- Engine:
- 1× Rolls-Royce F402-RR-408 turbofan
- Engine type:
- Turbofan
- Thrust:
- 23,500 lbf · 105 kN
- Avionics:
- Collins RT1250A/ARC U/UHF, Bendix RT-1157/APX-100 IFF system, Litton AN/ASN-130A INS
- Wing Tips:
- No winglets
- Seats:
- 1
- Exterior length:
- 46 ft 4 in · 14.12 m
- Tail height:
- 11 ft 8 in · 3.55 m
- Wing span / rotor:
- 30 ft 4 in · 9.25 m
- Max takeoff weight:
- 31,000 lb · 14,100 kg
- Max landing weight:
- 25,000 lb · 11,300 kg
- Max Payload:
- 13,200 lb · 6,000 kg
- Fuel capacity:
- 2,350 gal · 8,900 L · 7,200 kg (Jet A)
- Max cruise speed:
- 575 kt · 662 mph · 1,065 km/h
- Range:
- 1,965 nm · 2,260 mi · 3,640 km
- Fuel burn:
- 0.75 nm/gal · 0.37 km/L
- Ceiling:
- 50,000 ft · 15,200 m
- Rate of climb:
- 14,700 ft/min · 75 m/s
- Takeoff distance:
- 1,700 ft · 520 m
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