Document ID: chunk:federal_register_of_legislation:F2006B08488:body:0
Version: federal_register_of_legislation:F2006B08488
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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/CF6/5 Fuel Supply Manifold 9/85

 Applicability:  General Electric CF6-80A, -80A2 engines. Requirement: FAA TAD No. T85-15-51.
 Compliance: As per Requirement Document.

            Background: General Electric has advised of 3 fuel supply manifolds failing due to cracking at the "Y" section. The manifolds' Part No 9327M46G01, 02, are the subject of FAA Emergency Telegraphic Airworthiness Directive T85-15-51 which requires a cycle life limit of 2500 cycles. Any manifold in service with a cycle life in excess of 2500 cycles must be replaced within 100 cycles following receipt of FAA TAD No T85- 15-51.