AD 75-08-19
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lockheed Martin Corporation | L-1011-385-1 | LOCKHEED-CALIFORNIA COMPANY Model L-1011-385-1 Series Airplanes |
| aircraft | Lockheed Martin Corporation | L-1011-385-1-14 | LOCKHEED-CALIFORNIA COMPANY Model L-1011-385-1 Series Airplanes |
| aircraft | Lockheed Martin Corporation | L-1011-385-1-15 | LOCKHEED-CALIFORNIA COMPANY Model L-1011-385-1 Series Airplanes |
Unsafe Condition
Possible hangups of the rudder pedals due to insufficient clearance in the side panel kickshield splice areas.
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Required Actions
Within 200 hours time in service after the effective date, perform a visual inspection of the flight station side panel kickshield joint areas per Service Bulletin 093-25-155. If inadequate clearance is found, perform interim modifications per the Service Bulletin or the modifications in Part II. By July 1, 1975, complete the modification to the side and center/kickshield per Part II of the Service Bulletin.
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Compliance Time
Within 200 hours time in service thereafter, and on or before July 1, 1975 for the final modification.
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Affected Aircraft
Lockheed-California Company Model L-1011-385-1 series airplanes, including L-1011-385-1, L-1011-385-1-14, L-1011-385-1-15, certificated in all categories.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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