Document ID: chunk:federal_register_of_legislation:F2006B06359:body:0
Version: federal_register_of_legislation:F2006B06359
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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 - PT6A Series

AD/PT6A/19 Fuel Control Bypass Valve Diaphragm 10/85

            Applicability: PT6A-38, -41 and 45A engines fitted with Aviation Electric Fuel Control Units P/No 3244723-3 thru -10, 3244738-5, 3244738-6, 3244752-6 thru -10, and 3244755-7 thru-
            11.

            Document: 1. Pratt & Whitney Aircraft of Canada SB No. 3103; 2. FAA AD 78-17-07, Amendment 39-3287; or
            3. AD/UAC-T/31.

 Compliance: Within the next 100 hours time in service after 30 November 1978.