Lockheed L-1011 Tristar 1

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

The Lockheed L-1011 Tristar 1 was the first production model of the L-1011, an American medium-to-long-range, wide-body trijet airliner of Lockheed Corporation.

Specifications

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Lockheed L-1011 Tristar 1 Specifications

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General

ICAO aircraft code
L101
Manufacturer
Lockheed Martin Aeronautics
Manufactured
1968 - 1983
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:
520 Kts
963 Km/h
Approach Speed (Vref):
108 Kts
Travel range:
4,250 Nm
7,871 Kilometers
Service Ceiling:
42,000 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:
200,000 Kg
440,920 lbs
Max Landing Weight:
158,000 Kg
348,327 lbs
Max Payload:
33,656 Kg
74,198 lbs
Fuel Tank Capacity:
23,814 gallon
90,146 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 1

The Lockheed L-1011 Tristar 1 was the first production model of the L-1011, an American medium-to-long-range, wide-body trijet airliner of Lockheed Corporation. It was the third wide-body airliner in commercial operations and has a seating capacity of up to four hundred passengers with a maximum range of 4,250 Nms.

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