Airbus A321LR vs. de Havilland DH-82 Tiger Moth
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| Airbus A321LR |
versus |
de Havilland DH-82 Tiger Moth |
| 44.51 m |
146 ft 0 in |
length |
7.29 m |
23 ft 11 in |
| 11.76 m |
38 ft 7 in |
height |
2.67 m |
8 ft 9 in |
| 35.8 m |
117 ft 5 in |
wingspan |
8.97 m |
29 ft 5 in |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
1 x de Havilland Gipsy Major I inline engine |
| Over 33,000 lbs (147 kN) |
thrust per engine |
Approximately 130 hp |
| 66,000 lbs (294 kN) |
total thrust |
Approximately 130 hp |
| 97,000 kg |
213,800 lb |
MTOW |
1,825 lb |
828 kg |
| 7,400 km |
4,000 nm |
range |
322 km |
174 nm |
| 832 km/h |
517 mph |
cruise speed |
78 mph |
126 km/h |
| 180-220 passengers |
capacity |
Pilot and one passenger |
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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.
