Document ID: chunk:federal_register_of_legislation:F2006B08512:body:0
Version: federal_register_of_legislation:F2006B08512
Segment Type: other
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Character Range: 0–532

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 General Electric Turbine Engines - CF700 Series

AD/CF700/8 Fan Centre Vent System 9/85

 Applicability: All CF700-2C, -2D and -2D-2. Document:  General Electric SB (CF700) 79-8; or
            AD/GE-T/20.

            Compliance: Before installation in an aircraft following next hot end inspection or engine reconditioning completed after 28 January 1972, whichever occurs first.