Technical Specifications - L-1011
Please note that these numbers are believed to be correct but without guarantee. There are variations among the aircraft belonging to the versions listed below!

L-1011
L-1011-1 L-1011-100 L-1011-200 L-1011-250 L-1011-500
CAPACITY:
Passenger Capacity 362/400 362/400 362/400 362/400 315
Cargo capacity: 20 729 kg 20 729 kg 20 729 kg 20 729 kg 27 896 kg
Fuel Capacity: 72 360 kg 80 905 kg 80 905 kg 96 885 kg 96 885 kg
EXTERIOR DIMENSIONS:
Wingspan: 47.35 m 47.35 m 47.35 m 47.35 m 50.09 m
Fuselage length: 54.15 m 54.15 m 54.15 m 54.15 m 50.24 m
Height: 16.87 m 16.87 m 16.87 m 16.87 m 16.87 m
Wing area: 321 m2 321 m2 321 m2 321 m2 328.8 m2
Fuselage diameter: 5.97 m 5.97 m 5.97 m 5.97 m 5.97 m
ENGINES
Engine type: Rolls-Royce RB211-22B Rolls-Royce RB211-22B Rolls-Royce RB211-524B Rolls-Royce RB211-524B Rolls-Royce RB211-524B
Thrust: 19 051 kg 19 051 kg 22 680 kg 22 680 kg 22 680 kg
Engine weight: 5 809 kg 5 809 kg 6 184 kg 6 184 kg 6 184 kg
Fan Diameter: 2.13 m 2.13 m 2.13 m 2.13 m 2.13 m
WEIGHTS:
Maximum take-off weight: 430 000lbs
195 045 kg		 466 000lbs
211 375 kg		 466 000lbs
211 375 kg		 510 000lbs
231 438 kg		 496 000lbs
224 980 kg
Landing weight: 162 385 kg 162 385 kg 162 385 kg 162 385 kg 166 921 kg
Empty weight: 109 647 kg 111 696 kg 112 756 kg 113 198 kg 111 488 kg
PERFORMANCE:
Cruising speed: 964 km/h 954 km/h 982 km/h 973 km/h 973 km/h
Take-off field length: 2 560 m 3 426 m 2 438 m 2 804 m 2 865 m
Range: 5 319 km 6 783 km 6 820 km 8 376 km 9 748 km

Some of the information on this page is acquired from Lockheed.

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