Fairey Gannet vs. Airbus H225 Super Puma

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Fairey Gannet versus Airbus H225 Super Puma
10.87 m 35 ft 8 in length 14.06 m 46 ft 2 in
3.76 m 12 ft 4 in height 4.38 m 14 ft 4 in
13.87 m 45 ft 6 in wingspan
1 x Bristol Pegasus XVIII radial engine engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 690 hp (515 kW) thrust per engine 2,778 hp
Approximately 690 hp (515 kW) total thrust 5,556 hp
7,005 lb 3,178 kg MTOW 11,000 kg 24,251 lb
840 km 454 nm range 857 km 463 nm
139 mph 224 km/h cruise speed 242 km/h 150 mph
Pilot, Observer, and Air Gunner 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.