McDonnell Douglas · United States · ICAO: MD11 · 1988–2000 ·
$147.5 million (1999)

The Wide Body That Changed Commercial Aviation The McDonnell Douglas MD-11

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Engine:
3× Pratt & Whitney PW4460/62 or General Electric CF6-80C2D1F
Engine type:
Turbofan
Thrust:
3 × 61,500 lbf  ·  274 kN
Avionics:
Honeywell VIA 2000 computers
Wing Tips:
Canted winglets
Seats:
410 economy · 323 business · 293 first
Cabin width:
18 ft 9 in · 5.71 m
Cabin height:
ft 11 in · 2.41 m
Cabin length:
152 ft 7 in · 46.51 m
Exterior length:
202 ft 2 in · 61.62 m
Tail height:
57 ft 11 in · 17.65 m
Fuselage diameter:
19 ft 8 in · 6.00 m
Wing span / rotor:
170 ft 6 in · 51.97 m
Baggage volume:
5,297 ft³  ·  150.0 
Max takeoff weight:
630,000 lb  ·  286,000 kg
Max landing weight:
458,000 lb  ·  207,500 kg
Max Payload:
146,500 lb  ·  66,500 kg
Fuel capacity:
41,600 gal  ·  157,500 L  ·  126,000 kg  (Jet A)
Max cruise speed:
519 kt  ·  597 mph  ·  961 km/h
Approach speed (Vref):
150 kt  ·  173 mph  ·  278 km/h
Range:
7,240 nm  ·  8,330 mi  ·  13,410 km
Fuel burn:
0.19 nm/gal  ·  0.09 km/L
Ceiling:
43,000 ft  ·  13,100 m
Rate of climb:
2,000 ft/min  ·  10 m/s
Takeoff distance:
10,300 ft  ·  3,140 m
Landing distance:
6,950 ft  ·  2,120 m
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