Airbus A321XLR vs. de Havilland Canada DHC-6 Twin Otter
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here.
| Airbus A321XLR |
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 LEAP-1A and P&W PW1100G |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
| 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 |
| 101,000 kg |
222,700 lb |
MTOW |
5,670 kg |
12,500 lb |
| 4,700 nmi |
8,704 km |
range |
1,389 km |
750 nm |
| 963km/h |
598mph |
cruise speed |
280 km/h |
174 mph |
| 180-220 seats (typical 2-class seating) |
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.
