AD 76-14-04

final rule
Data completeness: 70%

LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes

AD Number
76-14-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Lockheed Martin Corporation L-1011-385-1 LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes
aircraft Lockheed Martin Corporation L-1011-385-1-14 LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes
aircraft Lockheed Martin Corporation L-1011-385-1-15 LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes
aircraft Lockheed Martin Corporation L-1011-385-3 LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes

Unsafe Condition

In-flight losses of the main landing gear fixed and hinged strut doors.

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Required Actions

Modify the landing gear maximum extend speed placard to reduce VLE to 250 KIAS/0.73M; amend the Airplane Flight Manual's Limitations Section with new VLO and VLE speeds and operational restrictions; perform visual integrity inspections of the main landing gear doors every 800 hours' time in service; and incorporate specified Service Bulletins within 9000 hours' time in service.

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Compliance Time

Within the next 300 hours' time in service after the effective date for paragraph (a), within the next 800 hours' time in service after the effective date for paragraph (b), and within the next 9000 hours' time in service after the effective date for paragraph (c).

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Affected Aircraft

Lockheed-California Company Model L-1011-385 series airplanes, including L-1011-385-1, L-1011-385-1-14, L-1011-385-1-15, and L-1011-385-3, certificated in all categories.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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