de Havilland Canada DHC-2 Beaver vs. Bell 206

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de Havilland Canada DHC-2 Beaver versus Bell 206
13.56 m 44 ft 6 in length 12.11 m 39 ft 9 in
5 m 16 ft 5 in height 2.88 m 9 ft 5 in
16.56 m 54 ft 4 in wingspan
2 x Armstrong Siddeley Double Mamba turboprop engines engines 1 × Allison 250-C20B
Approximately 3,100 hp (2,312 kW) each thrust per engine 420 shp (313 kW)
Approximately 6,200 hp (4,624 kW) total total thrust 420 shp (313 kW)
24,200 lb 10,977 kg MTOW 1,451 kg 3,199 lb
2,535 km 1,369 nm range 374 km 202 nm
228 mph 367 km/h cruise speed 222 km/h 138 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity 1 pilot + 4 passengers
rotor diameter 11.00 m 36 ft 1 in
rate of climb 425 m/min 1,395 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.