Document ID: chunk:federal_register_of_legislation:F2006B05655:body:0
Version: federal_register_of_legislation:F2006B05655
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Piper PA-30 & 39 (Twin Comanche) Series Aeroplanes

 AD/PA-30/13
 Amdt 1

 Pitch Trim Switch - Replacement 2/77

            Applicability: Model PA-30 with S/Nos. 30-1717 and 30-1745 to 30-2000 and all model PA-39 with S/Nos. 39-1 to 39-155 fitted with rocker type switch on pilot's control wheel.

 Document: 1. Piper SB No. 527; or FAA AD 77-09-10. Compliance:  Within 100 hours time in service after 28 February 1977.
            Note: Aircraft complying with previous issues of this Directive, satisfy this issue of the Directive.