Federal Register of Legislation
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
Agusta A109 Series Helicopters
AD Name AD Number
Main Rotor Blade AD/A109/1 Amdt 3
Tail Rotor Blade Root Fitting AD/A109/2 Amdt 3
Passenger and Pilots Door Emergency Release Mechanism AD/A109/3 Amdt 1
Retirement Lives - Fatigue Critical Components - CANCELLED AD/A109/4 Amdt 3
MLG Actuator Bracket Assembly Attachment Bolts - CANCELLED AD/A109/5 Amdt 1
Swashplate Bearing AD/A109/6
Superflexit Fuel Tanks AD/A109/7
Tail Rotor Blades AD/A109/8 Amdt 1
Engine Mount Installation AD/A109/9
Nose Landing Gear Actuator AD/A109/10
Emergency Float Assembly P/N 109-0715-01 AD/A109/11
Main Landing Gear Stiffening Struts AD/A109/12
Electrical Connectors P/N MS3456W14S-5S AD/A109/13
Main Landing Gear Wheels AD/A109/14
Modification of Overhead Console Relay Boards AD/A109/15
Main Rotor Blades AD/A109/16 Amdt 3
Main Gearbox Gleason Crown Bolts AD/A109/17 Amdt 1
Upper Transmission Mount Fitting AD/A109/18 Amdt 3
Tail Rotor Hub AD/A109/19 Amdt 2
Main Rotor Hydraulic Actuators AD/A109/20
Aircruiser Emergency Floats AD/A109/21
Sliding Doors Emergency Exit Panel AD/A109/22
Tail Boom and Vertical Fin Modification AD/A109/23
Main Rotor Blade - Trailing Edge AD/A109/24
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