Document ID: chunk:federal_register_of_legislation:F2006B06699:body:0
Version: federal_register_of_legislation:F2006B06699
Segment Type: other
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Character Range: 0–848

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-76/16
 Amdt 2

         Main Rotor Blade Root End - Inspection for Fatigue Cracking

 4/85

 Applicability: All models fitted with main rotor blades P/N 76150-09000 or 76150-09100. Requirement:               Sikorsky S76 Alert Customer Service Bulletin no. 76-65-18C.
            Compliance: As detailed in requirement document. Inspections carried out in accordance with the previous issue of this directive, meet the requirements of this issue.

            Background: The directive has been amended to nominate ACSB 76-65-18C as a more appropriate requirement document than the Composite Materials Manual. FAA AD 84-10-02 also refers to this subject.