Document ID: chunk:federal_register_of_legislation:F2006B08114:body:0
Version: federal_register_of_legislation:F2006B08114
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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 210/65 Fuel Line Chafing 1/92 DM

            Applicability: All Cessna 210 series with S/N 21059062 through 21064535, T210-0393 through T210-0454 and P21000001 through P21000760.

            Requirement: Unless previously carried out action in accordance with Cessna Service Information Letter SE82-32. A minimum clearance of 6.5mm (0.25 inches) must be obtained between the fuel line/electrical wiring loom.

            Note: FAA AD 91-22-01 Amdt 39-8061 refers.

            Compliance: Within 50 hours time in service from 22 November 1991 or by 30 April 1992, whichever occurs first.

            Background: Chafing of the fuel line by the wiring loom in the nose gear tunnel area could result in an inflight fire.