AD/S-76/58 - Tail Gearbox Output Shaft

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

Legislation au F2006B06733 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Sikorsky S-76 Series Helicopters

 

AD/S-76/58 Tail Gearbox Output Shaft 5/92

Applicability: All model S76A, S76B and S76C helicopters up to and including S/N 760390. Requirement:               Action in accordance with Sikorsky Alert Service Bulletin No 76-66-27.

Compliance: Within 150 hours time in service from 30 April 1992 or by 30 August 1992, whichever occurs first.

 

Background:  The manufacturer requires a one-time inspection of the tail rotor gearbox output shaft assembly internal bore for a surface irregularity/groove. Scoring in the bore area may initiate a premature fatigue failure.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.