Document ID: chunk:federal_register_of_legislation:F2006B09477:body:0
Version: federal_register_of_legislation:F2006B09477
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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-110/36
 Amdt 1

     Elevator Trim Tab Actuation - Dual Control Rod Installation

 11/85

 Applicability: All model EMB-110 with S/Nos referenced in the Requirement Document. Requirement:               Action in accordance with Embraer SB 110-27-068 Rev 1.
            Note: Brazilian AD 82-06-01 R5.

 Compliance: Within 250 hours time in service after 30 November 1985.

            Note: Aircraft which have complied with previous issues of this Directive require further rework in accordance with SB 110-27-068 R1.

            Background: To preclude the effect of rod failure the installation of dual rods with bearings and increased weight to the elevator mass balance is now a mandatory requirement. This amendment references Rev 1 to the Requirement Document.