Airbus A321LR vs. de Havilland Canada DHC-2 Beaver
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| Airbus A321LR |
versus |
de Havilland Canada DHC-2 Beaver |
| 44.51 m |
146 ft 0 in |
length |
13.56 m |
44 ft 6 in |
| 11.76 m |
38 ft 7 in |
height |
5 m |
16 ft 5 in |
| 35.8 m |
117 ft 5 in |
wingspan |
16.56 m |
54 ft 4 in |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
| Over 33,000 lbs (147 kN) |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
| 66,000 lbs (294 kN) |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
| 97,000 kg |
213,800 lb |
MTOW |
24,200 lb |
10,977 kg |
| 7,400 km |
4,000 nm |
range |
2,535 km |
1,369 nm |
| 832 km/h |
517 mph |
cruise speed |
228 mph |
367 km/h |
| 180-220 passengers |
capacity |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
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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.
