Document ID: chunk:federal_register_of_legislation:F2006B09038:body:0
Version: federal_register_of_legislation:F2006B09038
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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-2/20 Control Column Torque Tubes - Inspection 9/80

 Applicability: All models DHC-2 and DHC-2 Mk. III. Document:  De Havilland Aircraft of Canada SB No. 2/28.
            Compliance: Initially inspect within 25 hours time in service after 18 September 1980 and thereafter as noted in De Havilland Aircraft of Canada SB No. 2/28.

            Background:  Three overseas operators have reported cracks in the horizontal torque tube at the base of the control column.