Airbus A220-300 vs. McDonnell Douglas A-4 Skyhawk
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Airbus A220-300 |
versus |
McDonnell Douglas A-4 Skyhawk |
38.7 m |
127 ft 0 in |
length |
12.19 m |
40 ft 0 in |
11.5 m |
37 ft 9 in |
height |
4.57 m |
15 ft |
35.1 m |
115 ft 2 in |
wingspan |
8.08 m |
26 ft 6 in |
2 x Pratt & Whitney PurePower PW1500G |
engines |
1x Pratt & Whitney J52-P-6A Jet |
21,000–23,000 lb |
thrust per engine |
8,500 pound-force |
42,000–46,000 lb |
total thrust |
8,500 pound-force |
70,900 kg |
156,300 lb |
MTOW |
11,113 kg |
24,500 lb |
6,297 km |
3,402 nm |
range |
3,222 km |
1,739 nm |
Mach 0.82 |
101,3 km/h |
cruise speed |
586 kts |
364 mph |
Typical seating 2-class 120-150 |
capacity |
Up to 9,155 pounds of weapons on 5 hardpoints |
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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.