AD/F27/121 - Flight Controls - Elevator Trim System

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

Legislation au F2006B09688 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/F27/121 Flight Controls - Elevator Trim System 2/91

Applicability: F27 aircraft with S/No’s 10102 to 10684 inclusive, 10686, 10687 and 10689 to 10692 inclusive.

 

Requirement: Action in accordance with the technical requirements of Netherlands AD BLA 90-106.

 

Note: Fokker SB F27/27-130 refers.

 

Compliance: As specified in the Requirement document with effective date 5 October 1990.

 

Background: Country of origin AD. To modify the elevator and trim tab systems so that they are considerably more resistant to flutter and easier to maintain.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.