Description

The Ka-226T is powered by 580 h.p. FADEC-equipped Arrius 2G1 engines by SAFRAN HE which enables the helicopter to land or take-off safely if one engine fails.

The coaxial main rotor system and absence of a tail rotor not only makes it safer on the ground and in the air, but also makes it possible to use the Ka-226T in spaces with scant room for manoeuver, as the fuselage does not extend beyond the area swept by the rotors.

Performance:
Max. cruise Speed – 190 km/h
Max. speed – 220 km/h
Max. flight – 460 km
Hovering in ground effect (MTOW, ISA) – 5 200 m
Service ceiling (ISA) – 6 200 m

Weights:
Maximum takeoff weight – 3 600 kg
Max. cabin load – 1 000 kg
Max. external sling load – 1 000 kg

Dimensions:
Length – 13,24 m
Height – 4,21 m
Rotor diameter – 13,24 m
Passenger cabin volume – 6,1 ㎥

Capacity:
up to 7 persons in passenger configuration (PAX)
up to 4 persons in VIP configuration

Specification

1. Ка-226T_rus.pdf
2. Ка-226T_ENG.pdf