Document ID: chunk:federal_register_of_legislation:F2006B06109:body:0
Version: federal_register_of_legislation:F2006B06109
Segment Type: other
Provision Reference: 
Character Range: 0–796

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.