AD/PA-32/75 - Stabilator Attach Fitting Corrosion

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

Legislation au F2006B05871 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-32/75 Stabilator Attach Fitting Corrosion 5/87

Applicability: All models listed in Piper SB No 856. Requirement: Action in accordance with Piper SB No 856.

Compliance: At the next scheduled inspection for Maintenance Release issue after 7 May 1987 and thereafter at intervals not exceeding one year.

 

Background:  The manufacturer reports instances of severe corrosion between the steel attach fittings and fuselage structure.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.