AD/PA-32/34 Amdt 1 - Main Landing Gear Cylinder Cracking

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

Legislation au F2006B05829 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-32/34

Amdt 1


Main Landing Gear Cylinder Cracking 12/85

 

Applicability: All models with fixed landing gear.

 

Requirement: Visually inspect the landing gear cylinder for cracks at the base of each torque link attachment lug.

 

Compliance: Within 100 hours time in service after 31 December 1974 and there- after at each issue of a new Maintenance Release.

 

Background:  This amendment revises the compliance requirement 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.