AD/CESSNA 210/47 - Fuel Vapour Return Line - Repositioning

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

Legislation au F2006B08095 Not 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 210/47 Fuel Vapour Return Line - Repositioning 7/80

Applicability: Models T210 and P210 with S/Nos. 21063661 to 21063886, 21063888 to 21063914, P21000390 to P21000473, P21000475 to P21000481; AND Those aircraft which have had the fuel system modified using Service Kit SK210-93A or SK210-93B as per AD/CESSNA 210/45 (Cessna SIL No. 79-60 Supplement No. 1).

 

Document: Cessna SIL No. SE 80-50.

 

Compliance: Within 100 hours time in service after 31 July 1980.

 

Background:  The manufacturer has found it necessary to provide a more positive separation between the alternator leads and the fuel vapour return line.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.