Airbus A220-100 vs. Airbus H225 Super Puma
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Airbus A220-100 |
versus |
Airbus H225 Super Puma |
35.0 m |
114 ft 10 in |
length |
14.06 m |
46 ft 2 in |
11.5 m |
37 ft 9 in |
height |
4.38 m |
14 ft 4 in |
35.1 m |
115 ft 2 in |
wingspan |
|
|
2 Turbofans (wing mounted) |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
21,000–23,000 lb |
thrust per engine |
2,778 hp |
42,000–46,000 lb |
total thrust |
5,556 hp |
63,100 kg |
139,100 lb |
MTOW |
11,000 kg |
24,251 lb |
6,390 km |
3,451 nm |
range |
857 km |
463 nm |
871 km/h |
541 mph |
cruise speed |
242 km/h |
150 mph |
Typical seating 2-class 100-120 |
capacity |
24-28 |
|
|
rotor diameter |
16.2 m |
53 ft 2 in |
|
|
rate of climb |
10.7 m/s |
2,106 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.