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.
The JCAB has issued AD TCD-6832-2006 affecting Fuji FA-200 model aircraft. Japan is the State of Design for this type. CASA has assessed this AD and has issued Australian AD/FA-200/27, which will become effective on 27 August 2009.
As this AD is issued because of Australia’s obligations under Convention on International Civil Aviation, and because it is issued in response to an AD raised by the relevant State of Design, no consultation of the Australian public has taken place on this AD. 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 Initial Airworthiness in the Airworthiness and Engineering Branch, on behalf of CASA, in accordance with subsection 84A (2) of the Act.
Overview
The Civil Aviation Act 1988 was enacted to establish a legal framework for civil aviation in Australia, with a strong emphasis on safety. The Act empowers the Governor-General to create regulations that ensure the safety of air navigation, which is a critical component of maintaining national and international air safety standards. The Civil Aviation Safety Regulations 1998 further delineate specific areas of regulation, including the issuance of airworthiness directives (ADs) by the Civil Aviation Safety Authority (CASA). These ADs are crucial for ensuring the continuing airworthiness of aircraft and aeronautical products, aligning with international standards set by the Convention on International Civil Aviation. The legislative process for issuing such ADs involves careful assessment by CASA, ensuring that any directives issued comply with Australia's obligations under international agreements and are appropriate for the Australian context. The ADs are legislative instruments that do not require public consultation or a Regulatory Impact Statement, reflecting their technical nature and the international obligations that underpin them.
Scope and Application
The Civil Aviation Act 1988, complemented by the Civil Aviation Safety Regulations 1998, provides the legislative framework through which the Civil Aviation Safety Authority (CASA) can issue airworthiness directives (ADs) to ensure the safety of air navigation. Specifically, regulation 39.001 of the Civil Aviation Safety Regulations 1998 empowers CASA to issue ADs for particular types of aircraft or aeronautical products. These directives, which are legislative instruments under the Legislative Instruments Act 2003, are crucial for maintaining the continuing airworthiness of aircraft as stipulated by Annex 8 of the Convention on International Civil Aviation. The State of Design of an aircraft type holds the primary responsibility for its airworthiness and must provide necessary information to States of Registry, which in turn, like Australia through CASA, must ensure the airworthiness of aircraft within their jurisdiction. This legislative process is designed to align with international obligations and standards, ensuring that Australian aviation practices are consistent with global safety protocols. The issuance of ADs such as AD/FA-200/27, which corresponds to an AD issued by the State of Design for Fuji FA-200 model aircraft, is conducted without public consultation due to the international nature of the obligations and the specific regulatory requirements under the Convention on International Civil Aviation.
Key Provisions
The key operative sections of this legislation revolve around the Civil Aviation Act 1988 and the Civil Aviation Safety Regulations 1998, specifically section 98 and regulation 39.001. Section 98 of the Civil Aviation Act 1988 empowers the Governor-General to make regulations to ensure the safety of air navigation. Under regulation 39.001 of the Civil Aviation Safety Regulations 1998, the Civil Aviation Safety Authority (CASA) has the authority to issue airworthiness directives (ADs) for certain types of aircraft or aeronautical products. These ADs are legislative instruments and are subject to disallowance under section 46A of the Acts Interpretation Act 1901.
The obligations and requirements imposed by this Act on the parties and entities it governs are primarily focused on ensuring the continuing airworthiness of aircraft. According to Annex 8 to the Convention on International Civil Aviation, the State of Design has the primary responsibility for the continuing airworthiness of an aircraft type and must provide necessary information to the States of Registry. The State of Registry, in this case CASA as Australia’s national airworthiness authority, must then assess this information and issue an Australian AD if appropriate. This ensures that the requirements of the State of Design are adopted and enforced within Australia. In the case of the Fuji FA-200 model aircraft, Japan as the State of Design issued AD TCD-6832-2006, which CASA assessed and translated into Australian AD/FA-200/27.
There are specific offences, penalties, or civil/criminal consequences for breaches of these regulations. However, the explanatory statement does not detail specific penalties for non-compliance with the ADs. Typically, non-compliance with ADs can result in severe consequences, including the grounding of aircraft, fines, or other regulatory actions by CASA. The seriousness of the consequences depends on the severity of the non-compliance and the risk posed to public safety. While the exact penalties are not specified in this particular explanatory statement, they are generally severe enough to ensure adherence to airworthiness standards and directives.