Document ID: chunk:federal_register_of_legislation:F2006B03742:body:0
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Beechcraft 19, 23 and 24 Series Aeroplanes

 AD/BEECH 23/29
 Amdt 2

 Wing Main Spar Corrosion 12/86

 Applicability: All 19, 23 and 24 series.

 Requirement: Action in accordance with Beechcraft SI No. 0824-035 Rev. II.

            Compliance: Prior to the issue of the next Maintenance Release after 31 December 1986 and thereafter at intervals not exceeding 12 months.

            Background: A history of Major Defect Reports has warranted an increase in the periodicity of this Directive to that originally called up by Beech.