Airworthiness Directives 2004 - Revocation and Remaking - Eurocopter EC 135 Series Helicopters

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 Airworthiness Directives 2004

 I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety

 Authority, acting under subregulation 39.001 (1) of the Civil

 Aviation Safety Regulations 1998:

 (a) revoke the Airworthiness Directives mentioned in

 Schedule 1; and

 (b) make, as separate instruments, each Airworthiness

 Directive mentioned in Schedule 1 and attached.

 

 

 David Villiers

 Delegate of the Civil Aviation Safety Authority

 

  20 December 2004

 Note:   Each attached Airworthiness Directive is being re-made in exactly the

 same form as appears in the latest published edition of the Directive.

 


 Schedule 1 Revocation and Remaking of

 Airworthiness Directives

 Eurocopter EC 135 Series Helicopters

 AD Name AD Number

 Main Rotor Hub-Shaft AD/EC 135/1 Amdt 1

 Tail Rotor Drive Shaft Bearing Attachment Flange AD/EC 135/2

 Tail Boom Bearing Supports AD/EC 135/3

 Air Conditioning System AD/EC 135/4

 Main Rotor Drive Torque Struts AD/EC 135/5 Amdt 3

 SMD45H Display Systems AD/EC 135/6

 Automatic Engine Control AD/EC 135/7 Amdt 1

 FADEC Fail Warning Light AD/EC 135/8

 Main Rotor Hydraulic Actuators - CANCELLED AD/EC 135/9

 

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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.