor.
Two turboshaft engines producing approximately 2,200 shaft horsepower each power the helicopter. Cruise speed approaches 140 knots (259 km/h). Maximum takeoff weight exceeds 26,000 pounds (11,793 kg).
The Ka-32A has been used in firefighting, construction, and rescue missions worldwide. Its lifting capability and compact footprint are key advantages. The aircraft remains in production in modernized forms.
Sources and references used for research and fact-checking.