AD/S-76/39 Amdt 1 - Main Rotor Blade Tip Block and Tip End Assemblies - Inspection and Rectification

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

Legislation au F2006B06720 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-76/39

Amdt 1


Main Rotor Blade Tip Block and Tip End Assemblies - Inspection and Rectification


7/85

DM

 

Applicability: All model S-76A Helicopters fitted with main rotor blades prior to S/N A086-01461. Requirement:              Sikorsky Alert S.B. 76-65-36. Amdt 1.

Compliance: Unless already accomplished, as detailed in the requirement document.

 

Background: 1. The manufacturer has advised that an operator has experienced the loss of a main rotor blade tip block.

 

2. This Directive is amended to include an amendment to the Requirement Document, the intent of which results in changes to certain inspection criteria and the addition of a calendar compliance time.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.