AD 81-26-06

final rule

LOCKHEED-CALIFORNIA COMPANY Model L-1011 Series Airplanes

AD Number
81-26-06
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 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

False Airborne Vibration Monitor System indications may cause an unnecessary shutdown of the number 2 engine.

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

Required Actions

Incorporate electrical system modifications per Lockheed-California Company L-1011 Service Bulletin 093-23-083 dated October 13, 1981. Alternative 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-California Company Model L-1011 series airplanes with serial numbers: 1083-1090, 1092-1097, 1099-1103, 1105-1106, 1112-1113, 1117-1119, 1121-1123, 1126-1129, 1132, 1134-1136, 1139, 1141, 1145-1147

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

Federal Register Abstract

Electrical System Modification

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_81-26-06.html
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AD Number:
81-26-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED-CALIFORNIA COMPANY Model L-1011 Series Airplanes
Subject:
Electrical System Modification
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/31/1981
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Superseded AD: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Superseded By: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: 81-26-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4283

AD NUMBER:   81-26-06

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

ACTION:  

SUMMARY:  

DATES:   Effective December 31, 1981.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
81-26-06 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-4283. Applies to Lockheed Model L-1011 series airplanes, Serial Numbers as listed below, certificated in all categories. Compliance required within 30 days after the effective date of this AD, unless previously accomplished:

A. To prevent an unnecessary shutdown of the number 2 engine due to false Airborne Vibration Monitor System indications, incorporate electrical system modifications in accordance with Part 2, Accomplishment Instructions, of Lockheed-California Company L-1011 Service Bulletin 093-23-083 dated October 13, 1981, for the following 42 aircraft:

S/N 1083-1090	S/N 1117-1119	S/N 1134-1136
S/N 1092-1097	S/N 1121-1123	S/N 1139
S/N 1099-1103	S/N 1126-1129	S/N 1141
S/N 1105-1106	S/N 1132	S/N 1145-1147
S/N 1112-1113		
B. Alternative means of compliance providing an equivalent level of safety may be used when approved by the Chief, Los Angeles Area 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.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).

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 FAA Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington 98108; or the Los Angeles Area Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California 90808.

This Amendment becomes effective December 31, 1981.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_81-26-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
81-26-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED-CALIFORNIA COMPANY Model L-1011 Series Airplanes
Subject:
Electrical System Modification
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/31/1981
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: 81-26-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4283

AD NUMBER:   81-26-06

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

ACTION:  

SUMMARY:  

DATES:   Effective December 31, 1981.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
81-26-06 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-4283. Applies to Lockheed Model L-1011 series airplanes, Serial Numbers as listed below, certificated in all categories. Compliance required within 30 days after the effective date of this AD, unless previously accomplished:

A. To prevent an unnecessary shutdown of the number 2 engine due to false Airborne Vibration Monitor System indications, incorporate electrical system modifications in accordance with Part 2, Accomplishment Instructions, of Lockheed-California Company L-1011 Service Bulletin 093-23-083 dated October 13, 1981, for the following 42 aircraft:

S/N 1083-1090	S/N 1117-1119	S/N 1134-1136
S/N 1092-1097	S/N 1121-1123	S/N 1139
S/N 1099-1103	S/N 1126-1129	S/N 1141
S/N 1105-1106	S/N 1132	S/N 1145-1147
S/N 1112-1113		
B. Alternative means of compliance providing an equivalent level of safety may be used when approved by the Chief, Los Angeles Area 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.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).

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 FAA Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington 98108; or the Los Angeles Area Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California 90808.

This Amendment becomes effective December 31, 1981.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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