AD/F27/107 - Inboard Aileron Hinge Bolt Retention - Inspection and Replacement

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

Legislation au F2006B09676 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

 


Fokker F27 Series Aeroplanes

 

AD/F27/107  Inboard Aileron Hinge Bolt Retention - Inspection and Replacement

Applicability: All model F27 with S/Nos. 10105 to 10635. Document:  Fokker SB F27/57-58.

Note: RLD AD BLA 83-20-57 refers.

 

Compliance: Before 1st January 1984.


8/83

 

Background: Restricted aileron movement was reported due to migration of hinge bolt and bush.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.