Kamov Ka-226 Sergei
A continuation of the Ka-26 design, the Ka-226 remains modular in its configuration. Maximum internal and slung loads are 1400 kg and 1500 kg, respectively.
There are several versions, including: the Ka-226A rescue version, with 9 seats and a rescue winch with a lift capacity of 300 kg; the fire fighting version; the passenger version, equipped with 6-8 seats.
.jpg "The Russian Ka-226 Sergei multipurpose helicopter on display at the MAKS-2013. The twin-engine coaxial aircraft is derived from the Ka-26, retaining the modular configuration.
Taken 30 August 2013.")
Overview
Data on design, manufacture and statusDesign authority: Kamov Design Bureau
Primary manufacturer: Kamov
Parent type: Kamov Ka-26
Aircraft status: Operational
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift devices: 2 in Coaxial configuration
Crew required: 1 in Side-by-side arrangement
Landing gear: Wheels (non-retractable)
Key Characteristics
Data on key physical featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentReferences
References and sources used2003 (page 186)
Book
1999 (page 274)
Book
5 July 2017 (page 186)
Website
