AD 57-10-02

final rule

Airworthiness Directives; Piper Model PA-23 Aircraft

AD Number
57-10-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-23 Airworthiness Directives; Piper Model PA-23 Aircraft

Unsafe Condition

The flare on the oil pressure gage line has cracked or broken where it attaches to the connector fitting on the aft side of the firewall, resulting in loss of oil pressure.

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

Required Actions

Inspect both right and left oil pressure line flares to ensure they are intact and that the lines near the flares are not cracked or broken. Replace cracked or broken lines or those with defective flares by cutting off and reflaring, ensuring no line strain against fittings or retainer blocks. If the line is too short, cut off and splice using Piper P/N 17766-07 or equivalent connector and flexible hose.

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

Compliance Time

not later than June 15, 1957

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

Affected Aircraft

Piper Aircraft Inc. Model PA-23 Aircraft, serial numbers 23-1 to 23-1391 inclusive.

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

Federal Register Abstract

Oil Pressure Gage Line

Applicability Source Text

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Details
AD Number:
57-10-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA-23 Aircraft
Subject:
Oil Pressure Gage Line
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
08/01/1957
Effective Date:
Make:
Piper Aircraft Inc.
Model:
PA-23
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Superseded AD: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Superseded By: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:
unable to find issue date
AIRWORTHINESS DIRECTIVES FINAL RULES: 57-10-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   57-10-02

SUBJECT HEADING:   Airworthiness Directives; Piper Model PA-23 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
57-10-02 PIPER: Applies to Model PA-23 Aircraft Serial Numbers 23-1 to 23-1391 Inclusive.

Compliance required as soon as possible but not later than June 15, 1957.

It has been reported that the flare on the oil pressure gage line has cracked or broken where it attaches to the connector fitting on the aft side of the firewall resulting in loss of oil pressure.

Inspect both right and left oil pressure line flares to determine whether or not they are normal and also to determine that the lines in the area of the flares are not cracked or broken.

Lines that are cracked or broken or have defective flares should be cut off and reflared. Care should be taken that there is no line strain against the fitting or the retainer block and that the line into the fitting is straight. If the line is too short for this repair, it should be cut off and spliced using a connector and flexible hose, Piper P/N 17766-07 or equivalent.

(Piper Service Bulletin No. 152A covers this subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_57-10-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
57-10-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA-23 Aircraft
Subject:
Oil Pressure Gage Line
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
08/01/1957
Effective Date:
Make:
Piper Aircraft Inc.
Model:
PA-23
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:
unable to find issue date
AIRWORTHINESS DIRECTIVES FINAL RULES: 57-10-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   57-10-02

SUBJECT HEADING:   Airworthiness Directives; Piper Model PA-23 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
57-10-02 PIPER: Applies to Model PA-23 Aircraft Serial Numbers 23-1 to 23-1391 Inclusive.

Compliance required as soon as possible but not later than June 15, 1957.

It has been reported that the flare on the oil pressure gage line has cracked or broken where it attaches to the connector fitting on the aft side of the firewall resulting in loss of oil pressure.

Inspect both right and left oil pressure line flares to determine whether or not they are normal and also to determine that the lines in the area of the flares are not cracked or broken.

Lines that are cracked or broken or have defective flares should be cut off and reflared. Care should be taken that there is no line strain against the fitting or the retainer block and that the line into the fitting is straight. If the line is too short for this repair, it should be cut off and spliced using a connector and flexible hose, Piper P/N 17766-07 or equivalent.

(Piper Service Bulletin No. 152A covers this subject.)

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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