AD/CJ610/7 State of Design Airworthiness Directives

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2022L00972 In force Legislative Instrument

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Explanatory Statement

Civil Aviation Safety Regulations 1998

AD/CJ610/7 – State of Design Airworthiness Directives

Legislation

Under section 98 of the Civil Aviation Act 1988 (the Act), the Governor-General may make regulations for the purpose of carrying out and giving effect to the provisions of the Convention on International Civil Aviation relating to safety, amongst other things. Under regulation 39.001 of the Civil Aviation Safety Regulations 1998 (CASR), the Civil Aviation Safety Authority (CASA) may issue an airworthiness directive (AD) for a kind of aircraft or aeronautical product. Under subsections 98 (5B) and (5BA) of the Act, an AD is a legislative instrument unless it is expressed to apply in relation to a particular person, a particular aircraft or a particular aeronautical product. Under subsection 98 (5D) of the Act, a legislative instrument made under the regulations may apply, adopt or incorporate any matter contained in any instrument or other writing as in force or existing from time to time.

Under subsection 33 (3) of the Acts Interpretation Act 1901, where an Act confers a power to make, grant or issue any instrument of a legislative or administrative character (including rules, regulations or by-laws), the power shall be construed as including a power exercisable in the like manner and subject to the like conditions (if any) to repeal, rescind, revoke, amend, or vary any such instrument.

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 International Civil Aviation Organization 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 foreign State of Design issued an AD before 1 October 2009 for a type of aircraft on the Australian Register, CASA, as Australia’s national airworthiness authority, must assess that information and, if appropriate, issue an Australian AD to mandate the requirements of the foreign State of Design.

The United States of America Federal Aviation Administration (FAA) issued ADs 75‑19-05, 80-08-06R1, 85-18-03, 97‑25-08, 98-23-06 and 2001-10-12 affecting General Electric CJ610 series engines in 1975, 1981, 1985, 1997, 1998 and 2001 respectively. The United States of America is the State of Design for this engine series. As an aircraft fitted with this engine series has now been registered in Australia, and as the FAA ADs pre-date automatic acceptance of foreign ADs under Part 39 of CASR, CASA has issued AD/CJ610/7 to mandate the requirements of FAA ADs 75‑19-05, 80-08-06R1, 85-18-03, 97‑25-08, 98-23-06 and 2001-10-12.

 

Documents Incorporated by Reference

Under subsection 14 (2) of the Legislation Act 2003 (the LA), unless the contrary intention appears, a legislative instrument may not incorporate any matter contained in an instrument or other writing as existing from time to time. Subsection 98 (5D) of the Act provides that, despite section 14 of the LA, a legislative instrument made under the Act or the regulations may apply, adopt or incorporate any matter contained in any instrument or other writing as in force or existing from time to time.

FAA AD 75-19-05 provides instructions for the inspection and replacement of certain General Electric (GE) CJ610 accessory drive horizontal. For subsection 98 (5D) of the Act, the technical document is incorporated as it exists from time to time. The technical document is freely available from the following website address:

https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf/0/2FC56FB8683888FF8625682C0052ECB2?OpenDocument&Highlight=75-19-05

FAA AD 80-08-06R1 provides instructions for the replacement of certain GE CJ610 first stage turbine disks and second stage turbine disks. For subsection 98 (5D) of the Act, the technical document is incorporated as it exists from time to time. The technical document is freely available from the following website address:

https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf/0/DDB1EBB4E63C006D86256840005F92E7?OpenDocument&Highlight=80-08-06

FAA AD 85-18-03 provides instructions for the replacement of certain GE CJ610 stage 1 turbine disks. For subsection 98 (5D) of the Act, the technical document is incorporated as it exists from time to time. The technical document is freely available from the following website address:

https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf/0/2EDE4C77E2DAF75586256840005FFF77?OpenDocument&Highlight=85-18-03

FAA AD 97-25-08 provides instructions for the replacement of certain GE CJ610 turbine torque rings and compressor drive shafts. For subsection 98 (5D) of the Act, the technical document is incorporated as it exists from time to time. The technical document is freely available from the following website address:

https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf/0/36F824FD42BAE0A086256846006C1A01?OpenDocument&Highlight=97-25-08

FAA AD 98-23-06 provides instructions for the replacement of certain GE CJ610 combustion liner assemblies. For subsection 98 (5D) of the Act, the technical document is incorporated as it exists from time to time. The technical document is freely available from the following website address:

https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf/0/478326720EAA435086256846006C76CC?OpenDocument&Highlight=98-23-06

FAA AD 2001-10-12 provides instructions for the removal from service of GE CJ610 unapproved parts. For subsection 98 (5D) of the Act, the technical document is incorporated as it exists from time to time. The technical document is freely available from the following website address:

https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf/0/088BB6060FB45AD086256A56005F9E4E?OpenDocument&Highlight=2001-10-12

Consultation

As AD/CJ610/7 is being made in accordance with CASA’s obligations under Annex 8 to the Convention on International Civil Aviation, it is CASA’s view that it was not necessary or appropriate to undertake any further consultation under section 17 of the Legislation Act 2003.

Sector risk, economic and cost impact

Subsection 9A (1) of the Act states that, in exercising its powers and performing its functions, CASA must regard the safety of air navigation as the most important consideration. Subsection 9A (3) of the Act states that, subject to subsection (1), in developing and promulgating aviation safety standards under paragraph 9 (1) (c), CASA must:

(a) consider the economic and cost impact on individuals, businesses and the community of the standards; and

(b) take into account the differing risks associated with different industry sectors.

The cost impact of a standard refers to the direct cost (in the sense of price or expense) which a standard would cause individuals, businesses and the community to incur. The economic impact of a standard refers to the impact a standard would have on the production, distribution and use of wealth across the economy, at the level of the individual, relevant businesses in the aviation sector, and the community more broadly. The economic impact of a standard could also include the general financial impact of that standard on different industry sectors.

The economic and cost impact of the instrument has been determined by:

(a) the identification of individuals and businesses affected by the instrument;

(b) consideration of how the requirements to be imposed on individuals and businesses under the instrument will be different compared to existing requirements;

(c) a valuation of the impact, in terms of direct costs on individuals and businesses affected by the instrument to comply with the different requirements. This valuation is consistent with the principles of best practice regulation of the Australian Government.

CASA has assessed that the economic and cost impact of the instrument is not significant and the operator of the one affected aircraft currently on the Australian aircraft register should already be compliant with the AD. The requirements of the instrument apply to holders of certificates of registration of relevant aircraft.

Impact on categories of operations

The instrument is likely to have no effect on operations conducted by the relevant aircraft because the aircraft should already be compliant with the AD.

Impact on regional and remote communities

The instrument will not have a negative impact on regional and remote communities.

Regulation Impact Statement

A Regulation Impact Statement (RIS) is not required because ADs are covered by a standing agreement between CASA and the Office of Best Practice Regulation under which a RIS is not required for ADs (OBPR id. 14507).

Statement of Compatibility with Human Rights

A Statement of Compatibility with Human Rights is at Attachment 1.

Making and commencement

The instrument has been made by a delegate of CASA relying on the power of delegation under subregulation 11.260 (1) of CASR and subsection 94 (1) of the Act.

As an instrument relating to aviation safety made under CASR, Part 4 of Chapter 3 of the Legislation Act 2003 (sunsetting of legislative instruments) does not apply to this instrument (item 15 of the table in section 12 of the Legislation (Exemptions and Other Matters) Regulation 2015). The instrument requires that the action set out in the instrument, that relates to aircraft or aeronautical products, be taken to correct an unsafe condition. As such, the instrument is intended to have enduring operation and it would not be appropriate for it to be subject to sunsetting.

The instrument commences on 15 July 2022.

[Instrument number AD/CJ610/7]


Attachment 1

Statement of Compatibility with Human Rights

Prepared in accordance with Part 3 of the
Human Rights (Parliamentary Scrutiny) Act 2011

AD/CJ610/7 - State of Design Airworthiness Directives

This legislative 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.

Overview of the legislative instrument

The United States of America Federal Aviation Administration (FAA) issued ADs 75‑19-05, 80-08-06R1, 85-18-03, 97‑25-08, 98-23-06 and 2001-10-12 affecting General Electric CJ610 series engines in 1975, 1981, 1985, 1997, 1998 and 2001 respectively. The United States of America is the State of Design for this engine series. As an aircraft fitted with this engine series has now been registered in Australia, and as the FAA ADs pre-date automatic acceptance of foreign ADs under Part 39 of CASR, CASA has issued AD/CJ610/7 to mandate the requirements of FAA ADs 75‑19-05, 80-08-06R1, 85-18-03, 97-25-08, 98-23-06 and 2001-10-12.

The primary purpose of this legislative instrument is to mandate the requirements of FAA ADs 75‑19-05, 80-08-06R1, 85-18-03, 97-25-08, 98-23-06 and 2001-10-12.

Human rights implications

This legislative instrument does not engage any of the applicable rights or freedoms.

Conclusion

This legislative instrument is compatible with human rights as it does not raise any human rights issues.

Civil Aviation Safety Authority

Interactions

Authorises

All Versions

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.