Simple Flying aviation site released a recent article about the L-1011 TriStar:
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TAP Air Portugal CS-TEF © Felix Goetting |
- Simple Flying: 5 Fun Facts About The Lockheed L-1011 'TriStar'
Simple Flying aviation site released a recent article about the L-1011 TriStar:
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TAP Air Portugal CS-TEF © Felix Goetting |
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CS-TMP © Brett Hoelzer/Deep Blue Dive Center |
The venerable old Lockheed Martin L1011 Tristar airplane, with its three engines, mounted on wings and tail fin, would be a sight to behold in the air or on the ground, let alone deep beneath the surface of the Red Sea, among the fish and coral.
The abandoned jet, sunk in 2019 to create an artificial reef to encourage marine life, has been photographed by American underwater photographer Brett Holzer in a series of images that capture the eerie spectacle created by this aquatic airliner.
YQB Aviation published a nice article about the L-1011 history in Canada:
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Air Canada L-1011 © YQB Aviation |
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Thai Sky L-1011 © Sam Chui |
Key.Aero published an article evoking the 50 years since the first flight of the Lockheed L-1011 TriStar.
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N1011 © Jon Proctor |
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Aviation News / November 2020 |
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Aviation News - June 2018 |
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Delta L-1011 ad |
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Flying tail |
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Aviation News - December 2016 |
TriStar: A Widebody Pioneer
The L-1011 TriStar was the only jet airliner ever built by Lockheed. Philip Birtles details the development and career of this tri-jet.
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Self-dimming windows © AirlineReporter/Lockheed |
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Airways Magazine - November 2014 |
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L-1011 © Lockheed Martin |
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euroAtlantic airways magazine |
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Aviation News - March 2014 |
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Jets Monthly - May 2012 |
Summary: We are adopting a new airworthiness directive (AD) for certain Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model L-1011-385-1, L-1011-385-1-14, L-1011-385-1-15, and L-1011-385-3 airplanes. This AD was prompted by results from a damage tolerance analysis conducted by the manufacturer indicating that fatigue cracking could occur in wing rear spar and upper surface zones. This AD requires repetitive inspections for cracking of the wing rear spar and upper surface zones, and repair if necessary. We are issuing this AD to detect and correct such fatigue cracking, which could result in cracking that grows large enough to reduce the wing strength below certificated requirements and possibly cause fracture of the rear spar, resulting in extensive damage to the wing and possible fuel leaks.