Lockheed L-1011 Tri Star

1970

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Lockheed L-1011 Tri Star

The Lockheed L-1011 TriStar was the third widebody passenger jet airliner to reach the marketplace, following the Boeing 747 "jumbo jet" and the Douglas DC-10. In the 1960s, American Airlines approached Lockheed and competitor Douglas with a need for an aircraft smaller than the existing 747, but still capable of flying to distant locales such as London, the Caribbean, and Latin America from company hubs in Dallas/Ft Worth and New York. Lockheed answered the call with the TriStar. Ironically, American Airlines never flew the "Ten Eleven," purchasing many DC-10s instead.

First flown on November 16, 1970, the twin-aisle TriStar was considered a technological marvel of its day, featuring low noise emissions, improved reliability, and efficient operation. The main visible difference between the TriStar and DC-10 is in the middle/tail engine; the DC-10's engine is external for more power, while the TriStar's engine is integrated into the tail through an S-duct (similar to the Boeing 727) for improved quietness and stability. Although the TriStar's design schedule closely followed that of its fierce competitor, the DC-10, Douglas beat Lockheed to market by a year due to delays in powerplant development. Rolls-Royce, the maker of the TriStar's RB211 turbofan engines, had filed for bankruptcy, halting L-1011 final assembly. The British government did not approve the large state subsidy used to restart Rolls-Royce operations until after the U.S. government had guaranteed the Lockheed loans previously provided to Rolls for the extensive engine contract. (The UK Goverment also took the contentious step (for a Conservative administration) of taking the aero-engine side of RR into public ownership, to maintain national defence capability). The first TriStar was finally delivered to Eastern Airlines on April 26, 1972.

Designed for a maximum seating of 400 passengers, the TriStar utilized a new engine layout: in addition to Rolls-Royce turbofan jet engines on each wing, a third engine was located dorsally below the vertical stabilizer. Manufactured in Lockheed facilities in Palmdale, California, the TriStar faced brisk competition with the Boeing 747 and, even more directly, the Douglas (later McDonnell Douglas) DC-10/MD-10, which it closely resembled. The TriStar had a better safety record than the DC-10, and Trans World Airlines heralded the TriStar as one of the safest airplanes in the world in some of its promotional literature in the 1980s when concern over the safety record of the DC-10, which was flown by most of its competitors, was at its peak. However, the DC-10 outsold the TriStar nearly two to one, partly because of the TriStar's delayed introduction.

A longer-range variant of the standard-length L-1011 was developed in the late 1970s. Designated the L-1011-500, the fuselage length was shortened by 14 feet (4.3 m) to accommodate higher fuel loads.

Lockheed manufactured a total of 250 TriStars, ceasing production in 1984. Lockheed needed to sell 500 planes to break even. Failing to achieve profitability in the civilian airliner sector, the TriStar was to be Lockheed's last commercial aircraft. Airlines played Douglas and Lockheed off each other, driving the prices of both planes down, and the end result was Douglas' merger with McDonnell and Lockheed's departure from the commercial aircraft business.

Lockheed L-1011 Tri Star

Specification 
 CREW2-3
 PASSENGERS256-345
 ENGINE3 x Rolls-Royce RB-211, 180.5kN
 WEIGHTS
  Take-off weight185500 kg408960 lb
  Empty weight102000 kg224873 lb
 DIMENSIONS
  Wingspan47.4 m156 ft 6 in
  Length54.0 m177 ft 2 in
  Height16.9 m55 ft 5 in
  Wing area312.1 m23359.41 sq ft
 PERFORMANCE
  Max. speed965 km/h600 mph
  Range w/max payload5000 km3107 miles

Comments1-20 21-40
L10tristar Captain, 27.10.2010 23:50

I flew all variants of the L1011 from 1984 through 2005 and loved them all, especially the -500 version. Wonderful, magical, dependable aircraft. The RB211 engine never let me down.

reply

John Bissonnette, e-mail, 22.01.2010 02:38

having flown the Tristar for 15yrs, I can tell you you specifications are incorrect. Just FYI, but a truely Marvouls machine

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T Hemphill, e-mail, 07.09.2010 06:42

Not mentioned during this period is Lockheed Helicopter development, The Model 286 rigid rotor also a jet powered with wings version of the 286 set a speed record of 302 mph and there was the AH56A Cheyenne a winged helicopter with turbine pusher propeller. 10 were built for the US Army, one crashed.

reply

T Hemphill, e-mail, 07.09.2010 06:41

Not mentioned during this period is Lockheed Helicopter development, The Model 286 rigid rotor also a jet powered with wings version of the 286 set a speed record of 302 mph and there was the AH56A Cheyenne a winged helicopter with turbine pusher propeller. 10 were built for the US Army, one crashed.

reply

AHM FAN, e-mail, 20.04.2009 04:43

The Airline History Museum www.airlinehistorymuseum.com in Kansas City, Missouri will own a L-1011 and have it on display from 4-26-2009 on.

kcstar.com has info about it. We also have a DC-3, L-1049G [Connie] and a Martin 404 on display. Come see us!!

reply

bill benton, e-mail, 08.04.2009 19:52

are there any L1011s that a person could take a tour of? Like a museum?

reply

Muhamed Gandura, e-mail, 04.12.2006 22:03

Dear Sirs,

How many tons are in aluminum? How many in copper? how many in steel?

Thanks for prompt reply,

Sincerely,

Muhamed Gandura

reply

Syed H. Karim, e-mail, 11.02.2007 18:53

I would like to know how many commercial passenger air lines are still using Lockheed L-1011 Tri Star in their current fleet.

Also which airlines or private maintenance companies are conducting major base check of the above said air craft and how many service ebullition and air worthiness directives are issued science 1998 till now.

We will appreciate your quick response and if possible we can get the proper guide line to learn all above.


Regards

S.H. Karim

reply

1-20 21-40

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