AD/HU 369/43 - Main Rotor Blade Root Fitting Assemblies and Lead-Lag Assemblies - Inspection
1AD/HU 369/43 - Main Rotor Blade Root Fitting Assemblies and Lead-Lag Assemblies - 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 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.