Airbus A300-600 vs. Bombardier CRJ1000
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Airbus A300-600 |
versus |
Bombardier CRJ1000 |
54.10 m |
177 ft 6 in |
length |
39.1 m |
128 ft 5 in |
16.5 m |
54 ft 2 in |
height |
7.5 m |
24 ft 7 in |
44.84 m |
147 ft 1 in |
wingspan |
26.2 m |
86 ft |
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
2 GE CF34-8C5A1 turbofans |
56,000lb to 61,500lb |
thrust per engine |
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 |
112,000–123,000 lb |
total thrust |
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve |
171,700 kg |
378,600 lb |
MTOW |
41,640 kg |
91,800 lb |
7,500 km |
4,052 nm |
range |
3,004 km |
1,623 nm |
897 km/h |
557 mph |
cruise speed |
515 mph |
829 km/h |
210-250 passengers |
capacity |
100 (common) |
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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.