AD 47-10-08

final rule

LOCKHEED Model 49

AD Number
47-10-08
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 Aircraft Corporation 49-46 LOCKHEED Model 49

Unsafe Condition

The elevator booster shifter horn assembly's teeth on 278488 gear may have insufficient width due to inadequate manufacturing tolerances, leading to potential gear tooth failure.

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

Required Actions

Rework the elevator booster shifter horn assembly by reducing the width of the teeth on 278488 gear by 0.120 inch from each end of all teeth.

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

Compliance Time

prior to August 9, 1946

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

Affected Aircraft

Lockheed Aircraft Corporation Model 49 serial numbers 1975 to 1978, inclusive; 1980; and 2021 to 2059, inclusive.

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

Federal Register Abstract

Elevator Booster Shifter Horn

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_47-10-08.html
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Details
AD Number:
47-10-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED Model 49
Subject:
Elevator Booster Shifter Horn
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Lockheed Aircraft Corporation
Model:
49-46
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Superseded AD: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Superseded By: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: 47-10-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-10-08

SUBJECT HEADING:   LOCKHEED Model 49

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
47-10-08 LOCKHEED: (Was Mandatory Note 9 of AD-763-3.) Applies Only to Model 49 Serial Numbers 1975 to 1978, Inclusive; 1980; and 2021 to 2059, Inclusive.

Compliance required prior to August 9, 1946.

Rework the elevator booster shifter horn assembly by reducing the width of the teeth on 278488 gear. 0.120 inch should be removed from each end of all the teeth.

(LAC Service Bulletin 049/SB-19 covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_47-10-08.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
47-10-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED Model 49
Subject:
Elevator Booster Shifter Horn
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Lockheed Aircraft Corporation
Model:
49-46
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: 47-10-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-10-08

SUBJECT HEADING:   LOCKHEED Model 49

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
47-10-08 LOCKHEED: (Was Mandatory Note 9 of AD-763-3.) Applies Only to Model 49 Serial Numbers 1975 to 1978, Inclusive; 1980; and 2021 to 2059, Inclusive.

Compliance required prior to August 9, 1946.

Rework the elevator booster shifter horn assembly by reducing the width of the teeth on 278488 gear. 0.120 inch should be removed from each end of all the teeth.

(LAC Service Bulletin 049/SB-19 covers this same subject.)

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.