Document ID: chunk:federal_register_of_legislation:F2006B10705:body:0
Version: federal_register_of_legislation:F2006B10705
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters

 AD/HU 369/43 Main Rotor Blade Root Fitting Assemblies
                    and Lead-Lag Assemblies - Inspection

 2/80

 Applicability: All model 369H with component S/Nos. as listed in the requirement document. Document:               Hughes SIN No. HN-140.
 Compliance: Part 1 - Initial Inspection - within 25 hours time in service after 3 January 1980.

Part 2 - Periodic Inspection - as detailed in requirement document.

Background: Cracking of the main rotor hub lead-lag link attach lugs has been reported in service.