Lockheed L-1011 TriStar 500 vs. Airbus H225 Super Puma

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Lockheed L-1011 TriStar 500 versus Airbus H225 Super Puma
50.05 m 164 ft 3 in length 14.06 m 46 ft 2 in
16.87 m 55 ft 4 in height 4.38 m 14 ft 4 in
50.09 m 164 ft 4 in wingspan
3 Rolls-Royce RB211 engines engines 2 x Turbomeca Makila 2A turboshaft engines
42,000 lbf thrust per engine 2,778 hp
126,000 lbf (3 engines x 42,000 lbf per engine) total thrust 5,556 hp
231,330 kg 510,000 lb MTOW 11,000 kg 24,251 lb
11,260 km 6,100 nm range 857 km 463 nm
525 knots 972 km/h cruise speed 242 km/h 150 mph
Max. 315 passengers (typical 253) 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.