Airbus A321LR vs. Lockheed Ventura
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Airbus A321LR |
versus |
Lockheed Ventura |
44.51 m |
146 ft 0 in |
length |
15.7 m |
51 ft 5 in |
11.76 m |
38 ft 7 in |
height |
3.6 m |
11 ft 10 in |
35.8 m |
117 ft 5 in |
wingspan |
20 m |
65 ft 7 in |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
2 x Pratt & Whitney R-2800 radial engines |
Over 33,000 lbs (147 kN) |
thrust per engine |
2,000 hp |
66,000 lbs (294 kN) |
total thrust |
4,000 hp |
97,000 kg |
213,800 lb |
MTOW |
15,000 kg |
33,100 lb |
7,400 km |
4,000 nm |
range |
2,670 km |
1,440 nmi |
832 km/h |
517 mph |
cruise speed |
230 mph |
370 km/h |
180-220 passengers |
capacity |
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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.