AD/PC-12/7 - Aileron Tie Rod Assembly

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

Legislation au F2006B06109 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Pilatus PC-12 Series Aeroplanes

 

AD/PC-12/7 Aileron Tie Rod Assembly 8/97

Applicability: Model PC-12 and PC-12/45 aircraft, with serial numbers MSN 101 through to and including MSN 169.

 

Requirement: Inspect and modify in accordance with Pilatus Mandatory Service Bulletin 27-001.

 

Note: FOCA Switzerland AD HB 97-174 refers.

 

Compliance: Unless already accomplished, before 17 October 1997.

 

This airworthiness directive becomes effective on 17 July 1997.

 

Background: A report was received where the aileron tie-rod jam-nuts, on the aileron movement chain of the control wheels, became loose.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.