AD/CESSNA 400/37 - Crankcase Oil Separator Return Line Check Valve - Incorporation of

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Legislation au F2006B08323 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 400/37 Crankcase Oil Separator Return Line

Check Valve - Incorporation of


8/73

 

Applicability: Model 421B S/Nos. 421B0260 to 421B0346 fitted with new Airesearch TH0871 turbochargers with S/No. prefixes BC or later. S/Nos. 421B0001 to 421B0259 fitted with new Airesearch TH0871 turbochargers with S/No. prefixes BC or later or with remanufactured Airesearch TH0871 turbo-chargers with S/No. prefixes BCR or later.

 

Document: 1. Cessna SL ME73-10; or

 

2. FAA AD 73-13-8.

 

Effective: 28 September 1973.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.