AD 60-05-03

final rule

Airworthiness Directives; Piper Models PA-22 "150" and PA-22 "160" Aircraft

AD Number
60-05-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-22-150 Airworthiness Directives; Piper Models PA-22 "150" and PA-22 "160" Aircraft
aircraft Piper Aircraft Inc. PA-22-160 Airworthiness Directives; Piper Models PA-22 "150" and PA-22 "160" Aircraft

Unsafe Condition

Deterioration due to heat from the rear seat heater outlet and chafing where the web attaches to the attaching lug on the front seat belt.

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

Required Actions

Install safety belt extension P/N 14920-02 or equivalent on the front seat belt to eliminate deterioration and chafing.

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

Compliance Time

by April 1, 1960

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

Affected Aircraft

Piper Models PA-22-150 and PA-22-160 Aircraft with serial numbers 22-3218, 22-3387, 22-3388 to 22-7049 inclusive, and 22-7054.

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

Federal Register Abstract

Safety Belt

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
60-05-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-22 "150" and PA-22 "160" Aircraft
Subject:
Safety Belt
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
11/02/1960
Effective Date:
Make:
Piper Aircraft Inc.
Model:
PA-22-150 | PA-22-160
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Superseded AD: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Superseded By: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: 60-05-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   60-05-03

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-22 "150" and PA-22 "160" Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
60-05-03 PIPER: Amdt. 108 Part 507 Federal Register March 2, 1960. Applies to PA-22 "150" and PA-22 "160" Aircraft Serial Numbers 22-3218, 22-3387, 22-3388 to 22-7049 Inclusive, and 22-7054.

Compliance required by April 1, 1960.

Install safety belt extension, P/N 14920-02 or equivalent, on the front seat belt in order to eliminate deterioration due to heat from the rear seat heater outlet and chafing where the web attaches to the attaching lug. P/N 14920-02 has the same geometric design as P/N 14920-0 being replaced, except that P/N 14920-02 is one inch longer measuring 3.5 inches between bolt centerlines.

(Piper Service Bulletin No. 184 covers this same subject.)

This supersedes AD 57-17-02.

Revised November 2, 1960.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_60-05-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
60-05-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-22 "150" and PA-22 "160" Aircraft
Subject:
Safety Belt
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
11/02/1960
Effective Date:
Make:
Piper Aircraft Inc.
Model:
PA-22-150 | PA-22-160
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: 60-05-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   60-05-03

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-22 "150" and PA-22 "160" Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
60-05-03 PIPER: Amdt. 108 Part 507 Federal Register March 2, 1960. Applies to PA-22 "150" and PA-22 "160" Aircraft Serial Numbers 22-3218, 22-3387, 22-3388 to 22-7049 Inclusive, and 22-7054.

Compliance required by April 1, 1960.

Install safety belt extension, P/N 14920-02 or equivalent, on the front seat belt in order to eliminate deterioration due to heat from the rear seat heater outlet and chafing where the web attaches to the attaching lug. P/N 14920-02 has the same geometric design as P/N 14920-0 being replaced, except that P/N 14920-02 is one inch longer measuring 3.5 inches between bolt centerlines.

(Piper Service Bulletin No. 184 covers this same subject.)

This supersedes AD 57-17-02.

Revised November 2, 1960.

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.