AD 75-06-04

final rule

Airworthiness Directives; Piper Model PA-31-350 Airplanes

AD Number
75-06-04
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-31-350 Airworthiness Directives; Piper Model PA-31-350 Airplanes

Unsafe Condition

Improper routing of forward rudder control cables (P/N 41947-03) and contact between cable guard pins and control cable, which could lead to cable damage or failure.

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

Required Actions

Inspect the forward rudder control cable installation by removing the left pilot's seat and floor panels, checking cable routing between pulleys and guard pins, and inspecting pins for cable contact. Replace cables with acceptable P/N 41947-03 parts if improperly routed or showing contact evidence, before further flight except under FAR 21.197.

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

Compliance Time

within the next ten hours in service from the effective date of this AD unless previously accomplished

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

Affected Aircraft

Piper Model PA-31-350, Serial Nos. 31-5001 through 31-7405495

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

Federal Register Abstract

Forward Rudder Control Cable

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-06-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-06-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA-31-350 Airplanes
Subject:
Forward Rudder Control Cable
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
03/07/1975
Effective Date:
03/13/1975
Make:
Piper Aircraft Inc.
Model:
PA-31-350
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Superseded AD: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Superseded By: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: 75-06-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2121

AD NUMBER:   75-06-04

SUBJECT HEADING:   Airworthiness Directives; Piper Model PA-31-350 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 13, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-06-04 PIPER: Amendment 39-2121. Applies to Model PA-31-350, Serial Nos. 31- 5001 through 31-7405495 certificated in all categories. Compliance required within the next ten hours in service from the effective date of this AD unless previously accomplished, as indicated.

1. Inspect the forward rudder control cable installation as follows:

a. Remove the left pilot's seat and associated floor panels.

b. Inspect the left- and right-hand forward rudder control cables P/N 41947-03 for proper routing between the pulleys and cable guard pins.

c. Remove the forward rudder cable guard pins and inspect the pins for evidence of contact with the control cable.

d. If a forward rudder control cable is not properly routed or the cable guard pins show evidence of contact with the control cable, the control cable must be replaced with an acceptable part of the same part number, before further flight, except that the airplane may be flown in accordance with FAR 21.197 to a base where repairs can be made.

(Piper Service Bulletin No. 379A refers to this subject.)

This amendment is effective March 13, 1975, and was effective for all recipients of the airmail dispatch of February 12, 1975, upon receipt.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-06-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-06-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Model PA-31-350 Airplanes
Subject:
Forward Rudder Control Cable
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
03/07/1975
Effective Date:
03/13/1975
Make:
Piper Aircraft Inc.
Model:
PA-31-350
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: 75-06-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2121

AD NUMBER:   75-06-04

SUBJECT HEADING:   Airworthiness Directives; Piper Model PA-31-350 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 13, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-06-04 PIPER: Amendment 39-2121. Applies to Model PA-31-350, Serial Nos. 31- 5001 through 31-7405495 certificated in all categories. Compliance required within the next ten hours in service from the effective date of this AD unless previously accomplished, as indicated.

1. Inspect the forward rudder control cable installation as follows:

a. Remove the left pilot's seat and associated floor panels.

b. Inspect the left- and right-hand forward rudder control cables P/N 41947-03 for proper routing between the pulleys and cable guard pins.

c. Remove the forward rudder cable guard pins and inspect the pins for evidence of contact with the control cable.

d. If a forward rudder control cable is not properly routed or the cable guard pins show evidence of contact with the control cable, the control cable must be replaced with an acceptable part of the same part number, before further flight, except that the airplane may be flown in accordance with FAR 21.197 to a base where repairs can be made.

(Piper Service Bulletin No. 379A refers to this subject.)

This amendment is effective March 13, 1975, and was effective for all recipients of the airmail dispatch of February 12, 1975, upon receipt.

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.