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Lockheed L-1011-385-3 TriStar 500 Specifications

Announced in November of 1975, the TriStar 500 first flew in 16 October 1978. It was designed by Lockheed as a truly long-range aircraft with a shortened fuselage with less 4.1 m in comparison with standard TriStars. It has also a larger wingspan with active ailerons. Only 50 were built until end of production in 1983.

Maximum Passengers Capacity: 315 pax
Lenght: 50.05 m
Wingspan: 50.09 m
Height: 16.87 m
Economic Mach Cruise: 0.84 M
Engines: 3 x Rolls-Royce RB211-524B4-02 (50,000 lbs)
Fuel Capacity: 96,615 kg
MTOW: 231,332 kg
MLAW: 166,922 kg
OEW: 112,091 kg
MZFW: 153,314 kg
Maximum Payload: 41,050 kg
Maximum Range: 5,600 nm
Take-off Field with Maximum Load @ ISA: 9,400 ft
Service Ceiling: 43,000 ft
Crew: 3 cockpit crew + 7 cabin crew (minimum)

 

DOCUMENT SOURCE FORMAT
Type Certificate Data Sheet (includes all L-1011 versions) faa.gov PDF
L-1011-500 Fuel Consumption Charts TriStar500.net PDF

 


Lockheed L-1011-Tristar 500 Cutaway

 

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