Avro 652 Anson vs. Airbus H225 Super Puma

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Avro 652 Anson versus Airbus H225 Super Puma
12.88 m 42 ft 3 in length 14.06 m 46 ft 2 in
2.9 m 9 ft 6 in height 4.38 m 14 ft 4 in
17.22 m 56 ft 6 in wingspan
2 × Armstrong Siddeley Cheetah VI engines 2 x Turbomeca Makila 2A turboshaft engines
290 hp (220 kW) thrust per engine 2,778 hp
580 hp (440 kW) total thrust 5,556 hp
7,500 lb 3,402 kg MTOW 11,000 kg 24,251 lb
1,267 km 684 nm range 857 km 463 nm
165 mph 266 km/h cruise speed 242 km/h 150 mph
4 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.