Document ID: chunk:federal_register_of_legislation:F2006B06382:body:0
Version: federal_register_of_legislation:F2006B06382
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Pratt and Whitney Canada Turbine Engines - PW100 Series

 AD/PW100/3 Fuel Pump Outlet Filter Cover 5/91

DM

 Applicability: All PW100 series engines.

            Requirement: Action in accordance with the technical requirements of Transport Canada Airworthiness Directive CF-90-21.

            Note: Netherlands Airworthiness Directive 90-130 refers.

 Compliance: Prior to 30 April 1991.

            Background:  This Directive requires modification of the engine driven fuel pump outlet filter cover assembly. This requirement reflects the requirements of Transport Canada AD CF- 90-21, and advice of a recent in-flight fuel leak event involving an Australian registered DHC-8. Investigation of this event indicated the leak source to be a cut fuel pump outlet filter cover O-ring.