AD/CESSNA 400/7 - Turbocharger Air Inlet Duct - Inspection

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

Legislation au F2006B08353 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 400 Series Aeroplanes

 

AD/CESSNA 400/7 Turbocharger Air Inlet Duct - Inspection 1/69

Applicability: All models 401 and 402 with S/Nos. below 401-0145 and 402-0145.

 

Requirement: Visually inspect the fibreglass inlet duct to the turbocharger compressor for signs of cracking and or breakup.

 

Compliance: Within 25 hours time in service after 14 February 1969 and there- after at intervals not exceeding 100 hours time in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.