de Havilland Canada DHC-2 Beaver vs. Percival Provost

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de Havilland Canada DHC-2 Beaver versus Percival Provost
13.56 m 44 ft 6 in length 9.0 m 29 ft 6 in
5 m 16 ft 5 in height 3.02 m 9 ft 11 in
16.56 m 54 ft 4 in wingspan 12.19 m 40 ft
2 x Armstrong Siddeley Double Mamba turboprop engines engines 1 x Alvis Leonides Major 755/1 inline engine
Approximately 3,100 hp (2,312 kW) each thrust per engine Approximately 550 hp
Approximately 6,200 hp (4,624 kW) total total thrust Approximately 550 hp
24,200 lb 10,977 kg MTOW 5,500 lb 2,495 kg
2,535 km 1,369 nm range 1,127 km 608 nm
228 mph 367 km/h cruise speed 175 mph 282 km/h
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.