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 nautical miles.

Lockheed Martin Aeronautics
United States
1968 to: 1983
US$20 million (1972)
L-1011 Avionics Flight Control System
3x Rolls-Royce RB211-22
42,000 pound-force
Max Cruise Speed:
520 knots
963 Km/h
Approach Speed (Vref):
108 knots
Travel range:
4,250 Nautical Miles
7,871 Kilometers
Fuel Economy:
Service Ceiling:
42,000 feet
Rate of Climb:
2800 feet / minute
14.22metre / second
Take Off Distance:
2350 metre - 7,709.88 feet
Landing Distance:
1960 metre - 6,430.37 feet
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 litre
Baggage Volume:
97.2 m3 / 3,433 ft3
Seats - Economy / General:
400 seats
Seats - Business Class:
Seats - First Class:
Cabin Height:
2.7 metre - 8.86 feet
Cabin Width:
5.77 metre - 18.93 feet
Cabin Length:
33 metre - 108.27 feet
Exterior Length:
54.17 metre - 177.72 feet
Tail height:
16.87 metre - 55.35 feet
Fuselage Diameter:
5.97 metre - 19.59 feet
Wing Span / Rotor Diameter:
47.35 metre - 155.35 feet
Wing Tips:
No Winglets

In the mid-1960s, when American Airlines had a requirement for an airliner that could accommodate 250 passengers on transcontinental routes, Lockheed Corporation and its competitor Douglas Aircraft responded. Since 1961’s L-188 Electra, Lockheed had not produced any civilian airliners again and just focused on military transports.

However, having suffered problems with several of their military programs, the company desired to re-enter the civilian market with a smaller wide-body jet, named as the L-1011 Tristar. Douglas Aircraft produced the DC-10 which had the same three-engine configuration and dimensions.

Despite their resemblance, the two aircraft’s engineering approaches were different. Douglas focused on developing an economical DC-10 aircraft while Lockheed created a costly but technologically-advanced L-1011-1. The aircraft produces lower noise emissions, enhanced reliability, and greater efficiency over first-generation jet airliners. The L-1011-1 was named as Tristar due to a Lockheed employee naming contest for the airliner.

The first production model of the airliner was the L-1011-1 which was designed for short and medium-range flight. This initial model served as the basis for the succeeding versions such as the L-1011-100, L-1011-50, L-1011-150, L-1011-200, L-1011-250, and L-1011-500. The L-1011-1 was acquired by several airlines such as Air Canada, All Nippon Airways, Cathay Pacific, Eastern Airlines, and other operators with regional trunk routes that need a widebody aircraft. Two L-101101 were purchased by Pacific Southwest Airlines configured with lower deck seats. This version was also one of the few widebody aircraft to be fitted with an optional full-height built-in airstair.

On April 5, 1972, the aircraft was first delivered to Eastern Airlines. In 1983, production ended with a total of 160 L-1011-1 Tristars built. Most of the aircraft were sold to US operators, with just a combination of 110 orders from Delta Airlines, Eastern Airlines, and Trans World Airlines.

The L-1011-1 is powered by three Rolls-Royce RB211-22 turbofan engines with a maximum thrust of 42,000 lbf each.

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