AD/F50/60 Amdt 1 - Bottom Hinged Cowl Door

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

Legislation au F2006B09889 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/F50/60

Amdt 1


Bottom Hinged Cowl Door 7/93

 

Applicability: Model F27 Mk.050 with serial numbers 20103 through 20265. Requirement:  Action in accordance with Fokker Service Bulletin F50-71-035 Revision 1.

Note: RLD AD 93-032/2 (A) refers.

 

Compliance: Within 650 hours time in service after 29 April 1993 or prior to 1 September 1993, whichever occurs first.

 

The compliance time of this Directive remains unchanged. This Amendment is effective from 24 June 1993.

Background: Reports have been received of fluid accumulating in the aft section of the engine bottom hinged cowl door. The introduction of a drain hole in the affected cowl door will prevent the accumulation of possibly flammable fluids.

 

Amendment 1 is issued in response to a revision of the Requirement Document which requires a new (different) drain hole location.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.