Document ID: chunk:federal_register_of_legislation:F2006B09948:body:0
Version: federal_register_of_legislation:F2006B09948
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Franklin Piston Engines

AD/FK-P/3 Engine Drive Fuel Pump - Inspection NK

            Applicability: Model 6A-350-C1 with S/Nos 52501 and subsequent and Model 6A-335-B1A with S/Nos 56001-3 and subsequent fitted with fuel pumps Part No 20574.

 Requirement: Franklin SB No 114.

            Compliance: Part 1. Inspection of Pump Diaphragm. Within 5 hours time in service after 6 March 1972 and thereafter at intervals not exceeding 100 hours time in service.

            Part 2. Inspection for Fuel Leaks. At intervals not exceeding 50 hours time in service after 6 March 1972.

            Note: Inspection for fuel leaks as per Part 2 may be carried out and certified by the pilot.