AD 79-12-02

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AD Number:
79-12-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-31 Series
Subject:
Elevator Surface Travel
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
06/25/1979
Effective Date:
07/02/1979
Make:
Piper Aircraft Inc.
Model:
PA-31 | PA-31-300 | PA-31-325 | PA-31-350 | PA-31P | PA-31T | PA-31T1
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Superseded AD: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Superseded By: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: 79-12-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3501

AD NUMBER:   79-12-02

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-31 Series

ACTION:  

SUMMARY:  

DATES:   Effective July 2, 1979.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
79-12-02 PIPER AIRCRAFT CORPORATION: Amendment 39-3484 as amended by Amendment 39-3501. Applies to the following Model PA-31 series airplanes, certificated in all categories: PA-31; PA-31-300; PA-31-325, S/N 31-5 through 31-7912049 inclusive; PA-31-350, S/N 31-5001 through 31-7952091 inclusive; PA-31P, S/N 31P-1 and up; PA-31T, S/N 31T-7400002 through 31T-7920060 inclusive; and PA-31T1, S/N 31T-7804001 through 31T-7904031 inclusive.

Compliance required within the next 25 hours' time in service after the effective date of this AD,unless already accomplished.

To prevent the possible restriction of elevator surface travel, accomplish the following:

a. Remove the upper and lower tail cone halves and gain access to the elevator hinge assembly (Piper P/N 40249-00, 45253-00, or 45253-03 as applicable).

b. Inspect the elevator stop bolts (Piper P/N 419 991) and lock nuts (Piper P/N 404 224) for signs of looseness or damage, or evidence of movement. Repair or replace, as necessary, in accordance with the airplane service manual.

c. Verify proper elevator travel in accordance with Section 5 of the airplane service manual. Elevator surface travel limits are also given in the airplane Type Certificate Data Sheet.

d. Torque elevator stop bolt lock nuts to 20-25 inch/pounds, and recheck elevator surface travel.

e. Paint or install a slip stripe or torque seal on lock nuts and stop bolts.

f. Reinstall tail cone.

g. If above inspections find any indications of loose or damaged stop bolts and/or lock nuts, or if elevator surface travel does not meet specification surface travel limits, report findings within 10 days to Chief, Engineering and Manufacturing Branch, FAA, Southern Region, P.O. Box 20636, Atlanta, Georgia 30320, also giving the airplane serial number, the owner/operator of the airplane, and the person and/or facility conducting the inspection. (Reporting approved by the Office of Management and Budget under OMB No. 04-R0174.)

Piper Service Bulletin No. 649 also pertains to this subject.

Compliance with the provisions of this AD may be accomplished in an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, FAA, Southern Region.

Amendment 39-3484 was effective June 14, 1979.

This amendment 39-3501 is effective July 2, 1979.

FOOTER: