AD 47-47-01

final rule

Airworthiness Directives; Piper Model PA-12 Aircraft

AD Number
47-47-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

Applicability

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

Unsafe Condition

The upper end of the tie strap on the landing gear may fail due to insufficient reinforcement, leading to potential structural failure of the landing gear during operation.

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

Required Actions

Reinforce the upper end of the tie strap with a 4130 steel plate (Piper No. 10028-13) by edge welding. Install a trapezoidal gusset plate (Piper No. 10028-14) on each side of the upper strap attachment by forming and edge welding on assembly.

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

Compliance Time

prior to January 15, 1948

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

Affected Aircraft

PA-12 Aircraft Serial Numbers 12-221, 12-236, 12-239, 12-244, 12-250 and Up to 12-3561 and 12-3901 to 12-3988.

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

Federal Register Abstract

Landing Gear Reinforcement

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
47-47-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA-12 Aircraft
Subject:
Landing Gear Reinforcement
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Superseded AD: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Superseded By: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: 47-47-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-47-01

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

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
47-47-01 PIPER: (Was Mandatory Note 5 of AD-780-3.) Applies to PA-12 Aircraft Serial Numbers 12-221, 12-236, 12-239, 12-244, 12-250 and Up to 12-3561 and 12-3901 to 12- 3988.

Compliance required prior to January 15, 1948.

Reinforce the upper end of the tie strap on the landing gear with a 4130 steel plate (Piper No. 10028-13). Install over end of strap by edge welding. As further reinforcement, install a trapezoidal gusset plate (Piper No. 10028-14) on each side of this upper strap attachment by forming and edge welding on assembly.

(Piper Service Bulletin No. 97 dated July 10, 1947, covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_47-47-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
47-47-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA-12 Aircraft
Subject:
Landing Gear Reinforcement
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: 47-47-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-47-01

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

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
47-47-01 PIPER: (Was Mandatory Note 5 of AD-780-3.) Applies to PA-12 Aircraft Serial Numbers 12-221, 12-236, 12-239, 12-244, 12-250 and Up to 12-3561 and 12-3901 to 12- 3988.

Compliance required prior to January 15, 1948.

Reinforce the upper end of the tie strap on the landing gear with a 4130 steel plate (Piper No. 10028-13). Install over end of strap by edge welding. As further reinforcement, install a trapezoidal gusset plate (Piper No. 10028-14) on each side of this upper strap attachment by forming and edge welding on assembly.

(Piper Service Bulletin No. 97 dated July 10, 1947, covers this same subject.)

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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