Document ID: chunk:federal_register_of_legislation:F2006B09464:body:0
Version: federal_register_of_legislation:F2006B09464
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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-110/23 Trim Tab Control Systems - Inspection
                              and Modification

 Applicability: All models EMB-110 with S/Nos. 110001 to 110364 and 110366 to 110384. Document:               Embraer SB No. 110-27-062 Parts I and II.
            Note: Brazilian AD 82-11-03 refers.

 Compliance: PART 1: Within 25 hours time in service after 25 January 1983.

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            PART II: Within 125 hours time in service or one month, whichever occurs first, after 25 January, 1983.

            Background: Investigation by the manufacturer revealed that the attaching nuts of the actuating rod ends of the trim cab systems may become loose.