Document ID: chunk:federal_register_of_legislation:F2006B05675:body:0
Version: federal_register_of_legislation:F2006B05675
Segment Type: other
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Character Range: 0–626

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-30/33 Wing Main Spar Lower Cap - Inspection 9/83

            Applicability: All model PA-30 with S/Nos. 30-2 to 30-2000. All model PA-39 with S/No. 39-1 to 39-155.

 Document: Piper Service Bulletin No. 751.

 Compliance: Within 100 hours time in service after 30th September 1983.

            Background: The Manufacturer reports cases of chafing of the wing main spar lower cap where the spar enters the fuselage.