Lockheed L-1011 TriStar 500 vs. de Havilland Canada DHC-2 Beaver

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Lockheed L-1011 TriStar 500 versus de Havilland Canada DHC-2 Beaver
50.05 m 164 ft 3 in length 13.56 m 44 ft 6 in
16.87 m 55 ft 4 in height 5 m 16 ft 5 in
50.09 m 164 ft 4 in wingspan 16.56 m 54 ft 4 in
3 Rolls-Royce RB211 engines engines 2 x Armstrong Siddeley Double Mamba turboprop engines
42,000 lbf thrust per engine Approximately 3,100 hp (2,312 kW) each
126,000 lbf (3 engines x 42,000 lbf per engine) total thrust Approximately 6,200 hp (4,624 kW) total
231,330 kg 510,000 lb MTOW 24,200 lb 10,977 kg
11,260 km 6,100 nm range 2,535 km 1,369 nm
525 knots 972 km/h cruise speed 228 mph 367 km/h
Max. 315 passengers (typical 253) 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.