Bombardier CRJ1000 vs. McDonnell-Douglas DC-9-30
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Bombardier CRJ1000 |
versus |
McDonnell-Douglas DC-9-30 |
39.1 m |
128 ft 5 in |
length |
36.36 m |
119 ft 3 in |
7.5 m |
24 ft 7 in |
height |
8.5 m |
27 ft 11 in |
26.2 m |
86 ft |
wingspan |
28.44 m |
93 ft 4 in |
2 GE CF34-8C5A1 turbofans |
engines |
2x Pratt & Whitney JT8D |
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve |
thrust per engine |
15,000 pound-force |
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve |
total thrust |
30,000 pound-force (2 engines) |
41,640 kg |
91,800 lb |
MTOW |
54,885 kg |
121,000 lb |
3,004 km |
1,623 nm |
range |
2,632 km |
1,422 nm |
515 mph |
829 km/h |
cruise speed |
898 km/h |
558 mph |
100 (common) |
capacity |
Up to 139 passengers |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.