Document ID: chunk:federal_register_of_legislation:F2006B09778:body:0
Version: federal_register_of_legislation:F2006B09778
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Fokker F28 Series Aeroplanes

 AD/F28/42
 Amdt 1

 Horizontal Stabiliser Hinge Bolt Retention - Inspection and Modification

 8/80

 Applicability: All models F28 with S/Nos. 11003 to 11145, 11147, 11150, 11151, 11991 and 11992.

             Requirement: 1. Inspect the retention of the horizontal stabiliser hinge bolts in accordance with RLD AD No. 79-89-55, or Fokker F28 SB No. F28/55-20.

             2. Modify the retention of the horizontal Stabiliser hinge bolts in accordance with RLD AD No. 80-37-55, OR Fokker SB No. F28/55-21.

 Compliance: 1. Before 1 June 1980.

            2. Before 1 November 1980.

            An overseas operator experienced migration of a horizontal stabiliser hinge bolt after loss of the retaining pin. This AD amendment adds a modification to provide back-up to bolt retention.