Document ID: chunk:federal_register_of_legislation:F2006B09463:body:0
Version: federal_register_of_legislation:F2006B09463
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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-110/22 Rudder Pedal Assembly, Main Bearing
                   Attachment - Inspection and Modification

 Applicability: All model EMB-110 with S/Nos. 110001 to 110385. Document:  Embraer SB No. 110-27-058.
            Note: Brazilian AD 82-11-02 refers.

3/83

            Compliance: Within 25 hours time in service after 21 January, 1983 and thereafter at intervals not exceeding 100 hours time in service until modified in accordance with Section II of the requirement document.

            Background: Manufacturer reports that a bearing was displaced from its housing flange rendering the rudder control inoperative.