CIVIL AVIATION ACT 1988
CIVIL AVIATION SAFETY REGULATIONS 1998
ISSUE OF AIRWORTHINESS DIRECTIVE
Under section 98 of the Civil Aviation Act 1988, 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. Subregulation 39.001(5) of the Civil Aviation Safety Regulations 1998 provides that an AD is a disallowable instrument for the purposes of section 46A of the Acts Interpretation Act 1901. Therefore, in accordance with section 6 of the Legislative Instruments Act 2003, an AD is a legislative 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 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 assess that information and, if appropriate, issue an Australian AD to mandate the requirements of the State of Design.
State of Design ADs issued on or after 1 October 2009 are defined as ADs per Civil Aviation Safety Regulations Part 39.001A.
CASA issued AD/CF34/5 Amdt 3 affecting General Electric CF34 series turbine engines. The United States FAA issued AD 2009-26-09 on 7 January 2010 which supersedes the requirements of AD/CF34/5 Amdt 3 and as such this AD has been cancelled. The United States is the state of design for these engines. The cancellation will become effective on 11 February 2010.
No consultation with the Australian public has taken place on this AD cancellation. The Office of Best Practice Regulation has determined that ADs do not require a Regulatory Impact Statement.
The AD 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.
Overview
The Civil Aviation Act 1988, enacted by the Australian Parliament, governs the regulation of civil aviation to ensure safety and efficiency. This Act provides the legal framework for the Australian Civil Aviation Safety Authority (CASA) to issue regulations, including airworthiness directives (ADs), under section 98 to maintain air navigation safety. The Civil Aviation Safety Regulations 1998, made under the authority of the Act, further detail the process for issuing ADs, which are legislative instruments used to mandate safety requirements for aircraft types. These regulations reflect international standards set by the International Civil Aviation Organization (ICAO) and are designed to ensure the continuing airworthiness of aircraft. CASA's role, as Australia's national airworthiness authority, is to assess and implement ADs issued by the aircraft's State of Design, ensuring compliance with safety standards. The ADs serve to address specific safety issues identified with certain aircraft types or aeronautical products, thereby mitigating risks associated with civil aviation operations.
Scope and Application
The Civil Aviation Act 1988, as supplemented by the Civil Aviation Safety Regulations 1998, governs the issuance of airworthiness directives (ADs) for the types of aircraft and aeronautical products registered in Australia. According to section 98 of the Act, the Governor-General has the authority to create regulations that serve the Act's objectives, particularly concerning the safety of air navigation. Regulation 39.001 specifically empowers the Civil Aviation Safety Authority (CASA) to issue ADs, which are formal mandates for the continuing airworthiness of aircraft and aeronautical products. These ADs are classified as disallowable instruments under the Acts Interpretation Act 1901 and are legislative instruments pursuant to the Legislative Instruments Act 2003. ADs are essential for ensuring that aircraft maintain their airworthiness, and CASA, as Australia's national airworthiness authority, is responsible for issuing them in response to ADs from the State of Design or based on its own assessments. In the case of AD/CF34/5 Amdt 3, CASA issued an AD affecting General Electric CF34 series turbine engines, which was later superseded and subsequently cancelled by a corresponding directive from the United States Federal Aviation Administration (FAA). The AD cancellation process does not require public consultation, as determined by the Office of Best Practice Regulation, and does not necessitate a Regulatory Impact Statement. The AD in question was made by the Manager, Continuing Airworthiness, within CASA's Airworthiness and Engineering Branch, in accordance with the Act's provisions.
Key Provisions
The Civil Aviation Act 1988 and the Civil Aviation Safety Regulations 1998 together provide the legal framework for issuing airworthiness directives (ADs) in Australia. Section 98 of the Civil Aviation Act 1988 allows the Governor-General to make regulations for the purposes of the Act, particularly concerning the safety of air navigation. Regulation 39.001 of the Civil Aviation Safety Regulations 1998 specifically empowers the Civil Aviation Safety Authority (CASA) to issue ADs for certain kinds of aircraft or aeronautical products. According to subregulation 39.001(5), an AD is a disallowable instrument under the Acts Interpretation Act 1901 and, therefore, constitutes a legislative instrument as defined by the Legislative Instruments Act 2003. This regulatory structure ensures that ADs, which are critical for maintaining the continuing airworthiness of aircraft, are issued in accordance with the international standards set by Annex 8 to the Convention on International Civil Aviation.
The obligations imposed by these provisions are substantial. The State of Design, which is the country where the aircraft or aeronautical product is designed, holds the primary responsibility for ensuring the continuing airworthiness of the type. It must provide necessary information to the appropriate States of Registry to maintain airworthiness. In Australia, CASA, as the national airworthiness authority, must assess information from the State of Design and issue corresponding ADs if necessary to mandate the required safety measures. When the United States issues an AD for a type of aircraft registered in Australia, such as the AD for General Electric CF34 series turbine engines, CASA must evaluate this information and decide whether to issue an Australian AD. This process ensures that Australian aircraft meet international safety standards.
Breach of the requirements set out in these ADs can lead to serious consequences. While the Civil Aviation Act 1988 and Civil Aviation Safety Regulations 1998 do not explicitly detail the penalties for non-compliance with ADs, general aviation regulations include provisions for enforcement actions. Non-compliance with ADs can result in civil penalties, such as fines or suspension of an aircraft's certificate of airworthiness. Criminal penalties may also apply in cases of gross negligence or willful disregard of safety regulations, potentially leading to imprisonment. These stringent measures underscore the importance of adhering to ADs to maintain the highest standards of aviation safety.