de Havilland Canada DHC-2 Beaver vs. Cessna 172

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de Havilland Canada DHC-2 Beaver versus Cessna 172
13.56 m 44 ft 6 in length 8.28 m 27 ft 2 in
5 m 16 ft 5 in height 2.72 m 8 ft 11 in
16.56 m 54 ft 4 in wingspan 11 m 36 ft 1 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 1 x Lycoming IO-360-L2A flat-4 piston engine
Approximately 3,100 hp (2,312 kW) each thrust per engine 180 to 200 horsepower (134 to 149 kW)
Approximately 6,200 hp (4,624 kW) total total thrust 180 to 200 horsepower (134 to 149 kW)
24,200 lb 10,977 kg MTOW 1,040 kg 2,293 lb
2,535 km 1,369 nm range 1,056 km 570 nm
228 mph 367 km/h cruise speed 226 km/h 140 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity 4
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.