Airbus A320-200 vs. Boeing CH-47 Chinook
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Airbus A320-200 |
versus |
Boeing CH-47 Chinook |
38.7 m |
127 ft 0 in |
length |
15.88 m |
51 feet 2 inches |
17.4 m |
57 ft 1 in |
height |
5.68 m |
18 feet 7.8 inches |
35.8 m |
117 ft 5 in |
wingspan |
|
|
Choice between Pratt & Whitney GTFâ„¢ and the LEAP-1A from CFM International |
engines |
2 x Honeywell T55-GA-714A turboshaft engines |
Between 21,000 - 33,000 lbf |
thrust per engine |
4,868 hp |
Between 42,000 - 66,000 lbf |
total thrust |
9,736 hp |
77,000 kg |
169,800 lb |
MTOW |
22,680 kg |
50,000 lb |
5,700 km |
3,078 nm |
range |
370 km |
200 nm |
530 mph |
853 km/h |
cruise speed |
259 km/h |
161 mph |
Typically between 140-180 passengers |
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.