COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
Airbus A330 Series Aeroplanes
AD/A330/8 Aileron Servo Control - Life Limits 13/2002
Applicability: Airbus A330 Series aeroplanes.
Requirement: Action as detailed in the DGAC AD 2001-530(B).
Note: DGAC AD 2001-530(B) refers.
Compliance: As detailed in the requirement document, with a revised effective date of 26 December 2002.
This Airworthiness Directive becomes effective on 26 December 2002.
Background: This directive specifies an “operational life limit” for the Aileron Servo Control which is inappropriate to be included in Section 9 of the Maintenance Planning Document (MPD) which specifies “ structural life limits”.
James Coyne
Delegate of the Civil Aviation Safety Authority 19 November 2002
The above AD is notified in the Commonwealth of Australia Gazette on 4 December 2002.
Overview
The Civil Aviation Regulations 1998 (CAR 1998) are a critical piece of Australian legislation governing civil aviation safety. Enacted in 1998, these regulations were designed to ensure that all civil aviation activities within Australia adhere to stringent safety standards. This is achieved through a comprehensive framework that encompasses aircraft design, manufacture, operation, and maintenance. The CAR 1998 was introduced to address the need for a cohesive and enforceable set of regulations that could be uniformly applied across the aviation industry to mitigate risks and enhance safety. The Civil Aviation Safety Authority (CASA) is the enacting body responsible for administering these regulations, with the overarching policy objective of maintaining the highest possible safety standards in Australian civil aviation. The regulations provide a detailed, rule-based approach to ensuring that all aviation activities comply with established safety protocols.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, establishes the scope and application of Airworthiness Directives (AD) issued by the Civil Aviation Safety Authority (CASA). These regulations pertain to all aircraft and aeronautical products operating within the Commonwealth of Australia. The directive for the Airbus A330 Series aeroplanes, AD/A330/8, addresses the Aileron Servo Control life limits, and mandates that the specified corrective actions as detailed in the DGAC AD 2001-530(B) be implemented by operators of these aircraft. The directive applies exclusively to Airbus A330 Series aeroplanes and necessitates compliance with the actions and timing outlined in the requirement and compliance sections of the directive. This particular AD was issued on 19 November 2002 and became effective on 26 December 2002, following its notification in the Commonwealth of Australia Gazette on 4 December 2002. The AD does not include any stated exclusions, exemptions, or thresholds, and its application is limited to the specified aircraft type and conditions.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39, which deals with airworthiness directives, contains specific provisions that are crucial for ensuring the safety of aircraft. Section 39.1 (1) allows the Civil Aviation Safety Authority (CASA) to issue airworthiness directives to address unsafe conditions. An example of such a directive is AD/A330/8, which pertains to Airbus A330 Series aeroplanes. This directive sets forth the requirements for maintaining the aileron servo control life limits, referencing DGAC AD 2001-530(B) for detailed action (Section 13/2002). The applicability of this directive extends to all Airbus A330 Series aeroplanes, necessitating specific actions to be taken in accordance with the detailed instructions provided.
The obligations under this airworthiness directive include adherence to the specified action detailed in DGAC AD 2001-530(B) to ensure that the aileron servo control life limits are appropriately managed. Operators of Airbus A330 Series aeroplanes must comply with these requirements to maintain the aircraft's airworthiness. This involves updating the Maintenance Planning Document (MPD) to reflect the new operational life limits for the aileron servo control, ensuring that these limits are distinct from structural life limits as outlined in Section 9 of the MPD. The directive mandates that these actions be completed by a specified date, ensuring that all relevant parties are aware of their responsibilities and the timeline for compliance.
Failure to comply with the provisions outlined in the airworthiness directive may result in serious consequences. Under the Civil Aviation Regulations 1998, non-compliance can lead to enforcement actions by CASA. The specific penalties for breaching these regulations may include substantial fines and potential grounding of the aircraft. The exact penalties are not explicitly stated in the text but generally, such breaches can attract severe financial penalties and administrative actions. These measures are in place to ensure that all stakeholders prioritise the safety and airworthiness of the aircraft, maintaining the highest standards of aviation safety.