Document ID: chunk:federal_register_of_legislation:F2006B08091:body:0
Version: federal_register_of_legislation:F2006B08091
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Cessna 210 Series Aeroplanes

 AD/CESSNA 210/42 Fuel Flow Indication System - Hose
                          Inspection and Replacement

 11/79

            Applicability: Models 210L and T210L with S/Nos. 21061040 and subsequent Models 210M, T210M and P210N modified to incorporate Symbolic Displays Inc. fuel flow indicating system per STC.SA3835WE.

             Requirement: 1. Inspect the fuel flow transducer installation on the upper left side of the engine adjacent to the fuel distributor manifold.

             2. If an NAS 424-4 coupling is installed between transducer and distributor manifold, remove coupling and replace with either hose assembly Aeroquip P/No. AE7010001E0040 or Stratoflex P/No. 111D417-45-0040.

            Note: FAA AD 79-19-06 Amendment 39-3558 also refers to this subject.

 Compliance: Within 25 hours time in service after 3 October 1979.

            Background: The hose assembly connecting the fuel flow transducer with the fuel distributor manifold has proved unsuitable in service and may leak fuel over the engine.