AD 76-21-01

final rule

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

AD Number
76-21-01
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

Incorrect installation of latch pins on the latch fittings of the C-1A cargo door surround structure could result in a possible in-flight loss of the C-1A cargo door.

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

Required Actions

Install latch pin guard assemblies and related components, reidentify the latch fitting assemblies, and check proximity sensors adjustment as necessary on the C-1A cargo door surround structure following Service Bulletin 093-52-083 or equivalent.

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

Compliance Time

within the next 300 hours' time in service after the effective date of this AD

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

Affected Aircraft

Lockheed-California Company Model L-1011-385 series airplanes with C-1A cargo door installed

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

Federal Register Abstract

C-1A Cargo Doors

Applicability Source Text

Show captured applicability text from the source AD
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AD Number:
76-21-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes
Subject:
C-1A Cargo Doors
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/20/1976
Make:
Lockheed Martin Corporation
Model:
L-1011-385-1 | L-1011-385-1-14 | L-1011-385-1-15 | L-1011-385-3
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 76-21-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2745

AD NUMBER:   76-21-01

SUBJECT HEADING:   LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective November 20, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-21-01 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-2745. Applies to Lockheed Model L-1011-385 series airplanes certificated in all categories having C-1A cargo door installed.

Compliance required within the next 300 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent the latch pins on the latch fittings of the C-1A cargo door surround structure from being incorrectly installed during maintenance replacement, which could result in a possible in-flight loss of the C-1A cargo door, accomplish the following:

a. Install latch pin guard assemblies and related components, reidentify the latch fitting assemblies and check proximity sensors adjustment as necessary, on the C-1A cargo door surround structure, in accordance with Lockheed-California Company Service Bulletin 093-52-083 dated May 25, 1976, or later FAA-approved revision or equivalent modification approved by the Chief, Aircraft Engineering Division, FAA Western Region.

b. Airplanes may be flown in accordance with FAR 21.197 to a base where the modification can be performed.

This amendment becomes effective November 20, 1976.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_76-21-01.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
76-21-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes
Subject:
C-1A Cargo Doors
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/20/1976
Make:
Lockheed Martin Corporation
Model:
L-1011-385-1 | L-1011-385-1-14 | L-1011-385-1-15 | L-1011-385-3
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 76-21-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2745

AD NUMBER:   76-21-01

SUBJECT HEADING:   LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective November 20, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-21-01 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-2745. Applies to Lockheed Model L-1011-385 series airplanes certificated in all categories having C-1A cargo door installed.

Compliance required within the next 300 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent the latch pins on the latch fittings of the C-1A cargo door surround structure from being incorrectly installed during maintenance replacement, which could result in a possible in-flight loss of the C-1A cargo door, accomplish the following:

a. Install latch pin guard assemblies and related components, reidentify the latch fitting assemblies and check proximity sensors adjustment as necessary, on the C-1A cargo door surround structure, in accordance with Lockheed-California Company Service Bulletin 093-52-083 dated May 25, 1976, or later FAA-approved revision or equivalent modification approved by the Chief, Aircraft Engineering Division, FAA Western Region.

b. Airplanes may be flown in accordance with FAR 21.197 to a base where the modification can be performed.

This amendment becomes effective November 20, 1976.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.