An-32 CLINE (ANTONOV)
Specifications | |
---|---|
Country of Origin | Russia |
Builder | |
Role | Short- to medium-range, light-transport, cargo (39 equipped troops, small vehicles), airdrop |
Similar Aircraft | An-24 Coke, An-26 Curl |
Wing Span | 95 ft, 9 in (29.2 m) |
Length | 78 ft (23.75 m) |
Height | |
take-off weight | 27000 kg |
empty weight | 17250 kg |
max payload | 6700 kg |
max fuel volume | 7100 liters |
Engine | - TVD AI-20D type, Series 5 - power 2x5180 horsepower - service life 6000 h |
Maximum speed | |
Cruising speed | 470-530 kph |
Range | |
takeoff run | 760-880 m |
run length | 470-505 m |
Service Ceiling | - with two working engines 9400-8300 m - with one working engine 4800-3400 m |
Armament | Usually none |
Crew | three - five |
Cost | |
User Countries | operated in 22 countries CIS, Cuba, India, Mongolia, Peru |
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