AD/PC-12/19 - Flap Inboard Attachment Fittings

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

Legislation au F2006B06082 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-12/19 Flap Inboard Attachment Fittings 9/99

Applicability: PC-12 and PC-12/45 aircraft, serial numbers MSN 101 up to and including MSN 300. Requirement:               Modify the flap inboard attachment fittings in accordance with Pilatus PC-12 Service

Bulletin No. 57-004 dated Jun 11, 1999.

 

Note: FOCA Switzerland AD HB 99-353 refers.

 

Compliance: Within 5 months of the effective date of this Airworthiness Directive. This Airworthiness Directive becomes effective on 9 September 1999.

Background: During static testing, it was found that under maximum loading conditions the existing flap attachment fitting could buckle.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.