AD/ROBIN/12 Amdt 1 - Safety Harness Link

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B06609 In force Legislative Instrument

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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/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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.