McDonnell Douglas · United States · ICAO: MD90 · 1995–2000 ·
$58.5 million

Capable Mid Range Passenger Jet The McDonnell Douglas MD-90

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Engine:
2× International Aero EnginesIAE V2525-D5
Engine type:
Turbofan
Thrust:
2 × 25,000 lbf  ·  111 kN
Wing Tips:
No winglets
Seats:
172 economy · 153 business
Cabin width:
10 ft 2 in · 3.10 m
Cabin height:
ft 7 in · 2.00 m
Cabin length:
105 ft 9 in · 32.23 m
Exterior length:
152 ft 7 in · 46.50 m
Tail height:
30 ft 7 in · 9.33 m
Fuselage diameter:
10 ft 12 in · 3.35 m
Wing span / rotor:
107 ft 10 in · 32.87 m
Baggage volume:
1,300 ft³  ·  36.8 
Max takeoff weight:
156,000 lb  ·  71,000 kg
Max landing weight:
142,000 lb  ·  64,500 kg
Max Payload:
41,800 lb  ·  19,000 kg
Fuel capacity:
6,400 gal  ·  24,200 L  ·  19,400 kg  (Jet A)
Max cruise speed:
506 kt  ·  582 mph  ·  937 km/h
Approach speed (Vref):
138 kt  ·  159 mph  ·  256 km/h
Range:
2,045 nm  ·  2,350 mi  ·  3,790 km
Fuel burn:
0.37 nm/gal  ·  0.18 km/L
Ceiling:
42,000 ft  ·  12,800 m
Rate of climb:
3,200 ft/min  ·  16 m/s
Takeoff distance:
7,200 ft  ·  2,200 m
Landing distance:
5,250 ft  ·  1,600 m
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