Airbus A220-100 vs. lockheed C-130 hercules
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Airbus A220-100 |
versus |
lockheed C-130 hercules |
35.0 m |
114 ft 10 in |
length |
29.79 m |
97 ft 9 in |
11.5 m |
37 ft 9 in |
height |
11.66 m |
38 ft 3 in |
35.1 m |
115 ft 2 in |
wingspan |
40.41 m |
132 ft 7 in |
2 Turbofans (wing mounted) |
engines |
4 x Allison T56-A-15 turboprop engines |
21,000–23,000 lb |
thrust per engine |
Approximately 4,590 hp per engine |
42,000–46,000 lb |
total thrust |
Approximately 18,360 hp total |
63,100 kg |
139,100 lb |
MTOW |
70,307 kg |
155,000 lb |
6,390 km |
3,451 nm |
range |
3,760 km |
2,031 nm |
871 km/h |
541 mph |
cruise speed |
540 km/h |
335 mph |
Typical seating 2-class 100-120 |
capacity |
based on configuration |
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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.