AD/F27/108 - Rudder Trim Tab Control Bracket Attachment - Inspection

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

Legislation au F2006B09677 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/F27/108 Rudder Trim Tab Control Bracket Attachment - Inspection


6/86

 

Applicability: All Models.

 

Requirement: Fokker Service Bulletin F27/55-58.

 

NOTE: R.L.D. AD 85-31 refers.

 

Compliance: Prior to 15 July 1985.

 

Background:  Investigation into a flutter occurrence revealed that substitute rivets had been installed in the rib skin attachment of the rudder trim tab actuating bracket. The clamping qualities of the installed rivets may substantially reduce stiffness of the tab control attachment.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.