Bombardier CRJ1000 vs. McDonnell-Douglas DC-10-30
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Bombardier CRJ1000 |
versus |
McDonnell-Douglas DC-10-30 |
39.1 m |
128 ft 5 in |
length |
55.35 m |
181 ft 8 in |
7.5 m |
24 ft 7 in |
height |
17.8 m |
58 ft 5 in |
26.2 m |
86 ft |
wingspan |
50.39 m |
165 ft 4 in |
2 GE CF34-8C5A1 turbofans |
engines |
3x GE CF6-50C Turbofan |
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 |
54,000 lbf |
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 |
162,000 lbf |
41,640 kg |
91,800 lb |
MTOW |
251,744 kg |
555,000 lb |
3,004 km |
1,623 nm |
range |
9,630 km |
5,200 nm |
515 mph |
829 km/h |
cruise speed |
507 knots |
939 km/h |
100 (common) |
capacity |
Up to 380 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.