Airbus A321LR vs. Canadair CL-415
... or view the full comparison list
here.
| Airbus A321LR |
versus |
Canadair CL-415 |
| 44.51 m |
146 ft 0 in |
length |
19.82 m |
65 ft 0 in |
| 11.76 m |
38 ft 7 in |
height |
8.66 m |
28 ft 5 in |
| 35.8 m |
117 ft 5 in |
wingspan |
28.6 m |
93 ft 1 |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
| Over 33,000 lbs (147 kN) |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
| 66,000 lbs (294 kN) |
total thrust |
4,300 to 4,760 shaft horsepower |
| 97,000 kg |
213,800 lb |
MTOW |
19,733 kg |
43,525 lb |
| 7,400 km |
4,000 nm |
range |
1,600 km |
864 nm |
| 832 km/h |
517 mph |
cruise speed |
290 km/h |
180 mph |
| 180-220 passengers |
capacity |
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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.
