Document ID: chunk:federal_register_of_legislation:F2006B05237:body:0
Version: federal_register_of_legislation:F2006B05237
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Cessna 206 Series Aeroplanes

AD/CESSNA 206/32 Turbocharger 6/80

 Applicability: Model U206 S/Nos. U2060487 thru U20605619;

            Model P206 S/Nos. P2060001, P2060191 thru P20600647.

 Requirement: Action in accordance with Cessna SIL No. SE 80-24.

            Note: FAA AD 80-07-01 Amdt. 39-3719 refers.

 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 both the pressure and scavenge pumps.