AD/CESSNA 206/35 - Cylinder Head Temperature Probe

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

Legislation au F2006B05240 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Cessna 206 Series Aeroplanes

 

AD/CESSNA 206/35 Cylinder Head Temperature Probe 8/82

Applicability: Model U206 with S/Nos. U20604650 thru U20606365, except the following U20606164, U20606173, U20606198, U20606204, U20606271, U20606281, U20606287, U20606298, U20606305, U20606314, U20606315, U20606322, U20606326, U20606327, U20606331, U20606334, U20606337, U20606338, U20606344, U20606345, U20606348, U20606349, U20606350, U20606352, U20606353, U20606355, U20606359, U20606364, U20606366, U20606367.

 

Requirement: Action in accordance with Cessna SIL No. SE82-18. Compliance:  Within 100 hours time in service after 31 August 1982.

Background:  It has been established by the airframe manufacturer that the hottest cylinder during most critical flight stages is cylinder No. 3 as distinct from cylinder No. 1 where the temperature probe is currently located.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.