Document ID: chunk:federal_register_of_legislation:F2006B06618:body:0
Version: federal_register_of_legislation:F2006B06618
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Robin Aviation Series Aeroplanes

AD/ROBIN/20 Main Gear Torque Link Attachment 13/94

 Applicability: Model HR100/250TR and HR100/285TR.

 Requirement: Action in accordance with Avions Pierre Robin Service Bulletin 134.

            Note: DGAC AD 94-129(A) refers.

            Compliance: Unless already accomplished, within 25 hours time in service after 8 December 1994, and thereafter at intervals as specified in the Requirement Document.

            Background: The DGAC requires an inspection in response to field reports of cracks on the strut torque link welded attachment points.