Document ID: chunk:federal_register_of_legislation:F2006B08796:body:0
Version: federal_register_of_legislation:F2006B08796
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Douglas DC3 Series Aeroplanes

AD/DC3/19 Aileron Trim Tab Control Rod - Inspection NK

 Applicability: All models.

             Requirement: 1. Inspect the aileron trim tab control rod for signs of chafing due to insufficient clearance at the point where the rod passes through the diagonal stiffening plate between the aileron main spar and the aileron rib.

             2. If chafing of the rod has taken place, increase the radius of the hole by the minimum amount necessary to ensure clearance throughout the full movement of the control.

            OR ANOs Part 100 Appendix "A" Notice No. 7/22; OR ANO 105.1.16.1.6.4.