Airbus A321LR vs. Bombardier CRJ1000
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Airbus A321LR |
versus |
Bombardier CRJ1000 |
44.51 m |
146 ft 0 in |
length |
39.1 m |
128 ft 5 in |
11.76 m |
38 ft 7 in |
height |
7.5 m |
24 ft 7 in |
35.8 m |
117 ft 5 in |
wingspan |
26.2 m |
86 ft |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
2 GE CF34-8C5A1 turbofans |
Over 33,000 lbs (147 kN) |
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 |
66,000 lbs (294 kN) |
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 |
97,000 kg |
213,800 lb |
MTOW |
41,640 kg |
91,800 lb |
7,400 km |
4,000 nm |
range |
3,004 km |
1,623 nm |
832 km/h |
517 mph |
cruise speed |
515 mph |
829 km/h |
180-220 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.