AD 85-05-04

final rule

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

AD Number
85-05-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

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

Loss of flight control capability due to loss of three out of four hydraulic systems.

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

Required Actions

Modify hydraulic system 'C' by installing a hydraulic fuse and associated hydraulic tubing, replace aluminum return lines with steel lines in accordance with specified service bulletins.

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

Compliance Time

Within one year 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 Model L-1011-385 series airplanes, certificated in all categories.

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

Federal Register Abstract

Hydraulic System

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_85-05-04.html
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Details
AD Number:
85-05-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes
Subject:
Hydraulic System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/01/1985
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Superseded AD: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Superseded By: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: 85-05-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5010

AD NUMBER:   85-05-04

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

ACTION:  

SUMMARY:  

DATES:   Effective April 1, 1985.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
85-05-04 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-5010. Applies to Lockheed Model L-1011-385 series airplanes, certificated in all categories. Compliance required as indicated unless previously accomplished.

To minimize potential for the loss of flight control capability due to the loss of three out of four hydraulic systems accomplish the following:

A. Within one year after the effective date of this AD, modify hydraulic system "C" by installing a hydraulic fuse and associated hydraulic tubing and replace aluminum return lines with steel lines in accordance with Lockheed L-1011 Service Bulletins Number 093-29-065, Revision 4, dated August 9, 1983, and 093-29-085, dated December 8, 1983, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Lockheed-California Company, P.O. Box 551, Burbank, California 91520, Attention: Commercial Support Contracts, Dept. 63-11, U-33, B-1. These documents also may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington or the Los Angeles Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California.

This amendment becomes effective April 1, 1985.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_85-05-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
85-05-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes
Subject:
Hydraulic System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/01/1985
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: 85-05-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5010

AD NUMBER:   85-05-04

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

ACTION:  

SUMMARY:  

DATES:   Effective April 1, 1985.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
85-05-04 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-5010. Applies to Lockheed Model L-1011-385 series airplanes, certificated in all categories. Compliance required as indicated unless previously accomplished.

To minimize potential for the loss of flight control capability due to the loss of three out of four hydraulic systems accomplish the following:

A. Within one year after the effective date of this AD, modify hydraulic system "C" by installing a hydraulic fuse and associated hydraulic tubing and replace aluminum return lines with steel lines in accordance with Lockheed L-1011 Service Bulletins Number 093-29-065, Revision 4, dated August 9, 1983, and 093-29-085, dated December 8, 1983, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Lockheed-California Company, P.O. Box 551, Burbank, California 91520, Attention: Commercial Support Contracts, Dept. 63-11, U-33, B-1. These documents also may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington or the Los Angeles Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California.

This amendment becomes effective April 1, 1985.

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.