Document ID: chunk:federal_register_of_legislation:F2006B08635:body:0
Version: federal_register_of_legislation:F2006B08635
Segment Type: other
Provision Reference: 
Character Range: 0–1178

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

 Teledyne Continental Motors Piston Engines

 AD/CON/53
 Amdt 1

 Starter Adaptor Shafts 12/88

 Applicability: IO-520BA, IO-520BB, IO-550B, TSIO-520BE, TSIO-520LB, TSIO-520UB, TSIO-
            520WB engines fitted with a starter adaptor shaft driving a freon compressor.

 Requirement: Part 1 Action in accordance with TCM SB M87-24.

            Note: FAA AD 88-17-03 Amdt 39-5943 Para (a) refers.

                Part 2 Replace starter drive assy in accordance with (IAW) TCM SB M88-5 and drive belt IAW TCM SB M88-6.

            Note: FAA AD 88-17-03 Amdt 39-5943 Para (b) refers.

 Compliance: For Part 1 Before further flight after 1 February 1988.

            For Part 2 Prior to refitment of compressor drive belt and reactivation of airconditioning system.

            Note: Compliance with CAO 106 AD/CON/50 does not constitute compliance with this Directive.

            Background: This Directive is amended to reflect and reference FAA AD 88-17-03 Amdt 39-5943 which supersedes FAA AD 87-26-01 Amdt 39-5882.