AD 74-17-08

final rule

Airworthiness Directives; Piper Model PA-34-200 Airplanes

AD Number
74-17-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-34-200 Airworthiness Directives; Piper Model PA-34-200 Airplanes

Unsafe Condition

Fuel line chafing and fuel leaks

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

Required Actions

Modify the fuel and instrumentation line clamping in accordance with Piper Service Bulletin No. 429 or an equivalent method approved by the FAA. Replace all damaged lines with serviceable lines of the same part number or equivalent approved by the FAA.

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

Compliance Time

within the next 50 hours' time in service after the effective date of this AD

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

Affected Aircraft

Piper Model PA-34-200 airplanes, Serial Numbers 34-7250001 to 34-7450209 inclusive

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

Federal Register Abstract

Fuel Line Clamps

Applicability Source Text

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AD Final Rules - DRS_74-17-08.html
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Details
AD Number:
74-17-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA-34-200 Airplanes
Subject:
Fuel Line Clamps
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
08/09/1974
Effective Date:
08/15/1974
Make:
Piper Aircraft Inc.
Model:
PA-34-200
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
AIR-700: Compliance & Airworthiness Division
Office of Primary Responsibility:
AIR-720: Operational Safety Branch
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 74-17-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1918

AD NUMBER:   74-17-08

SUBJECT HEADING:   Airworthiness Directives; Piper Model PA-34-200 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 15, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-17-08 PIPER: Amendment 39-1918. Applies to PA-34-200 airplanes Serial Numbers 34-7250001 to 34-7450209 inclusive, certificated in all categories.

Compliance required within the next 50 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent fuel line chafing and fuel leaks, accomplish the following:

Modify the fuel and instrumentation line clamping in accordance with Piper Service Bulletin No. 429 or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region. Replace all lines that have been damaged by chafing, wear, with serviceable lines of the same part number or equivalent lines approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration Southern Region.

This amendment becomes effective August 15, 1974.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_74-17-08.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
74-17-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA-34-200 Airplanes
Subject:
Fuel Line Clamps
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
08/09/1974
Effective Date:
08/15/1974
Make:
Piper Aircraft Inc.
Model:
PA-34-200
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
AIR-700: Compliance & Airworthiness Division
Office of Primary Responsibility:
AIR-720: Operational Safety Branch
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 74-17-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1918

AD NUMBER:   74-17-08

SUBJECT HEADING:   Airworthiness Directives; Piper Model PA-34-200 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 15, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-17-08 PIPER: Amendment 39-1918. Applies to PA-34-200 airplanes Serial Numbers 34-7250001 to 34-7450209 inclusive, certificated in all categories.

Compliance required within the next 50 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent fuel line chafing and fuel leaks, accomplish the following:

Modify the fuel and instrumentation line clamping in accordance with Piper Service Bulletin No. 429 or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region. Replace all lines that have been damaged by chafing, wear, with serviceable lines of the same part number or equivalent lines approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration Southern Region.

This amendment becomes effective August 15, 1974.

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.