Boeing 717-200HGW vs. Airbus H225 Super Puma
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Boeing 717-200HGW |
versus |
Airbus H225 Super Puma |
37.80 m |
123 ft 11 in |
length |
14.06 m |
46 ft 2 in |
8.87 m |
29 ft 1 in |
height |
4.38 m |
14 ft 4 in |
28.44 m |
93 ft 4 in |
wingspan |
|
|
2 Rolls-Royce BR715 |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
82.3kN (18,500lb) to 93.4kN (21,000lb) |
thrust per engine |
2,778 hp |
164.6kN (37,000lb) to 186.8kN (42,000lb) |
total thrust |
5,556 hp |
54,885 kg |
121,000 lb |
MTOW |
11,000 kg |
24,251 lb |
2,060 nm |
3,814 km |
range |
857 km |
463 nm |
811 km/h |
504 mph |
cruise speed |
242 km/h |
150 mph |
106 passengers in a 2 class configuration |
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.