Document ID: chunk:federal_register_of_legislation:F2006B05968:body:0
Version: federal_register_of_legislation:F2006B05968
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Piper PA-38 (Tomahawk) Series Aeroplanes

 AD/PA-38/3
 Amdt 1

             Vertical Fin/Rudder Leading Edge - Inspection and Modification

 1/79

            Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-78A0215 and 38-78A0217 to 38-78A0226.

Document: 1. Piper SB No. 607A, Parts I and II; or

2. FAA AD 78-22-01, Amdt. 39-3323.

 Compliance: 1. Inspect at intervals not exceeding 25 hours time in service; and

            2. Modify within 50 hours time in service after 20 November 1978.