The Ka-62 is built to a single-rotor design with a multi-blade anti-torque rotor ducted into the vertical tail fin. It has a five-bladed main rotor, enclosed tail rotor, secondary hydraulics circuit, heavy-duty wheeled landing gear, strengthened fuselage and mounting attachments for major components, as well as shock-absorbent seats for passengers and crew.

The Ka-62 is designed for cargo transportation, medevac and search and rescue operations, and can also be used in the oil and gas sector and for corporate purposes.

Performance:
Max. cruise Speed – 285 km/h
Max. speed – 300 km/h
Max. flight – 700 km
Hovering in ground effect (MTOW, ISA) – 3 800 m
Service ceiling (ISA) – 5 500 m

Weights:
Maximum takeoff weight – 6 800 kg
Max. cabin load – 2 000 kg
Max. external sling load – 2 500 kg

Dimensions:
Length – 13,5 m
Height – 4,87 m
Rotor diameter – 13,8 m
Passenger cabin volume – 9 ㎥

Capacity:
up to 15 persons in passenger configuration (PAX)
up to 9 persons in VIP configuration