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

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