Document ID: chunk:federal_register_of_legislation:F2006B05596:body:0
Version: federal_register_of_legislation:F2006B05596
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Piper PA-28 Series Aeroplanes

AD/PA-28/38 Stabilator Hinge Attaching Bolts - Inspection 6/78

 Applicability: All models referenced in requirement documents. Document:  1. Piper SL No. 614; or
            2. FAA AD 72-14-7.

 Compliance: Within 100 hours time in service after 31 August 1972.