Airbus A220-100 vs. Boeing CH-47 Chinook
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Airbus A220-100 |
versus |
Boeing CH-47 Chinook |
35.0 m |
114 ft 10 in |
length |
15.88 m |
51 feet 2 inches |
11.5 m |
37 ft 9 in |
height |
5.68 m |
18 feet 7.8 inches |
35.1 m |
115 ft 2 in |
wingspan |
|
|
2 Turbofans (wing mounted) |
engines |
2 x Honeywell T55-GA-714A turboshaft engines |
21,000–23,000 lb |
thrust per engine |
4,868 hp |
42,000–46,000 lb |
total thrust |
9,736 hp |
63,100 kg |
139,100 lb |
MTOW |
22,680 kg |
50,000 lb |
6,390 km |
3,451 nm |
range |
370 km |
200 nm |
871 km/h |
541 mph |
cruise speed |
259 km/h |
161 mph |
Typical seating 2-class 100-120 |
capacity |
33-55 |
|
|
rotor diameter |
18.3 m |
60 ft |
|
|
rate of climb |
10.2 m/s |
2,008 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.