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

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B10705 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.