CASA ADCX 003/12 - Revocation of Airworthiness Directives

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Legislation au F2012L00218 Not in force Legislative Instrument

Legislation content

Explanatory Statement

 

Civil Aviation Regulations 1988

 

Revocation of Airworthiness Directives

 

Legislation

Under section 98 of the Civil Aviation Act 1988 (the Act), the Governor-General may make regulations for the purposes of the Act and in the interests of the safety of air navigation.  Under regulation 39.001 of the Civil Aviation Safety Regulations 1998, CASA may issue airworthiness directives (ADs) for kinds of aircraft or aeronautical products.  Under the previous subregulation 39.001(5) of CASR 1998, an AD was a legislative instrument.  This is still the situation under subsection 98(5B) of the Act.

Under Annex 8 to the Convention on International Civil Aviation, the State of Design has overall responsibility for continuing airworthiness of an aircraft type, and must provide any information necessary to ensure the continuing airworthiness of a type to appropriate States of Registry.  ADs (and their equivalents) are the most common form of continuing airworthiness information, and are issued by most ICAO Contracting States.

The State of Registry of an individual aircraft is responsible for its continuing airworthiness.  Under Annex 8, the State of Registry must develop or adopt requirements to ensure the continuing airworthiness of aircraft.  When a State of Design issues an AD against a type of aircraft on the Australian Register, CASA, as Australia’s national airworthiness authority, must accept that AD.  State of Design ADs issued on or after 1 October 2009 are defined as ADs per Civil Aviation Safety Regulations Part 39.001A.

AD/A330/4 Amdt 2

 

A State of Design airworthiness directive issued on or after 1 October 2009 is defined as an airworthiness directive per CASR Part 39.001A.  The requirements of this airworthiness directive have been superseded by EASA AD 2012-0020 issued on
30 January 2012.

 

AD/A330/5

 

A State of Design airworthiness directive issued on or after 1 October 2009 is defined as an airworthiness directive per CASR Part 39.001A.  The requirements of this airworthiness directive have been superseded by EASA AD 2012-0020 issued on
30 January 2012.

 

AD/A330/8

 

A State of Design airworthiness directive issued on or after 1 October 2009 is defined as an airworthiness directive per CASR Part 39.001A.  The requirements of this airworthiness directive have been superseded by EASA AD 2012-0020 issued on
30 January 2012.


AD/A330/10

 

A State of Design airworthiness directive issued on or after 1 October 2009 is defined as an airworthiness directive per CASR Part 39.001A.  The requirements of this airworthiness directive have been superseded by EASA AD 2012-0020 issued on
30 January 2012.

 

AD/A330/15 Amdt 1

 

A State of Design airworthiness directive issued on or after 1 October 2009 is defined as an airworthiness directive per CASR Part 39.001A.  The requirements of this airworthiness directive have been superseded by EASA AD 2012-0020 issued on
30 January 2012.

 

AD/A330/29

 

A State of Design airworthiness directive issued on or after 1 October 2009 is defined as an airworthiness directive per CASR Part 39.001A.  The requirements of this airworthiness directive have been superseded by EASA AD 2012-0020 issued on
30 January 2012.

 

AD/A330/54 Amdt 1

 

A State of Design airworthiness directive issued on or after 1 October 2009 is defined as an airworthiness directive per CASR Part 39.001A.  The requirements of this airworthiness directive have been superseded by EASA AD 2012-0020 issued on
30 January 2012.

 

AD/A330/103

 

A State of Design airworthiness directive issued on or after 1 October 2009 is defined as an airworthiness directive per CASR Part 39.001A.  The requirements of this airworthiness directive have been superseded by EASA AD 2012-0020 issued on
30 January 2012.

 

AD/AS 355/61 Amdt 1

 

A State of Design airworthiness directive issued on or after 1 October 2009 is defined as an airworthiness directive per CASR Part 39.001A.  The requirements of this airworthiness directive have been superseded by EASA AD 2012-022 issued on
2 February 2012.

 

AD/CESSNA 170/81

 

A State of Design airworthiness directive issued on or after 1 October 2009 is defined as an airworthiness directive per CASR Part 39.001A.  The requirements of this airworthiness directive which referred to FAA AD 2008-03-02 have been superseded by FAA AD 2012-02-02, effective 13 March 2012.


Consultation

Foreign State of Design ADs are defined as ADs by CASR regulation 39.001A. Therefore if an Australian AD has its requirements superseded by the requirements of a State of Design AD, those requirements may under regulation 39.001A be given effect to without public consultation.

 

The Office of Best Practice Regulation has determined that ADs do not require a Regulatory Impact Statement.

 

Compatibility with human rights and freedoms

This instrument is compatible with the human rights and freedoms recognised or declared in the international instruments listed in section 3 of the Human Rights (Parliamentary Scrutiny) Act 2011.

 

Human Rights Implications

The instrument sets out technical requirements as detailed above.  The instrument does not engage any of the applicable rights or freedoms.

 

Conclusion

The instrument is compatible with human rights and freedoms.

 

This AD cancellation has been made by the Manager, Continuing Airworthiness in the Airworthiness and Engineering Branch, on behalf of CASA, in accordance with subsection 94 (1) of the Act.

[Instrument number CASA ADCX 003/12]

Overview

The Civil Aviation Regulations 1988, enacted in 1988, were designed to regulate civil aviation in Australia and ensure the safety of air navigation. Under section 98 of the Civil Aviation Act 1988, the Governor-General has the authority to make regulations that align with the Act's objectives, specifically focusing on the safety of air navigation. The Civil Aviation Safety Regulations 1998, as amended, empower the Civil Aviation Safety Authority (CASA) to issue airworthiness directives (ADs) for specific types of aircraft or aeronautical products. This legislative framework addresses the need to maintain the airworthiness of aircraft registered in Australia and to comply with international standards set by the International Civil Aviation Organization (ICAO). The policy objective of these regulations is to ensure that aircraft operating in Australian airspace meet safety standards, thereby protecting public safety and maintaining the integrity of the aviation industry. This specific legislative instrument, F2012L00218, was developed under the authority of the Civil Aviation Act 1988 and the Civil Aviation Safety Regulations 1998. It serves to revoke certain airworthiness directives issued by the State of Design, which have been superseded by equivalent directives from other jurisdictions such as the European Aviation Safety Agency (EASA) and the Federal Aviation Administration (FAA). The revocation of these directives ensures that Australian aviation standards remain current and aligned with international best practices, maintaining the safety and reliability of aircraft registered in Australia. This action was taken by the Manager, Continuing Airworthiness in the Airworthiness and Engineering Branch, on behalf of CASA, in accordance with the provisions of the Civil Aviation Act 1988.

Scope and Application

The Civil Aviation Regulations 1988, as amended by F2012L00218, pertains to the revocation of certain airworthiness directives (ADs) that are specific to types of aircraft and aeronautical products. These regulations apply to individuals and entities engaged in the aviation industry, including aircraft operators, manufacturers, and maintenance service providers, who must comply with the ADs to ensure the safety of air navigation. The scope of the Act is national, as it governs civil aviation within Australia and aligns with international standards set by the International Civil Aviation Organization (ICAO). The revocation of these ADs occurs when they are superseded by newer directives issued by the State of Design or other recognised authorities, such as the European Aviation Safety Agency (EASA) or the Federal Aviation Administration (FAA). Notably, this legislative instrument does not require public consultation as it pertains to the technical adjustments of ADs. Furthermore, the instrument is deemed compatible with human rights and freedoms, as it does not infringe upon any recognised rights or freedoms, focusing solely on the technical requirements for airworthiness.

Key Provisions

The Civil Aviation Regulations 1988, under the authority of the Civil Aviation Act 1988, mandate the revocation of specific airworthiness directives (ADs) for certain aircraft types, as detailed in the explanatory statement. The primary operative sections involved in these revocations are sections 39.001, 98, and 98(5B) of the Civil Aviation Safety Regulations 1998 (CASR), as well as subsection 94(1) of the Civil Aviation Act 1988. Section 39.001 of the CASR empowers the Civil Aviation Safety Authority (CASA) to issue ADs, which are legislative instruments aimed at ensuring the continuing airworthiness of aircraft. These ADs are often issued by the State of Design, which has the overall responsibility for the continuing airworthiness of an aircraft type according to Annex 8 of the Convention on International Civil Aviation. The obligations imposed by these regulations require CASA to accept ADs issued by the State of Design if they pertain to aircraft on the Australian Register. Moreover, the State of Registry of an individual aircraft must develop or adopt requirements to ensure the continuing airworthiness of that aircraft, which aligns with Annex 8's guidelines. The revocations mentioned in the explanatory statement pertain to specific ADs for aircraft types such as the Airbus A330 and the Cessna 170, which have been superseded by newer directives issued by the European Aviation Safety Agency (EASA) and the Federal Aviation Administration (FAA). In terms of legal consequences, non-compliance with these ADs could potentially lead to serious safety issues and regulatory penalties. Although the explanatory statement does not detail specific penalties for breaches, under the Civil Aviation Act 1988, contraventions of airworthiness directives can lead to significant penalties. The maximum penalties can include fines and imprisonment, depending on the severity of the breach and its impact on aviation safety. Additionally, non-compliance could result in the grounding of aircraft, thereby affecting the operations of airlines and potentially leading to civil litigation for any damages caused by non-compliance. The compatibility of these regulations with human rights is also considered, as outlined in the Human Rights (Parliamentary Scrutiny) Act 2011. The explanatory statement asserts that the instrument does not engage any of the applicable rights or freedoms, ensuring its compatibility with the human rights and freedoms recognised in international instruments. Therefore, the instrument's provisions do not infringe upon any fundamental human rights or freedoms. This revocation has been authorised by the Manager, Continuing Airworthiness in the Airworthiness and Engineering Branch, on behalf of CASA, in accordance with the Civil Aviation Act 1988.

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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.