Document ID: chunk:federal_register_of_legislation:F2006B09797:body:0
Version: federal_register_of_legislation:F2006B09797
Segment Type: other
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Character Range: 0–649

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Fokker F28 Series Aeroplanes

AD/F28/62 Aileron Dual Input Quadrant Bracket 13/90

 Applicability: F28 aircraft with S/Nos 11003 through 11241, 11991 and 11992. Requirement:  Action in accordance with Fokker SB F28/27-177.
            Note: AD BLA 90-097 refers.

 Compliance: Prior to 30 April 1991, unless previously accomplished.

            Background: Country of origin AD. Severe pitting corrosion on the mounting brackets has been reported, together with incorrect installation of bushings.