AD/CESSNA 400/59 - Fuselage Tailcone Structure - Modification
1AD/CESSNA 400/59 - Fuselage Tailcone Structure - Modification
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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 400/59 Fuselage Tailcone Structure - Modification 11/78
Applicability: All 401 and 411 series.
All model 402 with S/Nos. 402-0001 to 402B1361; All model 404 with S/Nos. 404-0001 to 404-0233; All model 414 with S/Nos. 414-0001 to 414A0071; All model 421 with S/Nos. 421-0001 to 421C0511; All model 441 with S/Nos. 441-0001 to 441-0059.
Document: Cessna SL ME78-24.
Compliance: Within 100 hours time in service after 30 November 1978.