AD/CFM56/15 Amdt 2 - Fuel Filter Cover Attachment Inspection

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

Legislation au F2017L00910 In force Legislative Instrument

Legislation content

Explanatory Statement

Civil Aviation Safety Regulations 1998

AD/CFM56/15 Amdt 2 Fuel Filter Cover Attachment Inspection

Legislation

Under section 98 of the Civil Aviation Act 1988 (the Act), the Governor-General may make regulations. Under regulation 39.001 of the Civil Aviation Safety Regulations 1998 (CASR 1998), 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. Therefore, this AD is a legislative instrument.

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. AD/CFM56/15 Amdt 2 applies to the CFM International CFM56-3 Series engines.

The French Direction Generale De L’Aviation Civile (DGAC) issued AD 1999245(B)R1 affecting CFM International (CFMI) CFM56-3 series engines in 1999. France is the State of Design for this engine type. CASA subsequently issued AD/CFM56/15 Amdt 1 to mandate the requirements of French DGAC AD 1999-245(B)R1. As a result of a request from industry CASA has issued AD/CFM56/15 Amdt 2 to correct a minor typographical error in the number of the DGAC AD referenced. This AD repeals and replaces the previous AD on this subject.

 

DGAC France AD 1999-245(B)R1 is freely available on the EASA website at:

 

https://ad.easa.europa.eu/ad/F-1999-245R1

 

The CFMI Service Bulletins referred to in the AD can be obtained from CFMI, however, any Australian aircraft operator which operates aircraft fitted with CFMI engines are provided with these documents by CFMI by subscription.

Consultation

This AD is being made at the request of industry. As this AD amendment is of a minor or machinery nature and does not substantially alter existing arrangements apart from correcting a minor typographical error in a referenced document number, 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.

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.

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 1998 and subsection 94 (1) of the Act.

The instrument commences on 19 July 2017.

[Instrument number AD/CFM56/15 Amdt 2]


Attachment 1

Statement of Compatibility with Human Rights

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

AD/CFM56/15 Amdt 2 Fuel Filter Cover Attachment Inspection

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 French Direction Generale De L’Aviation Civile (DGAC) issued AD 1999245(B)R1 affecting CFM International CFM56-3 series engines in 1999. France is the State of Design for this engine type. CASA subsequently issued AD/CFM56/15 Amdt 1 to mandate the requirements of French DGAC AD 1999-245(B)R1. As a result of a request from industry CASA has repealed and replaced AD/CFM56/15 Amdt 1 to correct a minor typographical error in the number of the DGAC AD referenced.

The primary purpose of this legislative instrument is to correct a typographical error in the number of a referenced document.

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

Overview

The Civil Aviation Safety Regulations 1998 were enacted to ensure the safety and airworthiness of civil aviation in Australia. These regulations empower the Civil Aviation Safety Authority (CASA) to issue airworthiness directives (AD) under regulation 39.001, thereby aligning Australian regulations with international standards. This authority is derived from section 98 of the Civil Aviation Act 1988, which allows the Governor-General to make regulations for the purposes of the Act. AD/CFM56/15 Amdt 2, a legislative instrument made under this framework, addresses a specific issue identified by industry, namely a typographical error in a referenced document number within an existing AD concerning CFM International CFM56-3 series engines. The policy objective is to ensure the accuracy and reliability of regulatory documents, thereby maintaining the high standards of aviation safety. This amendment was made at the request of industry and does not require additional consultation or a Regulation Impact Statement, as it involves a minor correction rather than a substantive change.

Scope and Application

The AD/CFM56/15 Amdt 2 pertains to the CFM International CFM56-3 Series engines, which are subject to regulations under the Civil Aviation Safety Regulations 1998. This legislative instrument applies to any Australian aircraft operator that operates aircraft fitted with CFM56-3 series engines. The regulation is a response to a minor typographical error correction in a referenced airworthiness directive (AD) issued by the French Direction Generale De L’Aviation Civile (DGAC), which was originally issued as AD 1999-245(B)R1. As the State of Design for this engine type, France holds responsibility for the continuing airworthiness of the CFM56-3 series engines, and CASA, as Australia's national airworthiness authority, must assess and implement the necessary requirements for these engines on the Australian Register. The AD/CFM56/15 Amdt 2 is issued under the authority of the Civil Aviation Act 1988 and the Civil Aviation Safety Regulations 1998, and it is applicable nationwide. The AD is a legislative instrument that mandates compliance with the corrected AD, ensuring that the engines meet the necessary safety standards. No exclusions or exemptions are explicitly stated in this legislative instrument. However, it is worth noting that the AD is made in response to a minor typographical error correction in a referenced document, and it is not intended to substantially alter existing arrangements. The AD/CFM56/15 Amdt 2 repeals and replaces the previous AD on this subject, ensuring that the corrected reference is implemented across the relevant aircraft operators. Furthermore, the AD does not require a Regulation Impact Statement or additional consultation, as it is of a minor nature and does not significantly change existing arrangements.

Key Provisions

The key provisions of this legislation concern the amendment of an airworthiness directive (AD) issued under the Civil Aviation Safety Regulations 1998 (CASR 1998). Specifically, AD/CFM56/15 Amdt 2 pertains to the correction of a typographical error in a referenced document number for AD 1999-245(B)R1 issued by the French Direction Generale De L’Aviation Civile (DGAC) affecting CFM International (CFMI) CFM56-3 series engines. This amendment was made at the request of industry and does not substantially alter existing requirements. The primary objective is to ensure the accuracy of the referenced document number for compliance purposes. The obligations imposed by this amendment are relatively straightforward. Aircraft operators and maintenance organisations must ensure that their compliance procedures and records accurately reflect the corrected document number. This includes updating any references to the corrected AD in their documentation, ensuring that maintenance and inspection tasks are performed in accordance with the accurate AD, and maintaining records that demonstrate compliance with the corrected AD. Essentially, the amendment requires operators and maintenance organisations to rectify any discrepancies caused by the typographical error to maintain the airworthiness of the affected aircraft. Regarding potential consequences for non-compliance, the AD itself does not specify particular offences or penalties. However, non-compliance with ADs generally can lead to serious consequences under the Civil Aviation Act 1988. Operators and maintenance organisations that fail to comply with an AD can be subject to enforcement actions by the Civil Aviation Safety Authority (CASA). This may include administrative penalties, enforcement notices, or in severe cases, legal proceedings that could result in substantial fines or other sanctions. The severity of the consequences will depend on the nature and extent of the non-compliance, but the overarching principle is that maintaining the airworthiness of aircraft is a strict requirement. The legislative instrument also includes a Statement of Compatibility with Human Rights, affirming that the amendment does not engage any of the applicable rights or freedoms as recognised in international human rights instruments. This statement underscores the fact that the amendment is purely a technical correction and does not impact any human rights considerations. The amendment’s focus on correcting a typographical error ensures that it remains within the bounds of necessary administrative corrections, without any broader implications for human rights.

Legal classification tags

Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Repeal & Amendment
Offence Provisions

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.