Editing Lockheed L-1011 TriStar (section)

===L-1011-200===
[[File:Saudi Arabian Airlines L-1011-200 HZ-AHE LHR 1985-5-17.png|thumb|A [[Saudia]] L-1011-200 TriStar at [[London Heathrow Airport]], 1985]]

The L-1011-200 (FAA certification L-1011-385-1-15), the third production model of the L-1011, was introduced in 1976. Although otherwise similar to the -100, the -200 uses [[Rolls-Royce RB.211]]-524B engines to improve its performance in hot and high-altitude conditions. Gulf Air used -200 models to replace its earlier-generation [[Vickers VC10]] fleet.

Other than the engines, the basic TriStar -200 is identical to the -100, with center-section fuel, having a MTOW of {{convert|466000|lb|kg}}, and fuel capacity of {{convert|26400|usgal|L}} as the -100. An increase of gross weight to {{convert|474000|lb|kg}} is possible, with the heavier aircraft offered by Lockheed as -200I or -200(Improved).  [[Saudi Arabian Airlines]] (Saudia) was a launch customer for the -200 series and operated a sizable fleet until 1998. A total of 24 L-1011-200 aircraft were built new, with the first delivered to Saudia on May 28, 1977. Like other TriStar improvements, a conversion program has also been offered.