AD/HILLER 12/28 - Main Rotor Blade Anti-Node Bar - Inspection

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

Legislation au F2006B10355 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

 


Hiller UH-12 Series Helicopters

 

AD/HILLER 12/28 Main Rotor Blade Anti-Node Bar - Inspection 5/80

Applicability:  All models UH-12D, UH-12E, UH-12E4, H-23F, OH-23G and all models converted by STC178WE or STC177WE, equipped with main rotor blades Parsons P/N 2253- 1101-04.

 

Document: Hiller Aviation SB No. UH-12-51-5. Compliance:  As per requirement document.

Background:  The manufacturer states that anti-node bars with machine cut threads may be installed on certain main rotor blades of the subject P/N 2253-1101-04.

 

Note: The requirement for inspection of these blades has been removed from AD/HILLER 12/23 to this Directive.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.