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Lockheed L-1011 TriStar specs
Last updated: 8 August 2013
Manufacturer:Lockheed
Country: United States of America
ICAO Type designator:L101
First flight:16 November 1970
Production ended: 1983
Production total:250
Series: Lockheed L-1011 TriStar 1: First production model
Lockheed L-1011 TriStar 100: TriStar 1 with new center fuel tank and higher gross weights
Lockheed L-1011 TriStar 150: TriStar 1 conversion to increase MTOW
Lockheed L-1011 TriStar 200: TriStar 100 with Rolls-Royce RB.211-524B engines
Lockheed L-1011 TriStar 250: TriStar 100/200 conversion to increase MTOW
Lockheed L-1011 TriStar 500: Fuselage length shortened by 14 feet (4.3 m) and MTOW increased
Propulsion:3 jet engines
Maximum number of passengers:400
Maximum take-off mass:234260 kg
ICAO Mass group:4
Design Service Objective:115500 flights
Design Service Objective:210000 flight hours
Design Service Objective:20 years

Lockheed L-1011 TriStar photo

Lockheed L-1011 TriStar file photo (photo: Aviation Safety Network archives)