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Lockheed L-1011-385-3 TriStar 500 Specifications

The TriStar 500 is a three-engined wide-body aircraft. Announced in November 1975, this model first flew in 16 October 1978. It was designed by Lockheed as a true long-range aircraft with a shortened fuselage with less 4.1 m in comparison with standard TriStars. It also has a larger wingspan and 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: 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
Flight Crew: 2 Pilots + 1 Flight Engineer

 

DOCUMENT SOURCE FORMAT
Type Certificate Data Sheet A23WE faa.gov pdf
L-1011-500 Fuel Consumption Charts tristar500.net pdf

 


Lockheed L-1011-Tristar 500 cutaway

Last updated: 03-05-2012
 

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