AD 74-26-06

final rule

LOCKHEED-CALIFORNIA Model L-1011-385-1 Series Airplanes

AD Number
74-26-06
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 Model L-1011-385-1 Series Airplanes

Unsafe Condition

An unknown incipient failure condition in the housing of the fire pull handle assembly, P/N 1520324 or P/N 1580810, could occur.

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

Required Actions

Modify the Control Panel Assembly per Part 2 of Lockheed Service Bulletin 093-26-010, and re-identify modified assemblies per Part 3B of the same service bulletin. Equivalent repairs or modifications may be approved by the FAA.

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

Compliance Time

Within 600 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 Model L-1011-385-1 Series Airplanes with Engine Shutoff Control Panel Assemblies P/N 1520324 or P/N 1580810

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

Federal Register Abstract

Fire Pull Handle Assembly

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
74-26-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED-CALIFORNIA Model L-1011-385-1 Series Airplanes
Subject:
Fire Pull Handle Assembly
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/04/1975
Make:
Lockheed Martin Corporation
Model:
L-1011-385-1
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Superseded AD: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Superseded By: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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 74-26-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2104

AD NUMBER:   74-26-06

SUBJECT HEADING:   LOCKHEED-CALIFORNIA Model L-1011-385-1 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 4, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-26-06 LOCKHEED-CALIFORNIA: Amendment 39-2049 as amended by Amendment 39-2104. Applies to all L-1011-385-1 Series Airplanes certificated in all categories, incorporating Engine Shutoff Control Panel Assemblies, P/N 1520324 or P/N 1580810, all configurations.

Compliance required as indicated, unless already accomplished.

To provide protection in the event of an unknown incipient failure condition in the housing of the fire pull handle assembly, P/N 1520324 or P/N 1580810, accomplish the following:

(1) Within 600 hours time in service after the effective date of this AD, as amended,

(a) Modify the Control Panel Assembly, P/N 1520324 or P/N 1580810, in accordance with Part 2 of Lockheed Service Bulletin 093-26-010, dated November 21, 1974, revised February 11, 1975 or later FAA-approved revisions.

(b) Re-identify all modified Control Panel Assemblies in accordance with Part 3B of Lockheed Service Bulletin 093-26-010, dated November 21, 1974, revised February 11, 1975, or later FAA-approved revisions.

(2) Equivalent repairs or modifications may be approved by the Chief, Aircraft Engineering Division, FAA Western Region, upon submission of adequate substantiating data.

Note: Those engine shutoff control panel assemblies marked as P/N 1604009 or P/N 1605009 are in compliance with this AD.

Amendment 39-2049 was effective December 23, 1974.

This amendment 39-2104 to AD 74-26-06 becomes effective March 4, 1975.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_74-26-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
74-26-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED-CALIFORNIA Model L-1011-385-1 Series Airplanes
Subject:
Fire Pull Handle Assembly
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/04/1975
Make:
Lockheed Martin Corporation
Model:
L-1011-385-1
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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 74-26-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2104

AD NUMBER:   74-26-06

SUBJECT HEADING:   LOCKHEED-CALIFORNIA Model L-1011-385-1 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 4, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-26-06 LOCKHEED-CALIFORNIA: Amendment 39-2049 as amended by Amendment 39-2104. Applies to all L-1011-385-1 Series Airplanes certificated in all categories, incorporating Engine Shutoff Control Panel Assemblies, P/N 1520324 or P/N 1580810, all configurations.

Compliance required as indicated, unless already accomplished.

To provide protection in the event of an unknown incipient failure condition in the housing of the fire pull handle assembly, P/N 1520324 or P/N 1580810, accomplish the following:

(1) Within 600 hours time in service after the effective date of this AD, as amended,

(a) Modify the Control Panel Assembly, P/N 1520324 or P/N 1580810, in accordance with Part 2 of Lockheed Service Bulletin 093-26-010, dated November 21, 1974, revised February 11, 1975 or later FAA-approved revisions.

(b) Re-identify all modified Control Panel Assemblies in accordance with Part 3B of Lockheed Service Bulletin 093-26-010, dated November 21, 1974, revised February 11, 1975, or later FAA-approved revisions.

(2) Equivalent repairs or modifications may be approved by the Chief, Aircraft Engineering Division, FAA Western Region, upon submission of adequate substantiating data.

Note: Those engine shutoff control panel assemblies marked as P/N 1604009 or P/N 1605009 are in compliance with this AD.

Amendment 39-2049 was effective December 23, 1974.

This amendment 39-2104 to AD 74-26-06 becomes effective March 4, 1975.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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