Airbus A220-300 vs. Lockheed Model 18 Lodestar
... or view the full comparison list
here.
Airbus A220-300 |
versus |
Lockheed Model 18 Lodestar |
38.7 m |
127 ft 0 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 x Pratt & Whitney PurePower PW1500G |
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 |
70,900 kg |
156,300 lb |
MTOW |
9,979 kg |
22,000 lb |
6,297 km |
3,402 nm |
range |
2,500 km |
1,350 nm |
Mach 0.82 |
101,3 km/h |
cruise speed |
300 km/h |
186 mph |
Typical seating 2-class 120-150 |
capacity |
14 passengers |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.