AD/ROBIN/12 Amdt 1 - Safety Harness Link
1AD/ROBIN/12 Amdt 1 - Safety Harness Link
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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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.