AD/PA-30/23 Amdt 2 - Stabilator Attachment Bolts - Inspection

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

Legislation au F2006B05665 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-30 & 39 (Twin Comanche) Series Aeroplanes

 

AD/PA-30/23

Amdt 2


Stabilator Attachment Bolts - Inspection 12/74

 

Applicability: All models PA-30 and PA-39.

 

Requirement: Remove the LH and RH stabilator attachment bolts and inspect bolts for corrosion.

 

Compliance: Unless already accomplished, within 100 hours time in service after 31 January 1975 and thereafter at intervals not exceeding 3 months until replaced in accordance with Piper SL No. 667.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.