Boeing · United States · ICAO: B742 · 1970–1991 ·
$39 million (1976)
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Engine:
4× Pratt & Whitney JT9D-7R4G2
Engine type:
Turbofan
Thrust:
4 × 54,750 lbf  ·  244 kN
Wing Tips:
No winglets
Seats:
480
Cabin width:
20 ft 0 in · 6.10 m
Cabin height:
ft 2 in · 2.50 m
Cabin length:
187 ft 0 in · 57.00 m
Exterior length:
230 ft 12 in · 70.40 m
Tail height:
64 ft 4 in · 19.60 m
Fuselage diameter:
21 ft 4 in · 6.50 m
Wing span / rotor:
195 ft 8 in · 59.64 m
Baggage volume:
5,509 ft³  ·  156.0 
Max takeoff weight:
833,000 lb  ·  378,000 kg
Max landing weight:
630,000 lb  ·  285,500 kg
Max Payload:
150,500 lb  ·  68,000 kg
Fuel capacity:
52,400 gal  ·  198,400 L  ·  158,700 kg  (Jet A)
Max cruise speed:
522 kt  ·  601 mph  ·  967 km/h
Approach speed (Vref):
141 kt  ·  162 mph  ·  261 km/h
Range:
6,560 nm  ·  7,550 mi  ·  12,150 km
Ceiling:
45,100 ft  ·  13,700 m
Rate of climb:
1,000 ft/min  ·  m/s
Takeoff distance:
10,500 ft  ·  3,200 m
Landing distance:
6,250 ft  ·  1,900 m
Live Fleet Activity Details (B742)
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