Lockheed L-1011 Tristar 100

ICAO aircraft code L101
Country United States
New price USD 20 million (1972)

The L-1011-100 was the second production model of the American medium-to-long-range, wide-body trijet Lockheed L-1011 Tristar family.

Specifications

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Lockheed L-1011 Tristar 100 Specifications

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General

ICAO aircraft code
L101
Manufacturer
Lockheed Martin Aeronautics
Manufactured
1968 - 1984
Country
United States
New purchase price
USD 20 million (1972)

Aircraft performance

Avionics:
L-1011 Avionics Flight Control System
Engine:
3x Rolls-Royce RB211-22
Turbofan
Power:
42,000 pound-force
Max Cruise Speed:
515 Kts
954 Km/h
Approach Speed (Vref):
145 Kts
Travel range:
3,600 Nm
6,667 Kilometers
Service Ceiling:
4,200 feet
Rate of Climb:
2800 feet / minute
14.22meter / second
Take Off Distance:
2350 meter - 7,709.88 feet
Landing Distance:
1960 meter - 6,430.37 feet

Weight & dimensions

Max Take Off Weight:
211,000 Kg
465,171 lbs
Max Landing Weight:
166,000 Kg
365,964 lbs
Max Payload:
33,656 Kg
74,198 lbs
Fuel Tank Capacity:
26,502 gallon
100,321 liter
Baggage Volume:
97.2 m3 / 3,433 ft3

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

About the Lockheed L-1011 Tristar 100

The L-1011-100 was the second production model of the American medium-to-long-range, wide-body trijet Lockheed L-1011 Tristar family. The Tristar 100 was designed with a new center fuel tank and higher gross weights that extended the range of the aircraft by around 810 Nms.

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