Airbus A220-100 vs. Lockheed Model 18 Lodestar
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Airbus A220-100 |
versus |
Lockheed Model 18 Lodestar |
35.0 m |
114 ft 10 in |
length |
13.61 m |
44 ft 8 in |
11.5 m |
37 ft 9 in |
height |
3.63 m |
11 ft 11 in |
35.1 m |
115 ft 2 in |
wingspan |
19.96 m |
65 ft 6 in |
2 Turbofans (wing mounted) |
engines |
2 x Wright R-1820 Cyclone radial engines |
21,000–23,000 lb |
thrust per engine |
1,200 to 1,350 horsepower (895 to 1,007 kW) |
42,000–46,000 lb |
total thrust |
2,400 to 2,700 horsepower |
63,100 kg |
139,100 lb |
MTOW |
9,979 kg |
22,000 lb |
6,390 km |
3,451 nm |
range |
2,500 km |
1,350 nm |
871 km/h |
541 mph |
cruise speed |
300 km/h |
186 mph |
Typical seating 2-class 100-120 |
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.