AD/PA-32/15 Amdt 2 - Rudder Trim Arm Assembly Cracking

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B05808 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Piper PA-32 (Cherokee Six) Series Aeroplanes

 

AD/PA-32/15

Amdt 2

Applicability: All models.


Rudder Trim Arm Assembly Cracking 12/85

 

Requirement: Inspect the rudder trim arm assembly for cracking at or near the rudder pedal bar attachment bolt.

 

Compliance: Within 100 hours time in service after 29 September 1969 and thereafter at each issue of a new Maintenance Release.

 

Background:  This amendment revises the compliance requirements to coincide with varying periodic inspection intervals.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.