Document ID: chunk:federal_register_of_legislation:F2006B06609:body:0
Version: federal_register_of_legislation:F2006B06609
Segment Type: other
Provision Reference: 
Character Range: 0–1042

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

 Robin Aviation Series Aeroplanes

 AD/ROBIN/12
 Amdt 1

 Safety Harness Link 6/92

 Applicability: Models as listed in the Requirement Document.

 Requirement: Action in accordance with Avions Pierre Robin SB 114 Rev.1.

            Note: DGAC AD 89-074(A)R1 Refers.

            Compliance: Within 50 hours time in service after 21 May 1992. The compliance of the previous issue of this Directive was:

            Prior to exceeding 25 hours time in service after 2 August 1989, and thereafter at intervals not exceeding 50 hours time in service.

            Background: Country of Origin AD. Manufacturer reports possibility of defective quick-disconnect link on safety belt.

            Amendment 1 is raised in response to a revision of the related DGAC AD which requires a modification to the link. This requirement constitutes terminating action in lieu of repetitive inspections.