de Havilland Canada DHC-2 Beaver vs. Max Holste M.H.1521 Broussard

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de Havilland Canada DHC-2 Beaver versus Max Holste M.H.1521 Broussard
13.56 m 44 ft 6 in length 10.46 m 34 ft 4 in
5 m 16 ft 5 in height 2.74 m 9 ft
16.56 m 54 ft 4 in wingspan 12.86 m 42 ft 2 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 1 x Lycoming GSO-480-B1A6 flat-six engine
Approximately 3,100 hp (2,312 kW) each thrust per engine Approximately 295 hp
Approximately 6,200 hp (4,624 kW) total total thrust Approximately 295 hp
24,200 lb 10,977 kg MTOW 1,900 kg 4,189 lb
2,535 km 1,369 nm range 1,030 km 556 nm
228 mph 367 km/h cruise speed 145 mph 233 km/h
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity 5-7 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.