Document ID: chunk:federal_register_of_legislation:F2006B09479:body:0
Version: federal_register_of_legislation:F2006B09479
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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-110/39
 Amdt 2

 Applicability: All models.

 Trim Tab Actuator Attachments 12/87

 Requirement: Action in accordance with Embraer SB110-027-0083. Compliance:  Within 500 hours time in service after 3 December 1987.
            Background: The Department has received reports of fractured spring pins on Australian aircraft. Pin failure could result in control surface flutter. Amdt 1 of this Directive extended compliance to all trim tab actuators. Amdt 2 of this Directive references SB110-027- 0083 which replaces existing spring pins with solid pins.