Airbus A321neo vs. Airbus H225 Super Puma
... or view the full comparison list
here.
Airbus A321neo |
versus |
Airbus H225 Super Puma |
44.51 m |
146 ft 0 in |
length |
14.06 m |
46 ft 2 in |
11.76 m |
38 ft 7 in |
height |
4.38 m |
14 ft 4 in |
35.8 m |
117 ft 5 in |
wingspan |
|
|
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
35,000 lb |
thrust per engine |
2,778 hp |
70,000 lb |
total thrust |
5,556 hp |
97,000 kg |
213,800 lb |
MTOW |
11,000 kg |
24,251 lb |
7,400 km |
4,000 nm |
range |
857 km |
463 nm |
828 km/h |
514 mph |
cruise speed |
242 km/h |
150 mph |
180 to 220 passengers |
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.