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 |