Technical specifications 
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A multipurpose coaxial transport helicopter derived from the Ka-27PS and powered by two TV3-117VK or TV3-117VMA 2.200-hp gas turbine engines. The maiden flight was made on 8 October, 1980.
Series production started at the Kumertau Aircraft Production Association in 1986. The following versions were developed:
Ka-32S shipborne ice patrol helicopter; Ka-32T transport featuring a lifting capacity of 5 tonnes; Ka-32K "flying crane" ; Ka-32A upgraded transport fitted with two TV3-117VMA engines , its Russian airworthiness certificate was received on 16 July 1993); Ka-32A1 rescue helicopter for rescuing people from highriser fires (its maiden flight was made on 12 January, 1994); Ka-32A2 police patrol helicopter; Ka-32A7 (Ka-327) armed borderguard patrol helicopter; Ka-32A11-the Ka-32A version intended for export to Canada (certified in line with US airworthiness standard FAR-29 in 1997); Ka-32A12- a Ka-32A version certified under the JAR-29 standard in Switzerland in June 1996; etc.
TECHNICAL SPECIFICATIONS
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DESIGNER
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OKB Kamov
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TYPE
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Multipurpose helicopter
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CREW
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3-4
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POWER-PLANT
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Klimov TV3-117VMA
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Power, h.p.
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2 x 2.200
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DIMENSIONS
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Length, m
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12,25
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Main rotor diameter, m
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15,90
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Wing span, m
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-
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Height, m
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3,80
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WEIGHT
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Empty, kg
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6.000
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Normal take-off, kg
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12.700
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Maximum take-off, kg
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-
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Internal fuel, kg
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-
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PERFORMANCE
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Maximum speed, km/h
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260
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Cruising speed, km/h
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230
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Range, km
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800
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Combat range, km
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-
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Service ceiling, m
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6.000
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Static ceiling, m
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3.500
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Payload, kg
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-
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| ARMAMENT | Anti-ship missile X-35U , X-35 (Kh-35U, Kh-35) |
