- Engine:
- 4× Rolls Royce RB211-524G/H, Pratt & Whitney PW4062, GE CF6-80C2B5F
- Engine type:
- Turbofan
- Thrust:
- 4 × 63,300 lbf · 282 kN
- Avionics:
- Rockwell Collins Avionics
- Wing Tips:
- Canted winglets
- Seats:
- 2
- Cabin width:
- 20 ft 1 in · 6.13 m
- Cabin height:
- 8 ft 4 in · 2.54 m
- Cabin length:
- 187 ft 0 in · 57.00 m
- Exterior length:
- 231 ft 10 in · 70.67 m
- Tail height:
- 64 ft 1 in · 19.54 m
- Fuselage diameter:
- 21 ft 4 in · 6.50 m
- Wing span / rotor:
- 212 ft 12 in · 64.92 m
- Baggage volume:
- 24,791 ft³ · 702.0 m³
- Max takeoff weight:
- 875,000 lb · 397,000 kg
- Max landing weight:
- 666,000 lb · 302,000 kg
- Max Payload:
- 271,000 lb · 123,000 kg
- Fuel capacity:
- 57,300 gal · 216,800 L · 173,500 kg (Jet A)
- Max cruise speed:
- 506 kt · 582 mph · 937 km/h
- Approach speed (Vref):
- 138 kt · 159 mph · 256 km/h
- Range:
- 4,455 nm · 5,130 mi · 8,250 km
- Fuel burn:
- 0.13 nm/gal · 0.06 km/L
- Ceiling:
- 43,000 ft · 13,100 m
- Rate of climb:
- 1,500 ft/min · 8 m/s
- Takeoff distance:
- 10,800 ft · 3,300 m
- Landing distance:
- 6,900 ft · 2,100 m
