Document ID: chunk:federal_register_of_legislation:F2006B10173:body:0
Version: federal_register_of_legislation:F2006B10173
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 GAF N22 and N24 Series Aeroplanes

                           AD/GAF-N22/26 Rudder Tab Mass Balance Hinge Pin - Inspection

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            Applicability: All models N22, N22B, N24 and N24A with Mod. N39 fitted and delivered before 1 March 1979.

 Document: GAF Alert SB No. ANMD-55-6.

            Compliance: Within 50 hours time in service after 16 March 1979 and thereafter at intervals not exceeding 100 hours time in service until modified in accordance with Alert SB No. ANMD-55-6.

            Background:  An instance has occurred where the rudder tab mass balance hinge pin seized in its bush and sheared the split pin retaining the hinge pin.