AD/CESSNA 206/32 - Turbocharger

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

Legislation au F2006B05237 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 206 Series Aeroplanes

 

AD/CESSNA 206/32 Turbocharger 6/80

Applicability: Model U206 S/Nos. U2060487 thru U20605619;

 

Model P206 S/Nos. P2060001, P2060191 thru P20600647.

 

Requirement: Action in accordance with Cessna SIL No. SE 80-24.

 

Note: FAA AD 80-07-01 Amdt. 39-3719 refers.

 

Compliance: Within 100 hours time in service after 30 June 1980.

 

Background: This Directive is issued to preclude a failure of the turbocharger anti-rotation pin and its ingestion into the scavenge pump. This in turn could cause a failure of both the pressure and scavenge pumps.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.