Document ID: chunk:federal_register_of_legislation:F2006B08468:body:0
Version: federal_register_of_legislation:F2006B08468
Segment Type: other
Provision Reference: 
Character Range: 0–707

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/CF6/25 Fan Disks - Removal From Service 10/92

 Applicability: CF6-50 and 80A series.
 Requirement: Action in accordance with the technical requirements of FAA AD 91-23-13. Compliance:              As specified in the Requirement Document with an effective date of 17 September
            1992.

            Background:  This AD requires removal of certain Stage 1 Fan Disks from service. It results from the possibility of a metallurgical defect which could adversely affect the service life of the disc.