AD/CESSNA 400/87 - Aileron Yoke Mounting Bracket Attachment - Inspection and Modification

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

Legislation au F2006B08370 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Cessna 400 Series Aeroplanes

 

AD/CESSNA 400/87 Aileron Yoke Mounting Bracket

Attachment - Inspection and Modification


4/83

 

Applicability: All models 402C with S/Nos. 402C0292 to 402C0528) All models 414A with S/Nos. 414A0498 to 414A0680) ** All models 421C with S/Nos. 421C0872 to 421C1115)

** Document No. 1 refers

 

All models 425 with S/Nos. 425-0002 to 425-0118 excepting S/Nos. 425-0107 and

425-0112 (Document No. 2 refers).

 

Document: 1. Cessna Customer Care S.I.L. ME82-57.

 

2. Cessna Customer Care S.I.L. PJ82-42. Compliance: Within 200 hours time in service after 30 April, 1983.

Background: Enlargement and elongation of the aileron yoke assembly attach holes and corresponding holes has been detected.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.