Document ID: chunk:federal_register_of_legislation:F2006B09209:body:0
Version: federal_register_of_legislation:F2006B09209
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Bombardier (Boeing Canada/De Havilland) DHC-8 Series Aeroplanes

AD/DHC-8/53 Roll Disconnect System 6/98

 Applicability: DHC-8 aircraft, Models 102, 103, 106, 201, 202, 301, 311, 314, and 315, with serial
            numbers 3 through 433.

            Requirement: Install Modification 8/2376 in accordance with de Havilland Service Bulletin 8-27- 79, Revision A.

            Note: Transport Canada AD CF-98-04 refers.

 Compliance: Before 21 November 1998.

            This airworthiness directive becomes effective on 21 May 1998.

            Background: Several incidents have been reported of uncommanded roll system disconnects during landing.