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Kamov KA-26

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General Data
Notes
First Flown
1965

NATO reporting name is HOODLUM
Length
Height
Rotor Span
Lift Capability
Range
248 nm
Top Speed
105 kts
Empty Weight
4,300 lb
Max Gross Weight
7,165 lb
Service Ceiling
Armament
n/a
Engines
2 Vedeneeb M14-V-26 radial piston engine rated at 325 shp each
Accommodations
1 pilot, 7 passengers
Cargo
n/a
Operators
Similar Aircraft
Other Features

Kamov KA-26 Kamov KA-26 Kamov KA-26 Kamov KA-26 Kamov KA-26 Kamov KA-26 Kamov KA-26
Kamov KA-26 Kamov KA-26 Kamov KA-26 Kamov KA-26 Kamov KA-26 Kamov KA-26 Kamov KA-26
Kamov KA-26

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