Document ID: chunk:federal_register_of_legislation:F2006B09633:body:0
Version: federal_register_of_legislation:F2006B09633
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Fokker F100 (F28 Mk 100) Series Aeroplanes

AD/F100/31 Flight Augmentation Computer Replacement 4/99

 Applicability: Model F.28 Mk.0100 aeroplanes serial numbers 11244 through 11348 inclusive.

             Requirement:  1. Unless previously accomplished replace all Collins Flight Augmentation Computer (FAC) units, part number (P/N) 622-7478-321, with modified units P/N 622-7478- 401 Mod.11 in accordance with Fokker Service Bulletin (SB) F100-22-026 dated 1 July 1991.

             2. Replace all Collins FAC units, P/N 622-7478-401, with modified units P/N 622-7478-401 Mod.11 in accordance with Fokker SB F100-22-032 dated
             2 September 1991.

            Note: Netherlands AD 1991-057/4 refers.

 Compliance: 1. Prior to 22 December 1999.

            2. Prior to 22 December 1999.

            This Airworthiness Directive becomes effective on 22 April 1999.

            Background: The modified computers provide improved fault isolation to allow cross comparison of more signals than previously possible. Problems with stabiliser trim systems during ground testing and nuisance yaw-damper faults during take off have been solved by the incorporation of an additional modification.