- Engine:
- 2× Rolls Royce RB211-524H or General Electric CF6-80C2B or Pratt & Whitney PW4060
- Engine type:
- Turbofan
- Thrust:
- 2 × 60,600 lbf · 270 kN
- Avionics:
- Rockwell Collins Avionics
- Wing Tips:
- No winglets
- Seats:
- 351 economy · 269 business · 218 first
- Cabin width:
- 15 ft 6 in · 4.72 m
- Cabin height:
- 9 ft 5 in · 2.87 m
- Cabin length:
- 132 ft 5 in · 40.36 m
- Exterior length:
- 180 ft 3 in · 54.94 m
- Tail height:
- 52 ft 7 in · 16.03 m
- Fuselage diameter:
- 16 ft 6 in · 5.03 m
- Wing span / rotor:
- 156 ft 1 in · 47.57 m
- Baggage volume:
- 4,029 ft³ · 114.1 m³
- Max takeoff weight:
- 350,000 lb · 159,000 kg
- Max landing weight:
- 300,000 lb · 136,000 kg
- Max Payload:
- 91,500 lb · 41,600 kg
- Fuel capacity:
- 16,700 gal · 63,200 L · 50,600 kg (Jet A)
- Max cruise speed:
- 486 kt · 559 mph · 900 km/h
- Approach speed (Vref):
- 140 kt · 161 mph · 259 km/h
- Range:
- 5,975 nm · 6,880 mi · 11,070 km
- Fuel burn:
- 0.25 nm/gal · 0.12 km/L
- Ceiling:
- 43,000 ft · 13,100 m
- Rate of climb:
- 3,000 ft/min · 15 m/s
- Takeoff distance:
- 7,900 ft · 2,410 m
- Landing distance:
- 5,900 ft · 1,800 m
