Airbus A321LR vs. de Havilland Canada DHC-6 Twin Otter
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here.
| Airbus A321LR |
versus |
de Havilland Canada DHC-6 Twin Otter |
| 44.51 m |
146 ft 0 in |
length |
15.32 m |
50 ft 3 in |
| 11.76 m |
38 ft 7 in |
height |
5.94 m |
19 ft 6 in |
| 35.8 m |
117 ft 5 in |
wingspan |
19.81 m |
65 ft |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
| Over 33,000 lbs (147 kN) |
thrust per engine |
550 to 750 shaft horsepower (410 to 560 kW) |
| 66,000 lbs (294 kN) |
total thrust |
1100 to 1500 shaft horsepower |
| 97,000 kg |
213,800 lb |
MTOW |
5,670 kg |
12,500 lb |
| 7,400 km |
4,000 nm |
range |
1,389 km |
750 nm |
| 832 km/h |
517 mph |
cruise speed |
280 km/h |
174 mph |
| 180-220 passengers |
capacity |
19 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.
