AD/S-76/24 - Rotor Brake Installation - Modification

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

Legislation au F2006B06706 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

 


Sikorsky S-76 Series Helicopters

 

AD/S-76/24 Rotor Brake Installation - Modification 10/82

Applicability: All models S-76A.

 

Requirement: Modify the rotor brake system by incorporation of the following Sikorsky documents: 1. CSB 76-66-7.

2. CSB 76-66-8A.

 

3. CSB 76-66-10B.

 

4. CSN 76-51B.

 

Note: FAA AD 82-17-03 refers.

 

Compliance: Within 100 hours time in service after 31 October, 1982.

 

Background: The manufacturer has introduced a number of modifications to the rotor brake system to reduce the possibility of brake drag and overheating.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.