- Engine:
- 2× CFM International CFM56
- Engine type:
- Turbofan
- Thrust:
- 2 × 24,000 lbf · 107 kN
- Avionics:
- Thales' D-HUDS Avionics
- Wing Tips:
- Split scimitar winglet
- Seats:
- 18
- Cabin width:
- 12 ft 2 in · 3.70 m
- Cabin height:
- 7 ft 5 in · 2.25 m
- Cabin length:
- 70 ft 2 in · 21.38 m
- Exterior length:
- 103 ft 2 in · 31.45 m
- Tail height:
- 41 ft 2 in · 12.56 m
- Fuselage diameter:
- 12 ft 12 in · 3.96 m
- Wing span / rotor:
- 111 ft 11 in · 34.10 m
- Baggage volume:
- 749 ft³ · 21.2 m³
- Max takeoff weight:
- 150,000 lb · 68,000 kg
- Max landing weight:
- 127,000 lb · 57,500 kg
- Max Payload:
- 26,500 lb · 12,000 kg
- Fuel capacity:
- 6,400 gal · 24,200 L · 19,400 kg (Jet A)
- Max cruise speed:
- 447 kt · 514 mph · 828 km/h
- Approach speed (Vref):
- 130 kt · 150 mph · 241 km/h
- Range:
- 4,200 nm · 4,830 mi · 7,780 km
- Fuel burn:
- 0.59 nm/gal · 0.29 km/L
- Ceiling:
- 41,000 ft · 12,500 m
- Rate of climb:
- 1,350 ft/min · 7 m/s
- Takeoff distance:
- 5,850 ft · 1,790 m
- Landing distance:
- 4,050 ft · 1,230 m
