Document ID: chunk:federal_register_of_legislation:F2006B06269:body:0
Version: federal_register_of_legislation:F2006B06269
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Transavia PL 12 Series Aeroplanes

AD/PL 12/4 Stub Wing Structure - Inspection 12/68

 Applicability: All models.

            Requirement: Inspect the stub wing leading edge tube for cracking in the vicinity of landing gear attachment.

            Compliance: Within 100 hours time in service after 14 February 1969 and thereafter at intervals not exceeding 100 hours time in service.