Bombardier CRJ1000 vs. Lockheed L-1011 TriStar 500

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Bombardier CRJ1000 versus Lockheed L-1011 TriStar 500
39.1 m 128 ft 5 in length 50.05 m 164 ft 3 in
7.5 m 24 ft 7 in height 16.87 m 55 ft 4 in
26.2 m 86 ft wingspan 50.09 m 164 ft 4 in
2 GE CF34-8C5A1 turbofans engines 3 Rolls-Royce RB211 engines
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine 42,000 lbf
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust 126,000 lbf (3 engines x 42,000 lbf per engine)
41,640 kg 91,800 lb MTOW 231,330 kg 510,000 lb
3,004 km 1,623 nm range 11,260 km 6,100 nm
515 mph 829 km/h cruise speed 525 knots 972 km/h
100 (common) capacity Max. 315 passengers (typical 253)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.