AD 51-10-02

final rule

Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft

AD Number
51-10-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Don Luscombe Aviation History Foundation, Inc. 8 Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft
aircraft Don Luscombe Aviation History Foundation, Inc. 8A Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft
aircraft Don Luscombe Aviation History Foundation, Inc. 8B Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft
aircraft Don Luscombe Aviation History Foundation, Inc. 8C Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft
aircraft Don Luscombe Aviation History Foundation, Inc. 8D Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft
aircraft Don Luscombe Aviation History Foundation, Inc. 8E Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft
aircraft Don Luscombe Aviation History Foundation, Inc. 8F Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft
aircraft Don Luscombe Aviation History Foundation, Inc. T-8F Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft

Unsafe Condition

Recurring failures of the control cables due to damage from passing over pulleys or through fairleads.

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

Required Actions

Inspect control cables at sections passing over pulleys or through fairleads, remove cables to expose sections for inspection without damaging them, replace unairworthy cables, check and adjust control system rigging, and ensure cables do not drag or rub against structure or equipment.

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

Compliance Time

By the next periodic inspection, but not later than June 1, 1951, and at each annual recertification thereafter.

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

Affected Aircraft

LUSCOMBE Model 8 Series Aircraft (Models 8, 8A, 8B, 8C, 8D, 8E, 8F, T-8F)

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

Federal Register Abstract

Control Cable Inspection

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_51-10-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
51-10-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft
Subject:
Control Cable Inspection
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Don Luscombe Aviation History Foundation, Inc.
Model:
8 | 8A | 8B | 8C | 8D | 8E | 8F | T-8F
Product Type:
Aircraft
Product Subtype:
Small 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: 51-10-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   51-10-02

SUBJECT HEADING:   Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
51-10-02 LUSCOMBE: Applies to All Model 8 Series Aircraft.

Compliance required by the next periodic inspection, but not later than June 1, 1951, and at each annual recertification thereafter.

Due to recurring failures of the control cables, all cables should be carefully inspected at each section which passes either over a pulley or through a fairlead. To properly inspect the cables, they should be removed from the airplane to the extent necessary to expose the sections to be inspected. Care should be taken that the method of inspection is not damaging to the cable; i.e., do not sharply bend any strand or the whole cable and do not "bird-cage" the cable to the extent of putting permanent set in the strands or the whole cable. Any unairworthy cables must be replaced.

In reinstalling the control cables, the rigging of the entire control system should be checked and properly adjusted. The control surface travels may be obtained from Aircraft Specification A-694. Care should be taken that none of the cables drag across or rub against any structure or equipment due to misalignment of the fairleads. Luscombe Airplane Corp. Service Bulletin No. 1-51 furnishes further information on this subject and Luscombe Airplane Corp., Garland, Texas, should be contacted for further information, if needed, in rigging controls.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_51-10-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
51-10-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft
Subject:
Control Cable Inspection
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Don Luscombe Aviation History Foundation, Inc.
Model:
8 | 8A | 8B | 8C | 8D | 8E | 8F | T-8F
Product Type:
Aircraft
Product Subtype:
Small 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: 51-10-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   51-10-02

SUBJECT HEADING:   Airworthiness Directives; LUSCOMBE Model 8 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
51-10-02 LUSCOMBE: Applies to All Model 8 Series Aircraft.

Compliance required by the next periodic inspection, but not later than June 1, 1951, and at each annual recertification thereafter.

Due to recurring failures of the control cables, all cables should be carefully inspected at each section which passes either over a pulley or through a fairlead. To properly inspect the cables, they should be removed from the airplane to the extent necessary to expose the sections to be inspected. Care should be taken that the method of inspection is not damaging to the cable; i.e., do not sharply bend any strand or the whole cable and do not "bird-cage" the cable to the extent of putting permanent set in the strands or the whole cable. Any unairworthy cables must be replaced.

In reinstalling the control cables, the rigging of the entire control system should be checked and properly adjusted. The control surface travels may be obtained from Aircraft Specification A-694. Care should be taken that none of the cables drag across or rub against any structure or equipment due to misalignment of the fairleads. Luscombe Airplane Corp. Service Bulletin No. 1-51 furnishes further information on this subject and Luscombe Airplane Corp., Garland, Texas, should be contacted for further information, if needed, in rigging controls.

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.