In addition to the Type Certificate designated as S?-236-?nsat dated December 29, 2004 on multi-purpose Ansat helicopter (basic variant with one pilot) Kazan Helicopters, JSC on February 24, 2005 has received Supplements on the following versions of the helicopter:
- air crew of two pilot (Supplement ? 1)
- with emergency floatation system (Supplement ? 2).
Equipped with two Pratt&Whitney/Canada PW-207K engines Ansat is intended for transport operations.
Performance (ISA)
| Take-off weight |
3300 kg |
| Take-off power |
2?630 h.p. |
| The maximum speed in level flight |
275 km/h |
| Cruise speed (long-range flight) |
220 km/h |
| Economic speed |
120 km/h |
| Static ceiling: |
|
| - HOGE |
2500 m |
| - HIGE |
2900 m |
| Service ceiling |
4200 m |
| Maximum rate of climb |
12 km/s |
| Range of flight (with full main fuel tanks) |
520 km |
 
Ansat features:
- hingeless main rotor hub
- fiberglass main and tail rotors
- fly-by-wire control system
- airborne information control system
- skid-type landing gear.
The helicopter is certified in accordance with transport A category and as per visual flight rules. Certification of its further modifications is in progress.
| 
