Airbus A330-300 vs. Bombardier CRJ1000
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Airbus A330-300 |
versus |
Bombardier CRJ1000 |
63.66 m |
208 ft 9 in |
length |
39.1 m |
128 ft 5 in |
16.79 m |
55 ft 1 in |
height |
7.5 m |
24 ft 7 in |
60.3 m |
197 ft 9 in |
wingspan |
26.2 m |
86 ft |
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 |
engines |
2 GE CF34-8C5A1 turbofans |
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) |
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 |
Depends on the engine type |
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 |
242,000 kg |
533,600 lb |
MTOW |
41,640 kg |
91,800 lb |
11,750 km |
6,346 nm |
range |
3,004 km |
1,623 nm |
900 km/h |
559 mph |
cruise speed |
515 mph |
829 km/h |
250-290 |
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.