Commonwealth legislation

AD/ROBIN/17 - Safety Harness Link

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive requires owners/operators of Robin Aviation "ATL, all types" aeroplanes to carry out the modification described in ROBIN SA Service Bulletin No.6 Rev 1 to prevent the quick‑disconnect link nut from unscrewing. The work must be completed within 50 hours time in service after 25 June 1992 (unless already done); technical details and costs are contained in the referenced service bulletin and DGAC AD.

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Current sections

Direct links to the current provisions in AD/ROBIN/17 - Safety Harness Link.

AD/ROBIN/17 - 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

View image in the official source Robin Aviation Series Aeroplanes

AD/ROBIN/17 Safety Harness Link 7/92

Applicability: ATL, all types.

Requirement: Action in accordance with ROBIN SA SB No.6 Rev 1.

Note: DGAC AD 89-075(A) R1 refers.

Compliance: Unless already accomplished; Within 50 hours time in service after 25 June 1992. Background: The DGAC requires modification action in order to prevent the nut of the quick-

disconnect link to unscrew.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.