Lockheed L-1011-385-1-15 TriStar 250
Lockheed
About
The TriStar 250 is the -100 airframe given the 500's strengthened wing and undercarriage, taking it to 510,000 lb take-off weight on 178,360 lb of fuel — a full-length TriStar with the long-range aeroplane's structure. The certificate reaches it not as a new build but as a conversion, under Service Bulletin 093-51-023. 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
100,771 L
Production & History
Production Status
Out of production
Manufacturing Period
1968–1984
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