AD 75-09-10

AD Final Rules - DRS_75-09-10.html
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AD Number:
75-09-10
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-31P, PA-31, PA-31-300, and PA-31- 350 Airplanes
Subject:
Push-Pull Tube End Fittings
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
04/23/1975
Effective Date:
04/28/1975
Make:
Piper Aircraft Inc.
Model:
PA-31 | PA-31-300 | PA-31-350 | PA-31P
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Superseded AD: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Superseded By: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: 75-09-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2183

AD NUMBER:   75-09-10

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-31P, PA-31, PA-31-300, and PA-31- 350 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 28, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-09-10 PIPER: Amendment 39-2183. Applies to Models PA-31P, Serial Nos. 31P-1 through 31P-7400213, PA-31 and PA-31-300, Serial Nos. 31-1 through 31-7401248, and PA-31- 350, Serial Nos. 31-5001 through 31-7405242 and 31-7405400 through 31-7405462 aircraft certificated in all categories.

To prevent possible hazards in flight associated with loose elevator push-pull tube end fittings, accomplish the following:

1. Within the next 100 hours in service from the effective date of this AD unless already accomplished, inspect the elevator push-pull tube P/N 40847-04 for looseness in its attachment to the end fittings in accordance with the instructions contained in Piper Service Bulletin No. 409 dated June 7, 1974, for Model PA-31P or Piper Service Bulletin No. 433 dated December 17, 1974, for Models PA-31, PA-31-300, and PA-31-350 or an equivalent inspection.

2. If looseness is detected, replace with an acceptable elevator torque tube assembly P/N 40847-04 on Model PA-31P or P/N 40847-00 on Models PA-31, PA-31-300 and PA31-350.

3. Equivalent inspections must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

This amendment is effective April 28, 1975.

FOOTER: