Document ID: chunk:federal_register_of_legislation:F2006B08094:body:0
Version: federal_register_of_legislation:F2006B08094
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Cessna 210 Series Aeroplanes

AD/CESSNA 210/46 Turbocharger - Inspection 6/80

            Applicability: Model T210 S/Nos. T210-0001 thru T210-0454. Model 210 S/Nos. 21058140, 21059200 thru 21063954.

 Document: 1. Cessna SIL No. SE 80-24; or

            2. FAA AD 80-07-01, Amdt. 39-3719.

 Compliance: Within 100 hours time in service after 30 June 1980.

            Background:  This Directive is issued to preclude a failure of the turbocharger anti-rotation pin and its ingestion into the scavenge pump. This in turn could cause a failure of the pressure and scavenge pumps.