AD/CESSNA 400/37 - Crankcase Oil Separator Return Line Check Valve - Incorporation of
1AD/CESSNA 400/37 - Crankcase Oil Separator Return Line Check Valve - Incorporation of
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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
- FAA AD 73-13-8.
Effective: 28 September 1973.