Document ID: chunk:federal_register_of_legislation:F2006B10600:body:0
Version: federal_register_of_legislation:F2006B10600
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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.