Document ID: chunk:federal_register_of_legislation:F2006B08451:body:0
Version: federal_register_of_legislation:F2006B08451
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 General Electric Turbine Engines - CF34 Series

AD/CF34/2 Fuel Control Bypass Valve 7/88

            Applicability:  CF34-1A and -3A engines installed in Canadair CL-600-2A12 and CL-600-2B16 aircraft.

            Requirement:  Action in accordance with FAA AD 88-06-07 amendment 39-5866, paragraph (A) items (1) and (2).

 Compliance: Before 30 September 1988.

            Background:  This Directive has been issued to require compliance with FAA AD 88-06-07. The FAA Directive requires replacement of the fuel control by-pass piston to prevent an engine flameout or uncommanded power roll back due to contamination of the fuel control.