Development of the Russian light multipurpose helicopter, the Ka-26 (NATO designation: 'Hoodlum'), began in 1962.  The removable cabin is capable of carrying either six passengers or 2 stretchers and 3 seats; when removed, a cargo platform or sling can be fitted.  Maximum internal and slung loads are 700 kg and 1000 kg, respectively.

Overview

Data on design, manufacture and status

Design authority: Kamov Design Bureau

Primary manufacturer: Kamov

Parent type: Kamov Ka-26

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 2 in Coaxial configuration

Crew required: 1 in Single seater arrangement

Landing gear: Wheels (non-retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Related VFS Resources

Resources related to the Ka-26 , provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.

Related Public Resources

Resources related to the Ka-26 , provided by public sources across the internet.

Images