Airworthiness Directives 2004 - Revocation and Remaking - Airbus Industrie A330 Series Aeroplanes

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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

 Airbus Industrie A330 Series Aeroplanes

 AD Name AD Number

 Pitot Probes AD/A330/1

 Digital Distance and Radio Magnetic Indicators AD/A330/2 Amdt 1

 Escape Slide Girt Bar Slider Mechanism AD/A330/3 Amdt 2

 THSA - Operational Life Limit AD/A330/4

 Elevator Servo Control - Operational Life Limit AD/A330/5

 Emergency Door 3 Type I - Escape Slide Parachute Pin AD/A330/6

 THSA  Transfer Tube AD/A330/7 Amdt 2

 Aileron Servo Control - Life Limits AD/A330/8

 Nose Landing Gear AD/A330/9 Amdt 2

 Spoiler Servo Control Unit - Inspection AD/A330/10

 Pitot Probes AD/A330/11

 Ram Air Turbine Rotary Solenoids AD/A330/12 Amdt 1

 Life Limits/Monitored Parts AD/A330/13 Amdt 2

 Windshield Central Retainer AD/A330/14 Amdt 1

 Flap Rotary Actuators AD/A330/15 Amdt 1

 Rudder Servo-Controls AD/A330/16

 Type A Passenger/Crew Door Slide Rafts and Type 1 Emergency Door Slides AD/A330/17 Amdt 2

 Forward Fuselage Frame 12A Stiffener AD/A330/18

 Thrust Reverser - Directional Pilot Valve Pressure Test/Replacement AD/A330/19

 Leading Edge Slat Rotary Actuator Type A - Inspection AD/A330/20

 Low Pressure Fuel Shut-Off Valve AD/A330/21 Amdt 1

 Flight Manual Amendment - Fuel Leak Procedure AD/A330/22

 Elevator Servo Control Transducer Attachment lug Inspection and FCOM  AD/A330/23 Amdt 1

 This AD not issued AD/A330/24

 Auxiliary Power Unit Control Box AD/A330/25

 Spoiler Servo-Controls Life Limitations AD/A330/26

 Nose Wheel Steering Limits AD/A330/27 Amdt 1

 Flight Control Primary Computer AD/A330/28

 'SAMM' Elevator Servo-control AD/A330/29


 Argo-Tech/Intertechnique Vent Float Valves AD/A330/30 Amdt 1

 Airworthiness Limitations Items - Time Limits/Maintenance Checks AD/A330/31

 Main Landing Gear Retraction Actuator Piston Rod AD/A330/32 Amdt 1

 Air Conditioning Pack Ram Air Outlet Ducts AD/A330/33

 MLG Retraction Actuator Lower Pin AD/A330/34

 Aileron Servo Control Fittings Attachment AD/A330/35

 Main Landing Gear Wheel Axles AD/A330/36

 Elevator Servocontrols AD/A330/37 Amdt 1

 Liquid Crystal Display Units AD/A330/38

 Elevator Structure AD/A330/39 Amdt 1

 Jettison Valve Mounting AD/A330/40

 Passenger Gaseous Oxygen Containers diaphragm AD/A330/41

 Integrated Standby Instrument System AD/A330/42

 Cockpit Instrument Panel AD/A330/43

 Cargo Restraint Strap Assemblies AD/A330/44

 

Overview

The Airworthiness Directives 2004, enacted under the authority of the Civil Aviation Safety Regulations 1998, was introduced to address the need for updating and ensuring compliance with current safety standards for specific aircraft components. This legislative instrument was enacted by David Alan Villiers, acting as the delegate of the Civil Aviation Safety Authority, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The policy objective of these directives is to ensure that all aircraft parts and systems continue to meet airworthiness standards, thereby enhancing the safety and reliability of air travel. Each Airworthiness Directive was re-made in exactly the same form as it appears in the latest published edition of the directive to ensure that operators and maintenance personnel have access to the most current safety information.

Scope and Application

The Airworthiness Directives 2004, made under the Civil Aviation Safety Regulations 1998, applies to all aircraft, specifically Airbus Industrie A330 Series Aeroplanes, within the Commonwealth of Australia. These directives are issued by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, and are aimed at ensuring the airworthiness of the specified aircraft through a series of amendments and remakings of previously issued directives. Each Airworthiness Directive in Schedule 1 has been re-made to match the latest published edition, ensuring that all safety requirements and technical standards are consistently applied across the aviation industry. The directives cover a wide range of aircraft components and systems, including pitot probes, digital distance and radio magnetic indicators, and various structural and operational aspects of the A330 series. These directives do not specify any exclusions or exemptions, and apply uniformly to all aircraft operators and maintenance providers within Australia. The application of these directives is further extended through subordinate instruments as needed to maintain safety standards and regulatory compliance.

Key Provisions

The Airworthiness Directives 2004, made under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, primarily focuses on the revocation and remaking of specific Airworthiness Directives (ADs) for Airbus Industrie A330 Series Aeroplanes. Section (a) revokes the listed ADs, while section (b) re-issues them as separate instruments, each mirroring the latest published edition of the directive (section 2). This legislative instrument aims to ensure that the ADs remain current and accurately reflect any changes or updates in safety requirements and maintenance procedures for the specified aircraft models. The obligations imposed by these ADs on the parties or entities they govern are significant. They must ensure compliance with the detailed safety instructions and maintenance requirements outlined in each directive. These obligations encompass regular inspections, repairs, modifications, and adherence to specified time limits and operational life limits for various aircraft components. The ADs cover a range of critical systems and parts, including pitot probes, digital distance and radio magnetic indicators, escape slide mechanisms, and structural components such as landing gear and fuselage frames. Non-compliance with these directives could result in serious safety risks and regulatory penalties. Violations of the Airworthiness Directives 2004 can lead to substantial legal consequences. Section 39.001 (1) of the Civil Aviation Safety Regulations 1998 specifies that failure to comply with an AD can result in both civil and criminal penalties. Civil penalties may include fines and enforcement actions taken by the Civil Aviation Safety Authority (CASA). Criminal penalties could be applicable in cases of gross negligence or willful disregard of safety regulations, potentially leading to imprisonment. The exact penalties, including maximum fines and imprisonment terms, depend on the specific circumstances of the breach and the severity of the non-compliance. Ensuring adherence to these directives is therefore crucial for maintaining air safety and avoiding severe legal repercussions.

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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.