Airbus A220-100 vs. Airbus A321LR
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Airbus A220-100 |
versus |
Airbus A321LR |
35.0 m |
114 ft 10 in |
length |
44.51 m |
146 ft 0 in |
11.5 m |
37 ft 9 in |
height |
11.76 m |
38 ft 7 in |
35.1 m |
115 ft 2 in |
wingspan |
35.8 m |
117 ft 5 in |
2 Turbofans (wing mounted) |
engines |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
21,000–23,000 lb |
thrust per engine |
Over 33,000 lbs (147 kN) |
42,000–46,000 lb |
total thrust |
66,000 lbs (294 kN) |
63,100 kg |
139,100 lb |
MTOW |
97,000 kg |
213,800 lb |
6,390 km |
3,451 nm |
range |
7,400 km |
4,000 nm |
871 km/h |
541 mph |
cruise speed |
832 km/h |
517 mph |
Typical seating 2-class 100-120 |
capacity |
180-220 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.