Lockheed L-1011 TriStar 500 vs. Canadair CL-415

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Lockheed L-1011 TriStar 500 versus Canadair CL-415
50.05 m 164 ft 3 in length 19.82 m 65 ft 0 in
16.87 m 55 ft 4 in height 8.66 m 28 ft 5 in
50.09 m 164 ft 4 in wingspan 28.6 m 93 ft 1
3 Rolls-Royce RB211 engines engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
42,000 lbf thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
126,000 lbf (3 engines x 42,000 lbf per engine) total thrust 4,300 to 4,760 shaft horsepower
231,330 kg 510,000 lb MTOW 19,733 kg 43,525 lb
11,260 km 6,100 nm range 1,600 km 864 nm
525 knots 972 km/h cruise speed 290 km/h 180 mph
Max. 315 passengers (typical 253) capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.