McDonnell-Douglas MD-11 vs. de Havilland Canada DHC-2 Beaver

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McDonnell-Douglas MD-11 versus de Havilland Canada DHC-2 Beaver
61.20 m 200 ft 10 in length 13.56 m 44 ft 6 in
17.6 m 57 ft 9 in height 5 m 16 ft 5 in
51.6 m 169 ft 4 in wingspan 16.56 m 54 ft 4 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 2 x Armstrong Siddeley Double Mamba turboprop engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine Approximately 3,100 hp (2,312 kW) each
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust Approximately 6,200 hp (4,624 kW) total
285,990 kg 630,400 lb MTOW 24,200 lb 10,977 kg
13,231 km 7,147 nm range 2,535 km 1,369 nm
961 km/h 597 mph cruise speed 228 mph 367 km/h
Max 410 passengers 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.