AD/HU 269/29 - Tail Rotor Blade Assembly - Inspection

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

Legislation au F2006B10600 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

 


Schweizer (Hughes) 269 Series Helicopters

 

AD/HU 269/29 Tail Rotor Blade Assembly - Inspection 12/68

Applicability: All models with tail rotor blade assemblies S/Nos up to and including 126-3312. Document:              Hughes SIN N-58.

Compliance: Within 25 hours time in service after 9 December 1968 and thereafter at intervals not exceeding 25 hours time 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.