- Engine:
- 2× Pratt and Whitney PW 4090 or Rolls-Royce Trent 895 or GE GE90-94B
- Engine type:
- Turbofan
- Thrust:
- 2 × 93,700 lbf · 417 kN
- Avionics:
- Honeywell Avionics
- Wing Tips:
- No winglets
- Seats:
- 440 economy · 400 business · 301 first
- Cabin width:
- 19 ft 3 in · 5.86 m
- Cabin height:
- 7 ft 3 in · 2.20 m
- Cabin length:
- 161 ft 1 in · 49.10 m
- Exterior length:
- 208 ft 12 in · 63.70 m
- Tail height:
- 60 ft 8 in · 18.50 m
- Fuselage diameter:
- 20 ft 4 in · 6.19 m
- Wing span / rotor:
- 199 ft 10 in · 60.90 m
- Baggage volume:
- 5,721 ft³ · 162.0 m³
- Max takeoff weight:
- 656,000 lb · 297,500 kg
- Max landing weight:
- 470,000 lb · 213,000 kg
- Max Payload:
- 131,000 lb · 59,500 kg
- Fuel capacity:
- 45,200 gal · 171,200 L · 136,900 kg (Jet A)
- Max cruise speed:
- 510 kt · 587 mph · 945 km/h
- Approach speed (Vref):
- 136 kt · 157 mph · 252 km/h
- Range:
- 7,510 nm · 8,640 mi · 13,910 km
- Fuel burn:
- 0.17 nm/gal · 0.08 km/L
- Ceiling:
- 43,100 ft · 13,100 m
- Rate of climb:
- 3,000 ft/min · 15 m/s
- Takeoff distance:
- 8,000 ft · 2,440 m
- Landing distance:
- 5,100 ft · 1,550 m
