AD 59-13-02

final rule

Airworthiness Directives; Piper Models PA-24 and PA-24 "250" Aircraft

AD Number
59-13-02
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 Piper Aircraft Inc. PA-24 Airworthiness Directives; Piper Models PA-24 and PA-24 "250" Aircraft
aircraft Piper Aircraft Inc. PA-24-250 Airworthiness Directives; Piper Models PA-24 and PA-24 "250" Aircraft

Unsafe Condition

Cracks have developed in the aileron balance weight attachment bulkheads, which are riveted to the front spar of the aileron and support the balance weight arm.

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

Required Actions

Install reinforced bulkheads on both ailerons except on Serial Number 24-980, where only the right aileron's balance weight attachment bulkhead needs replacement.

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

Compliance Time

within the next 100 hours of operation or by October 1, 1959, whichever occurs first

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

Affected Aircraft

Piper Models PA-24 and PA-24-250 Aircraft with serial numbers 24-1 to 24-978 inclusive and 24-980.

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

Federal Register Abstract

Aileron Balance Weight

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_59-13-02.html
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Details
AD Number:
59-13-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-24 and PA-24 "250" Aircraft
Subject:
Aileron Balance Weight
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
07/09/1959
Effective Date:
Make:
Piper Aircraft Inc.
Model:
PA-24 | PA-24-250
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Superseded AD: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Superseded By: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: 59-13-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   59-13-02

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-24 and PA-24 "250" Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
59-13-02 PIPER: Applies to Models PA-24 and PA-24 "250" Aircraft Serial Numbers 24-1 to 24-978 Inclusive and 24-980.

Compliance required within the next 100 hours of operation or by October 1, 1959, whichever occurs first.

Service experience indicates that cracks have developed in the aileron balance weight attachment bulkheads. These bulkheads are riveted to the front spar of the aileron and are the supports to which the balance weight arm is attached. To reduce the probability of failure of the aileron balance weight arm attachment install reinforced bulkheads on both ailerons except on Serial Number 24-980 replace the balance weight attachment bulkhead on right aileron only.

(Piper Service Bulletin No. 173 also covers this subject and states "Service Kit, Part Number 734-233, is available from your nearest Piper distributor or dealer free of charge if the airframe serial number is included on the purchase order.")

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_59-13-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
59-13-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-24 and PA-24 "250" Aircraft
Subject:
Aileron Balance Weight
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
07/09/1959
Effective Date:
Make:
Piper Aircraft Inc.
Model:
PA-24 | PA-24-250
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: 59-13-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   59-13-02

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-24 and PA-24 "250" Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
59-13-02 PIPER: Applies to Models PA-24 and PA-24 "250" Aircraft Serial Numbers 24-1 to 24-978 Inclusive and 24-980.

Compliance required within the next 100 hours of operation or by October 1, 1959, whichever occurs first.

Service experience indicates that cracks have developed in the aileron balance weight attachment bulkheads. These bulkheads are riveted to the front spar of the aileron and are the supports to which the balance weight arm is attached. To reduce the probability of failure of the aileron balance weight arm attachment install reinforced bulkheads on both ailerons except on Serial Number 24-980 replace the balance weight attachment bulkhead on right aileron only.

(Piper Service Bulletin No. 173 also covers this subject and states "Service Kit, Part Number 734-233, is available from your nearest Piper distributor or dealer free of charge if the airframe serial number is included on the purchase order.")

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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