McDonnell Douglas MD-90
The McDonnell Douglas MD-90 is a twin-engine, short/medium-range commercial jet airliner seating 172 passengers.
Specifications
MD-90[1]
2 class seats
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153-158 : 12J@36" + 141/146Y@31-33"
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1 class seats
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163-172Y@29-33"
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Cargo
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1,300 cu ft (36.8 m3) ER: 1,177 cu ft (33.3 m3)
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Length
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152.6 ft (46.51 m)
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Fuselage height
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142 in (360.7 cm)[2]
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Fuselage width
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131.6 in (334.3 cm)
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Wing span
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107.8 ft (32.86 m)
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Height
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30.6 ft (9.33 m)
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MTOW
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156,000 lb (70,760 kg) ER: 166,000 lb (75,296 kg)
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Empty weight
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88,200 lb (40,007 kg) ER: 88,400 lb (40,098 kg)[a]
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Max payload
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41,800 lb (18,960 kg) ER: 43,600 lb (19,777 kg)
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Fuel Capacity
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39,128 lb (17,748 kg)[b]
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Turbofans (2×)
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25,000 lbf (111.21 kN) IAE V2525-D5[c]
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VMO
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Mach 0.84 (506 kn; 937 km/h) at 27,240 ft (8,303 m)[3]
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Cruise
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Mach 0.74 (427 kn; 790 km/h) at 34,777 ft (10,600 m)[4]
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Ceiling
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37,000 ft (11,278 m)[3]
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Range, 153 pax
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2,045 nmi (3,787 km) ER: 2,237 nmi (4,143 km)[d]
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Takeoff
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7,000 ft (2,134 m) at 156,000 lb, ISA, SL[2]
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- ↑ with aux fuel tank: 89,188 lb (40,455 kg)
- ↑ with aux fuel tank: 42,913 lb (19,465 kg)
- ↑ Option: 28,000 lbf (124.55 kN) V2528-D5
- ↑ 2,455 nmi (4,547 km) with extra 565 US gal (2,140 L) auxiliary fuel tank
References
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