Document ID: chunk:federal_register_of_legislation:F2006B09470:body:0
Version: federal_register_of_legislation:F2006B09470
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Embraer EMB-110 (Bandeirante) Series Aeroplanes

                      AD/EMB-110/29  Flight Control Trim Tab Hinge Pins - Inspection and Replacement

3/84

 Applicability: All model EMB-110 with S/Nos 110001 to 110386, 110388 to 110397, 110399 to
            110401, 110404 to 110408, 110410 to 110412, 110414, 110415 and 110421.

 Document: Embraer S.B. No 110-55-023.

            Note: Brazilian AD 83-11-01 refers.

             Compliance: 1. Inspect within 25 hours time in service after 26th January 1984 and thereafter at intervals not exceeding 25 hours time in service until modified.

            2. Modify prior to 30 April 1984.

 Background: The manufacturer reports migration of an elevator trim tab hinge pin.