Airframer
Programs › Kamov Ka-226T

Aircraft program

Kamov Ka-226T

In production
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Twin turboshaft light utility helicopter with co-axial contra-rotating rotors. Includes the variant Ka-226T Climber.

Kamov Ka-226T
Lift type
Rotary wing
Assembly
Factory-built
Control
Piloted
Engine type
Turboshaft
Application
Cargo, Search & rescue, Surveillance, Trainer, Utility

Design & construction

The aircraft as engineered: what it is built from, the systems it flies with, and its configuration — each box a theme.

Airframe & structure
Primary structure
Composite
Landing gear
Fixed tricycle
Ice protection
None
Pressurisation
Unpressurised
Systems & avionics
Flight controls
Mechanical
Autopilot
3-axis
Avionics architecture
Integrated glass suite
Configuration & certification
Rotor configuration
Coaxial
Certification
Part 27
Minimum crew
1

Technical reference compiled with AI research; a value appears only where two independent research passes and a web fact-check agree. Gaps are deliberate.

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Type variants

VariantLaunch / first flightProduction endNotes
Kamov Ka-2261990 / 1997Baseline variant.
Kamov Ka-226T2009 / 2009Variant with enhanced engine and avionics.

Airframer

Ulan Ude Aviation Plant Joint Stock CompanyNews
National Centre for Helicopter Engineering, KamovNews

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