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