Cessna O-2 Skymaster vs. de Havilland Canada DHC-2 Beaver

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Cessna O-2 Skymaster versus de Havilland Canada DHC-2 Beaver
8.9 m 29 ft 2 in length 13.56 m 44 ft 6 in
2.87 m 9 ft 5 in height 5 m 16 ft 5 in
11.58 m 38 ft wingspan 16.56 m 54 ft 4 in
Two 210-hp Continental IO-360s engines 2 x Armstrong Siddeley Double Mamba turboprop engines
210 hp thrust per engine Approximately 3,100 hp (2,312 kW) each
420 hp total thrust Approximately 6,200 hp (4,624 kW) total
5,400 lb 2,449 kg MTOW 24,200 lb 10,977 kg
1,705 km 921 nm range 2,535 km 1,369 nm
144 mph 232 km/h cruise speed 228 mph 367 km/h
2 capacity Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.