Document ID: chunk:federal_register_of_legislation:F2006B10506:body:0
Version: federal_register_of_legislation:F2006B10506
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 British Aerospace BAe 125 Series Aeroplanes

AD/HS 125/66 Main Landing Gear Wheels - Inspection 8/84

 Applicability: All models HS/DH/BH 125 Series aircraft up to and including Series 700. Requirement:               British Aerospace 125 SB No. 32-201.
            Note: The eddy current scan pattern shall be as shown in Fig. 1 of Appendix A and the probe shall be jigged to ensure that the scan index is accurately maintained.

 Compliance: Inspect prior to 31 August 1984, as detailed in the Requirement Document. Background:               Main wheel flange fracture has occurred with resultant structural damage.