AD/F50/38 - Auto Flight Idle Stop Mechanism Modification

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

Legislation au F2006B09864 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 F50 (F27 Mk 50) Series Aeroplanes

 

AD/F50/38 Auto Flight Idle Stop Mechanism Modification 10/90

Applicability: Model F50 series with serial numbers 20103 through 20108, 20110 through 20159,

20161 through 20173 and 20176 through 20178.

 

Requirement: Action in accordance with Fokker Service Bulletin F50-76-008 Revision 1.

 

Note: RLD AD 90-043 refers.

 

Compliance: Prior to 1 January 1991.

 

Background: Reports have been received of incidents where the power levers could not be retarded below flight idle during landing. This Directive requires a modification of the mechanism adjustment of the auto flight idle stop located on the engine

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.