AD 86-01-03

final rule

LOCKHEED-CALIFORNIA COMPANY Model L-1011 Series Airplanes

AD Number
86-01-03
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 Series Airplanes
aircraft Lockheed Martin Corporation L-1011-385-1-14 LOCKHEED-CALIFORNIA COMPANY Model L-1011 Series Airplanes
aircraft Lockheed Martin Corporation L-1011-385-1-15 LOCKHEED-CALIFORNIA COMPANY Model L-1011 Series Airplanes
aircraft Lockheed Martin Corporation L-1011-385-3 LOCKHEED-CALIFORNIA COMPANY Model L-1011 Series Airplanes

Unsafe Condition

Malfunction of the door emergency mode opening system could cause loss of availability of one or more passenger doors during an emergency evacuation.

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

Required Actions

Test and repair all passenger doors prior to further flight within 30 days after the effective date, in accordance with Lockheed Service Bulletin 093-52-206 or later revisions approved by the FAA. Alternate means of compliance may be used if approved by the FAA.

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

Compliance Time

Within 30 days 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 series airplanes, certificated in any category

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

Federal Register Abstract

Passenger Doors

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_86-01-03.html
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Details
AD Number:
86-01-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED-CALIFORNIA COMPANY Model L-1011 Series Airplanes
Subject:
Passenger Doors
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/21/1986
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Superseded AD: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Superseded By: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: 86-01-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5211

AD NUMBER:   86-01-03

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

ACTION:  

SUMMARY:  

DATES:   Effective January 21, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
86-01-03 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-5211. Applies to Lockheed Model L-1011 series airplanes, certificated in any category. Compliance required as indicated, unless previously accomplished within 90 days prior to the effective date of this AD.

To prevent loss of the availability of one or more passenger doors during an emergency evacuation due to malfunction of the door emergency mode opening system, accomplish the following:

A. Within 30 days after the effective date of this AD, test and repair prior to further flight, as necessary, all passenger doors in accordance with Lockheed Service Bulletin 093-52-206, dated December 20, 1985, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

B. Alternate means of compliance with this AD 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 the airplane to a base for accomplishment of the tests or modifications required by this AD.

All persons affected by this directive who have not already received the appropriate service 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 may also 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 January 21, 1986.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_86-01-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
86-01-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED-CALIFORNIA COMPANY Model L-1011 Series Airplanes
Subject:
Passenger Doors
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/21/1986
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: 86-01-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5211

AD NUMBER:   86-01-03

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

ACTION:  

SUMMARY:  

DATES:   Effective January 21, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
86-01-03 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-5211. Applies to Lockheed Model L-1011 series airplanes, certificated in any category. Compliance required as indicated, unless previously accomplished within 90 days prior to the effective date of this AD.

To prevent loss of the availability of one or more passenger doors during an emergency evacuation due to malfunction of the door emergency mode opening system, accomplish the following:

A. Within 30 days after the effective date of this AD, test and repair prior to further flight, as necessary, all passenger doors in accordance with Lockheed Service Bulletin 093-52-206, dated December 20, 1985, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

B. Alternate means of compliance with this AD 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 the airplane to a base for accomplishment of the tests or modifications required by this AD.

All persons affected by this directive who have not already received the appropriate service 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 may also 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 January 21, 1986.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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