Document ID: chunk:federal_register_of_legislation:F2006B09676:body:0
Version: federal_register_of_legislation:F2006B09676
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Character Range: 0–556

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

 Fokker F27 Series Aeroplanes

                  AD/F27/107  Inboard Aileron Hinge Bolt Retention - Inspection and Replacement

 Applicability: All model F27 with S/Nos. 10105 to 10635. Document:  Fokker SB F27/57-58.
            Note: RLD AD BLA 83-20-57 refers.

 Compliance: Before 1st January 1984.

8/83

 Background: Restricted aileron movement was reported due to migration of hinge bolt and bush.