Commonwealth legislation

AD/PA-38/14 - Control Column Installation - Modification

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD mandates a Piper Service Bulletin No. 661 modification to the control column installation on PA-38-112 aeroplanes serials 38-78A0001 through 38-79A1160 to cure reported control-shaft roughness/binding. Owners/operators of those aircraft must arrange and fund the work.

If not already done, the modification must be completed within 100 hours TIS after 30 November 1979; the AD directs compliance to the manufacturer’s SB and contains no alternative method.

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AD/PA-38/14 - Control Column Installation - Modification

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Piper PA-38 (Tomahawk) Series Aeroplanes

AD/PA-38/14 Control Column Installation - Modification 11/79

Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-79A1160. Document: Piper SB No. 661.

Compliance: Unless already accomplished, within 100 hours time in service after 30 November 1979.

Background: It has been reported to the manufacturer that roughness or binding of the control shaft in the instrument panel can occur at the extremes of control movement.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.