Document ID: chunk:federal_register_of_legislation:F2006B09188:body:0
Version: federal_register_of_legislation:F2006B09188
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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-8/32 Landing Gear Hydraulic Selector Valve 7/94

            Applicability: All DHC-8-100 series aircraft S/N 003 through 038 not incorporating modification 8/0530.

            Requirement: Unless previously carried out action in accordance with de HAVILLAND Dash 8 Alert Service Bulletin A8-32-117.

            Note: Transport Canada AD CF-94-05 refers.

            Compliance: Within 300 hours time in service from 30 June 1994 or by 30 October 1994, whichever occurs first.

            Background: The manufacturer has advised that pilot valve leakage which has not been corrected may, when combined with a low voltage condition, lead to an inadvertent landing gear retraction.