Document ID: chunk:federal_register_of_legislation:F2006B06082:body:0
Version: federal_register_of_legislation:F2006B06082
Segment Type: other
Provision Reference: 
Character Range: 0–864

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.