AD 99-08-20

final rule

Airworthiness Directives; Lockheed Model L-1011-385 Series Airplanes

AD Number
99-08-20
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-NM-315-AD
FR Citation
Federal Register: April 14, 1999 (Volume 64, Number 71)
Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

Applicability

TypeManufacturerModelDetails
aircraft Lockheed Martin Corporation L-1011-385-1 Airworthiness Directives; Lockheed Model L-1011-385 Series Airplanes
aircraft Lockheed Martin Corporation L-1011-385-1-14 Airworthiness Directives; Lockheed Model L-1011-385 Series Airplanes
aircraft Lockheed Martin Corporation L-1011-385-1-15 Airworthiness Directives; Lockheed Model L-1011-385 Series Airplanes
aircraft Lockheed Martin Corporation L-1011-385-3 Airworthiness Directives; Lockheed Model L-1011-385 Series Airplanes

Unsafe Condition

Bulkhead Fuselage Inspection

Affected Aircraft

Lockheed Model L-1011-385 Series Airplanes

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Bulkhead Fuselage Inspection

Applicability Source Text

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Document Text

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United States Department of Transportation
About DOTOur ActivitiesAreas of Focus
FAA
Dynamic Regulatory System
A Comprehensive Knowledge Center of Regulatory and Guidance Material from the Office of
Aviation Safety and other Services and Offices

Welcome, Guest

Sign In
Search
What's New
DRS Feedback
Home
Technical issue with the system
There is a technical issue with the system. Please try again later.

U.S. Department of Transportation

Federal Aviation Administration

800 Independence Avenue, SW

Washington, DC 20591

(866) TELL-FAA | (866) 835-5322

Privacy Policy
Accessibility

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

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