AD/HU 269/62 Amdt 1 - Tail Rotor Hub - Inspection and Modification

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

Legislation au F2006B10623 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 269/62

Amdt 1


Tail Rotor Hub - Inspection and Modification 3/82

 

Applicability: All model 269C with S/Nos. 0004 to 0716.

 

All model 269A, TH-55A, 269A-1 and 269B with LTS tail rotor assembly P/N 269A6034 Series.

 

All P/N 369A1725and 369A1725-501 tail rotor hub assemblies. All P/N 369A1725-5 tail rotor assemblies with S/Nos. 001 to 862.

Document: Hughes SIN No. N-153.1.

 

Compliance: Within 100 hours time in service after 31 March, 1982.

 

Background: Manufacturer’s SI Notice Revision 1 extends part number effectivity.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.