Airbus A220-100 vs. Douglas DC-8-61
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Airbus A220-100 |
versus |
Douglas DC-8-61 |
35.0 m |
114 ft 10 in |
length |
57.0 m |
187 ft 0 in |
11.5 m |
37 ft 9 in |
height |
13.1 m |
43 ft |
35.1 m |
115 ft 2 in |
wingspan |
45.24 m |
148 ft 5 in |
2 Turbofans (wing mounted) |
engines |
4x P&W JT3D-3B Turbofan |
21,000–23,000 lb |
thrust per engine |
18,000 pound-force |
42,000–46,000 lb |
total thrust |
72,000 pound-force |
63,100 kg |
139,100 lb |
MTOW |
147,400 kg |
325,000 lb |
6,390 km |
3,451 nm |
range |
3,200 nm |
5,926 km |
871 km/h |
541 mph |
cruise speed |
483 knots |
282 mph |
Typical seating 2-class 100-120 |
capacity |
180 to 220 passengers in a mixed-class seating |
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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.