Boeing 747-400 vs. Airbus H225 Super Puma
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Boeing 747-400 |
versus |
Airbus H225 Super Puma |
70.56 m |
231 ft 10 in |
length |
14.06 m |
46 ft 2 in |
19.3 m |
63 ft 4 in |
height |
4.38 m |
14 ft 4 in |
59.49 m |
195 ft 4 in |
wingspan |
|
|
Pratt & Whitney PW4000, General Electric CF6 -80C2 or Rolls-Royce RB211 -524G/H |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
Around 60,000 to 70,000 pounds |
thrust per engine |
2,778 hp |
Around 240,000 to 280,000 pounds |
total thrust |
5,556 hp |
396,834 kg |
875,000 lb |
MTOW |
11,000 kg |
24,251 lb |
13,492 km |
7,285 nmi |
range |
857 km |
463 nm |
939 km/h |
584 mph |
cruise speed |
242 km/h |
150 mph |
Typically accommodates 416 passengers in a three-class layout |
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.