Document ID: chunk:federal_register_of_legislation:F2006B09047:body:0
Version: federal_register_of_legislation:F2006B09047
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 DHC-2 (Beaver) Series Aeroplanes

AD/DHC-2/29 Elevator Mass Balance Weight 9/97

            Applicability: All de Havilland DHC-2 MK I and MK II Beaver aircraft, and all DHC-2 MK III Turbo Beaver aircraft.

 Requirement: a. For all MK I and MK II Beaver aircraft:

             Inspect the elevator tip rib for corrosion and install Modification 2/1540 in accordance with instructions contained in de Havilland Service Bulletin 2/50 (Installation of Access Cover and Special Inspection of the Elevator Mass Balance Weight for Separation).

            b. For all MK III Turbo Beaver aircraft:

             Inspect the elevator tip rib for corrosion and install Modification T2/2079 in accordance with instructions contained in de Havilland Service Bulletin TB/58 (Installation of Access Cover and Special Inspection of the Elevator Mass Balance Weight for Separation).

            Note: Transport Canada AD CF-97-06 refers.

            Compliance: Before 31 January 1998; thereafter at intervals not to exceed 5 years. This airworthiness directive becomes effective on 14 August 1997.
            Background: Field reports were received of the elevator tip rib corroding underneath the mass balance weights. This corrosion could lead to a loss of the balance weight in flight, and possible flight control difficulties.