Airbus A321LR vs. Lockheed Model 18 Lodestar
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| Airbus A321LR |
versus |
Lockheed Model 18 Lodestar |
| 44.51 m |
146 ft 0 in |
length |
13.61 m |
44 ft 8 in |
| 11.76 m |
38 ft 7 in |
height |
3.63 m |
11 ft 11 in |
| 35.8 m |
117 ft 5 in |
wingspan |
19.96 m |
65 ft 6 in |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
2 x Wright R-1820 Cyclone radial engines |
| Over 33,000 lbs (147 kN) |
thrust per engine |
1,200 to 1,350 horsepower (895 to 1,007 kW) |
| 66,000 lbs (294 kN) |
total thrust |
2,400 to 2,700 horsepower |
| 97,000 kg |
213,800 lb |
MTOW |
9,979 kg |
22,000 lb |
| 7,400 km |
4,000 nm |
range |
2,500 km |
1,350 nm |
| 832 km/h |
517 mph |
cruise speed |
300 km/h |
186 mph |
| 180-220 passengers |
capacity |
14 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.
