Airbus A321LR vs. Percival Provost
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Airbus A321LR |
versus |
Percival Provost |
44.51 m |
146 ft 0 in |
length |
9.0 m |
29 ft 6 in |
11.76 m |
38 ft 7 in |
height |
3.02 m |
9 ft 11 in |
35.8 m |
117 ft 5 in |
wingspan |
12.19 m |
40 ft |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
1 x Alvis Leonides Major 755/1 inline engine |
Over 33,000 lbs (147 kN) |
thrust per engine |
Approximately 550 hp |
66,000 lbs (294 kN) |
total thrust |
Approximately 550 hp |
97,000 kg |
213,800 lb |
MTOW |
5,500 lb |
2,495 kg |
7,400 km |
4,000 nm |
range |
1,127 km |
608 nm |
832 km/h |
517 mph |
cruise speed |
175 mph |
282 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.