Specifications (Military configuration):
Powerplant:Two Garret single shaft 671kW/900shp TPE-331-10R Turboprops
with four-bladed Dowty Rotol R334/482-F/13 reversible propellers.
Capable of delivering 925 shp in case of one engine take-off.
Length: 16015m / 52ft 11¾ inc
WingSpan:20.28m / 66ft 6½ inc
MTOW:8000 kg / 17 637 lb.
Max landing weight: 7 450 kg / 16 424 lb.
Max Speed: 200kt / 370km/h / 230 mph
Max cruising speed: 191 kt / 354 km/h / 220 mph.
Economical cruising Speed: 162 kt / 300 km/h / 186 mph.
Stall speed at MTOW: 78 kt
Max Payload: 2 820 kg / 6 217 lb.
Range:
Max fuel & 2 120 kg (4 674 lb) payload : 907 nm / 1 682 km / 1 045 miles.
Max payload: 450 nm / 835 km / 519 miles.
With additional Fuel & 1 192 kg (2 628 lb) payload:1 446 nm /
2 680 km / 1 665 miles.
[All three with 45 min reserve].
Additional fuel in pylon underwing tanks: 1 000 kg / 1 764 lb.
Runway requirements:
Take-off STOL: 384 m / 1 260 ft
Landing STOL: 285 m / 935 ft.
Normal TO: 610m / 2000 ft.
Normal Landing: 462 m / 1 516 ft.
Service Ceiling: 7 925m / 26 000 ft. (unpressurized).
Max rate of climb at SL:
Normal: 1 630 fpm
One engine out: 312 fpm.
