McDonnell-Douglas DC-10-30 vs. Airbus H225 Super Puma
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McDonnell-Douglas DC-10-30 |
versus |
Airbus H225 Super Puma |
55.35 m |
181 ft 8 in |
length |
14.06 m |
46 ft 2 in |
17.8 m |
58 ft 5 in |
height |
4.38 m |
14 ft 4 in |
50.39 m |
165 ft 4 in |
wingspan |
|
|
3x GE CF6-50C Turbofan |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
54,000 lbf |
thrust per engine |
2,778 hp |
162,000 lbf |
total thrust |
5,556 hp |
251,744 kg |
555,000 lb |
MTOW |
11,000 kg |
24,251 lb |
9,630 km |
5,200 nm |
range |
857 km |
463 nm |
507 knots |
939 km/h |
cruise speed |
242 km/h |
150 mph |
Up to 380 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.