Lockheed L-1011-385-1-14 TriStar 100/200
Lockheed
Photograph of the Lockheed L-1011 TriStar family. No photograph on Wikimedia Commons identifies this variant specifically.
About
The L-1011-385-1-14 covers the TriStar 100 and 200, the longer-range developments with more fuel and, on the 200, the more powerful RB211-524 engine for hot-and-high work. It is the only one of the four certified models the certificate does not approve up to 510,000 lb: its single column stops at 466,000 lb take-off and 320,000 lb zero fuel. The cruise speed, cruise Mach, range, ceiling, climb rate, wingspan, length, height and take-off distance are EUROCONTROL's figures for the L101 type code rather than a certificate's: a type certificate states limits and weights, not cruise performance, and the source does not distinguish sub-variants.
Weightscompared to Airbus A380-800
Capacitycompared to Airbus A380-800
Passenger Capacity
47% of A380 maximum capacity
Crew
Dimensions
Length
Wingspan
Height
Engine Specifications
Engine Count
3×
Engine Model
Rolls-Royce RB211-22B-02 or RB211-524B-02 turbofan
Fuel & Cargo
Fuel Capacity
90,149 L
Production & History
Production Status
Out of production
Manufacturing Period
1968–1984
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