AD 48-13-04

final rule

Airworthiness Directives; Piper Model PA-12 Aircraft

AD Number
48-13-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

Applicability

TypeManufacturerModelDetails
aircraft FS 2003 Corp. PA-12 Airworthiness Directives; Piper Model PA-12 Aircraft

Unsafe Condition

Arcing between the fuse clip and the wire attachment plate on the fuse block caused by loosening of the fuse clip attaching rivets.

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

Required Actions

Replace rivets with No. 4 machine screws and stake threads.

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

Compliance Time

May 1, 1948

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

Affected Aircraft

PA-12 Aircraft Serial Numbers 12-1 Through 12-3450; 12-3452; 12-3454 Through 12-3467; 12-3469 Through 12-3471; 12-3473 Through 12-3504; 12-3506; 12-3507; 12-3511 Through 12-3520; 12-3522 Through 12-3531; 12-3533; 12-3535 Through 12-3543; 12-3545 Through 12-3548; 12-3553; 12-3901 Through 12-3958; 12-3960 Through 12-3962; 12-3965 Through 12-3976; 12-3983; 12-3984; 12-3988; 12-3990 Through 12-3994.

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

Federal Register Abstract

Fuse-Clip Attachment

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
48-13-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA-12 Aircraft
Subject:
Fuse-Clip Attachment
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
FS 2003 Corp.
Model:
PA-12
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Superseded AD: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Superseded By: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: 48-13-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   48-13-04

SUBJECT HEADING:   Airworthiness Directives; Piper Model PA-12 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
48-13-04 PIPER: Applies to PA-12 Aircraft Serial Numbers 12-1 Through 12-3450; 12- 3452; 12-3454 Through 12-3467; 12-3469 Through 12-3471; 12-3473 Through 12-3491; 12- 3993 Through 12-3504; 12-3506; 12-3507; 12-3511 Through 12-3520; 12-3522 Through 12- 3531; 12-3533; 12-3535 Through 12-3543; 12-3545 Through 12-3548; 12-3553; 12-3901 Through 12-3958; 12-3960 Through 12-3962; 12-3965 Through 12-3976; 12-3983; 12-3984; 12- 3988; 12-3990 Through 12-3994.

Compliance required by May 1, 1948.

To avoid arcing between the fuse clip and the wire attachment plate on the fuse block caused by loosening of the fuse clip attaching rivets, replace rivets by No. 4 machine screws and stake threads.

(Piper Service Bulletin No. 105 dated February 18, 1948, covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_48-13-04.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
48-13-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA-12 Aircraft
Subject:
Fuse-Clip Attachment
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
FS 2003 Corp.
Model:
PA-12
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: 48-13-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   48-13-04

SUBJECT HEADING:   Airworthiness Directives; Piper Model PA-12 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
48-13-04 PIPER: Applies to PA-12 Aircraft Serial Numbers 12-1 Through 12-3450; 12- 3452; 12-3454 Through 12-3467; 12-3469 Through 12-3471; 12-3473 Through 12-3491; 12- 3993 Through 12-3504; 12-3506; 12-3507; 12-3511 Through 12-3520; 12-3522 Through 12- 3531; 12-3533; 12-3535 Through 12-3543; 12-3545 Through 12-3548; 12-3553; 12-3901 Through 12-3958; 12-3960 Through 12-3962; 12-3965 Through 12-3976; 12-3983; 12-3984; 12- 3988; 12-3990 Through 12-3994.

Compliance required by May 1, 1948.

To avoid arcing between the fuse clip and the wire attachment plate on the fuse block caused by loosening of the fuse clip attaching rivets, replace rivets by No. 4 machine screws and stake threads.

(Piper Service Bulletin No. 105 dated February 18, 1948, covers this same subject.)

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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