Document ID: chunk:federal_register_of_legislation:F2006B11354:body:0
Version: federal_register_of_legislation:F2006B11354
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Mitsubishi MU-2 Series Aeroplanes

 AD/MU-2/25
 Amdt 2

 Flap Control System Torque Tube Assembly Joint 10/90

 Applicability: All models.

            Requirement: Action in accordance with Mitsubishi SB No 189A or SB No 067/27-008 as applicable by serial number.

            Note: Japan Civil Aviation Bureau AD No TCD-2252-1-87 refers.

            Compliance: Initially inspect prior to exceeding 4000 hours component time in service or within 100 hours component time in service after 1 November 1990, whichever occurs later. Repeat the inspections at intervals not exceeding 100 hours component time in service.

            Note: Modification in accordance with the applicable Requirement document constitutes terminating action for this Directive.

            Background: Amendment 1 extended the repeat inspection requirements, and introduced a new terminating action for the inspections.

            Amendment 2 introduces SB 067/27-008 which extends the inspection requirements to include all remaining serial numbers, and includes terminating action acceptable for those serial numbers.