Kazan Ansat

The light twin helicopter built for training and utility missions.

Overview

Kazan Russia ICAO: ANST 1997–Present $2.5 million

The Kazan Ansat is a Russian-designed light twin-engine helicopter introduced in the 2000s. Developed for civil and military roles, it emphasizes modern avionics and modular cabin layouts. The aircraft is used for training and medical missions.

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Specifications

Units
Engine
2 × Pratt And Whitney PW207K
Engine type
Turboshaft
Power
2 × 630 shp · 470 kW
Avionics
—
Wing tips
No winglets
Seats
9
Crew
—
Cabin width
5 ft 6 in  ·  1.68 m
Cabin height
4 ft 3 in  ·  1.30 m
Cabin length
15 ft 1 in  ·  4.60 m
Exterior length
44 ft 9 in  ·  13.64 m
Tail height
11 ft 2 in  ·  3.40 m
Fuselage diameter
6 ft 3 in  ·  1.90 m
Wing span
37 ft 9 in  ·  11.50 m
Baggage volume
35 ft³  ·  1.0 m³
Gross weight
—
Empty weight
—
Max takeoff weight
7,950 lb  ·  3,600 kg
Max landing weight
—
Max payload
3,850 lb  ·  1,750 kg
Fuel capacity
190 gal · 700 L · 600 kg (Jet A)
Max cruise speed
135 kt  ·  155 mph  ·  250 km/h
Maximum speed
—
Cruise speed
—
Approach speed
—
Range
343 nm  ·  390 mi  ·  640 km
Fuel burn
2.10 nm/gal  ·  1.03 km/L
Ceiling
18,045 ft  ·  5,500 m
Rate of climb
2,362 ft/min  ·  12 m/s
Takeoff distance
—
Landing distance
—
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ANSAT

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Operational Context

Kazan Ansat — light twin-engine helicopter

The Ansat first flew in 1999 and entered service in the 2000s. It features a conventional main rotor and tail rotor configuration. The helicopter was designed with a digital flight control system and adaptable cabin.

Two turboshaft engines producing approximately 630 shaft horsepower each power the helicopter. Cruise speed approaches 135 knots (250 km/h). Maximum takeoff weight exceeds 7,900 pounds (3,600 kg).

The Ansat serves in pilot training, air ambulance, and transport roles. Modernized variants include upgraded avionics and systems. The helicopter represents Russia’s effort to modernize light rotorcraft production.