AD/CESSNA 210/65 - Fuel Line Chafing

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B08114 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.