AD/HS 125/66 - Main Landing Gear Wheels - Inspection
1AD/HS 125/66 - Main Landing Gear Wheels - Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.