Kamov Ka-32A

The coaxial helicopter built for heavy utility and firefighting.

Overview

Kamov Russia ICAO: KA32 1980–Present $6.5 million

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

Units
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
—
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Kamov Ka-32A

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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.