Airbus A321LR vs. Bombardier CS100
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Airbus A321LR |
versus |
Bombardier CS100 |
44.51 m |
146 ft 0 in |
length |
35.00 m |
114 ft 10 in |
11.76 m |
38 ft 7 in |
height |
11.5 m |
37 ft 9 in |
35.8 m |
117 ft 5 in |
wingspan |
35.1 m |
115 ft 2 in |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
2 x Pratt & Whitney PurePower PW1500G |
Over 33,000 lbs (147 kN) |
thrust per engine |
84.1 kN |
66,000 lbs (294 kN) |
total thrust |
168.2 kN |
97,000 kg |
213,800 lb |
MTOW |
54,931 kg |
121,100 lb |
7,400 km |
4,000 nm |
range |
4,074 km |
2,200 nm |
832 km/h |
517 mph |
cruise speed |
871 km/h |
541 mph |
180-220 passengers |
capacity |
110 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.