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, the Civil Aviation Safety Authority (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 Airworthiness Limitation 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 limitation or AD to mandate the requirements of the State of Design.
In 1982 Piper Aircraft, Inc. published Service Bulletin No. 745 specifying periodic inspection of the spar of the vertical fin of the Piper PA-38-112 aircraft. In 1982 CASA’s predecessors issued AD/PA-38/7 Amdt 5 to match the requirement in Service Bulletin No. 745 Part I, II and III. In 1983 the USA Federal Aviation Administration issued Airworthiness Directive 82-27-08 specifying periodic inspection of similar areas in Piper PA-38-112 aircraft. The USA is the State of Design for this aircraft type. In 2008 CASA reviewed all ADs applicable to the Piper PA-38 aircraft, including AD/PA-38/7 Amdt 5. As a result, CASA decided to amend AD/PA-38/7 to amendment 6 to more closely match USA AD 82-27-08 (a)(1), (a)(2) and (a)(4). This AD will become effective on 18 December 2008. This AD cancels and replaces the previous issue.
As this AD is issued because of Australia’s obligations under the Convention on International Civil Aviation, and because it is issued in response to an Airworthiness Directive 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, Airframes and Structures in the Airworthiness Engineering Group, on behalf of CASA, in accordance with subsection 84A (2) of the Act.
Overview
The Civil Aviation Act 1988 was enacted to establish a regulatory framework ensuring the safety and efficiency of civil aviation within Australia. This legislation provides the foundation for the Civil Aviation Safety Regulations 1998, which further detail the requirements for airworthiness and safety standards. One of the critical tools within this regulatory framework is the issuance of airworthiness directives (ADs), which are formal and enforceable rules aimed at maintaining the continuing airworthiness of aircraft. The Civil Aviation Safety Authority (CASA) is tasked with issuing these directives under regulation 39.001 of the Civil Aviation Safety Regulations 1998, ensuring compliance with international standards set forth by the Convention on International Civil Aviation. This AD, issued in 2008, reflects Australia's commitment to international air safety standards and ensures that Australian-registered aircraft meet the necessary safety requirements aligned with those of the United States, the State of Design for the Piper PA-38-112 aircraft.
Scope and Application
The Civil Aviation Safety Regulations 1998, under the Civil Aviation Act 1988, empower the Civil Aviation Safety Authority (CASA) to issue airworthiness directives (ADs) for specific types of aircraft or aeronautical products, thereby ensuring the continuing airworthiness of aircraft within Australia. These directives are legislative instruments, subject to disallowance, and are integral to meeting Australia's international obligations under Annex 8 to the Convention on International Civil Aviation. The ADs are designed to mandate requirements for aircraft registered in Australia, particularly in response to directives issued by the State of Design, which in the case of the Piper PA-38-112 aircraft is the USA. CASA, as Australia’s national airworthiness authority, assumes the responsibility of assessing information from the State of Design and issuing corresponding Australian ADs to enforce these requirements. This process ensures that the aircraft's continuing airworthiness aligns with international safety standards, as demonstrated by the amendment of AD/PA-38/7 to amendment 6 to align with the USA’s AD 82-27-08. These directives are issued without public consultation due to their alignment with international agreements and are considered not to require a Regulatory Impact Statement.
Key Provisions
The Civil Aviation Safety Regulations 1998, under regulation 39.001, empower the Civil Aviation Safety Authority (CASA) to issue airworthiness directives (ADs) for specific types of aircraft or aeronautical products. These directives are integral to ensuring the safety and continuing airworthiness of aircraft, as outlined in Annex 8 to the Convention on International Civil Aviation. Regulation 39.001(5) further clarifies that an AD is considered a disallowable instrument under section 46A of the Acts Interpretation Act 1901, and thus qualifies as a legislative instrument according to section 6 of the Legislative Instruments Act 2003. The State of Design holds the primary responsibility for the ongoing airworthiness of an aircraft type and must provide necessary information to the appropriate States of Registry to support this responsibility. As the national airworthiness authority in Australia, CASA is tasked with evaluating this information and, if necessary, issuing corresponding Australian limitations or ADs to enforce the requirements set forth by the State of Design.
In practical terms, these obligations require CASA to closely monitor directives issued by other national aviation authorities, particularly those from the State of Design. For instance, in the case of the Piper PA-38-112 aircraft, CASA reviewed and amended AD/PA-38/7 to more closely align with the requirements set by the USA Federal Aviation Administration's Airworthiness Directive 82-27-08. This process includes a detailed assessment of any newly issued service bulletins or directives from the State of Design, such as Service Bulletin No. 745 from Piper Aircraft, Inc. in 1982, which specified periodic inspections of the spar of the vertical fin. CASA's role ensures that Australian regulations remain consistent with international standards, thereby maintaining a high level of safety across the aviation sector.
Entities governed by these regulations, primarily aircraft operators and maintenance organisations, are obligated to comply with the ADs issued by CASA. This compliance includes conducting necessary inspections, maintenance, and modifications as specified in the ADs. Failure to adhere to these directives can result in serious safety risks, as the ADs are designed to address identified hazards and prevent accidents. Additionally, the State of Registry of an individual aircraft must implement and enforce these directives to ensure that all aircraft registered within its jurisdiction meet the required safety standards.
Failure to comply with an airworthiness directive can lead to significant legal and financial consequences. Under the Civil Aviation Act 1988, non-compliance can be considered an offence, potentially resulting in civil or criminal penalties. The severity of these penalties can vary depending on the nature and extent of the breach, but they may include substantial fines and, in more serious cases, imprisonment. The exact penalties are not specified in the provided text but are typically outlined in the relevant sections of the Civil Aviation Act 1988 and associated regulations. Ensuring adherence to these directives is therefore crucial for all parties involved in the operation and maintenance of aircraft within Australia.