Airbus A220-300 vs. McDonnell-Douglas DC-9-30
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Airbus A220-300 |
versus |
McDonnell-Douglas DC-9-30 |
38.7 m |
127 ft 0 in |
length |
36.36 m |
119 ft 3 in |
11.5 m |
37 ft 9 in |
height |
8.5 m |
27 ft 11 in |
35.1 m |
115 ft 2 in |
wingspan |
28.44 m |
93 ft 4 in |
2 x Pratt & Whitney PurePower PW1500G |
engines |
2x Pratt & Whitney JT8D |
21,000–23,000 lb |
thrust per engine |
15,000 pound-force |
42,000–46,000 lb |
total thrust |
30,000 pound-force (2 engines) |
70,900 kg |
156,300 lb |
MTOW |
54,885 kg |
121,000 lb |
6,297 km |
3,402 nm |
range |
2,632 km |
1,422 nm |
Mach 0.82 |
101,3 km/h |
cruise speed |
898 km/h |
558 mph |
Typical seating 2-class 120-150 |
capacity |
Up to 139 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.