Document ID: chunk:federal_register_of_legislation:F2006B08470:body:0
Version: federal_register_of_legislation:F2006B08470
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 General Electric Turbine Engines - CF6 Series

AD/CF6/27 High Pressure Turbine Thermal Shield Inspection 12/93

 Applicability: CF6-45, -50, -80A and -80C2 series.

 Requirement: Action in accordance with the technical requirements of FAA AD 93-14-18.

            Note: General Electric Service Bulletins 72-1021,-596, and -565 refer.

 Compliance: As specified in the FAA AD with effectivity commencing 11 Nov 1993.

            Background:  This directive is raised because of a HPT thermal shield separation. Such separations could result in uncontained failure.