Airbus A220-300 vs. North American B-25 Mitchell
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Airbus A220-300 |
versus |
North American B-25 Mitchell |
38.7 m |
127 ft 0 in |
length |
16.15 m |
53 ft 0 in |
11.5 m |
37 ft 9 in |
height |
5 m |
16 ft 4 in |
35.1 m |
115 ft 2 in |
wingspan |
20.58 m |
67 ft 6 in |
2 x Pratt & Whitney PurePower PW1500G |
engines |
2 x Wright R-2600-92 Twin Cyclone |
21,000–23,000 lb |
thrust per engine |
1,700 horsepower |
42,000–46,000 lb |
total thrust |
3,400 horsepower |
70,900 kg |
156,300 lb |
MTOW |
7,484 kg |
16,500 lb |
6,297 km |
3,402 nm |
range |
1,350 mi |
1,175 nm |
Mach 0.82 |
101,3 km/h |
cruise speed |
233 MPH |
375 km/h |
Typical seating 2-class 120-150 |
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.