Document ID: chunk:federal_register_of_legislation:F2006B09889:body:0
Version: federal_register_of_legislation:F2006B09889
Segment Type: other
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Character Range: 0–1094

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.