Document ID: chunk:federal_register_of_legislation:F2006B06026:body:0
Version: federal_register_of_legislation:F2006B06026
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Piper PA-46 (Malibu) Series Aeroplanes

AD/PA-46/20 Exhaust Transition Bolts 8/91 TX

            Applicability: All model PA-46-350P fitted with Textron Lycoming TI0-540-AE2A engine with engine S/No up to but not including L9161-61A and excluding S/No L9157-61A.

            Requirement: Action in accordance with the Technical Requirements of FAA AD 91-10-04 Amdt 39-6981.

            Note: Textron Lycoming SB No 491A refers.

 Compliance: Within 10 hours time in service from 31 May 1991.

            Background: An aircraft accident has occurred caused by engine power loss, which resulted from exhaust transition flange bolt loss and flange separation.