COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 19, 23 and 24 Series Aeroplanes
AD/BEECH 23/14
Amdt 2
Front Fuselage Wing Attachment 3/80
Applicability: All models with S/Nos. referenced in Beechcraft SI No. 0042-031, Rev. 2. Requirement: Action in accordance with Beechcraft SI No. 0042-031. Rev. 2.
Compliance: As per Requirement Document.
Overview
The Civil Aviation Regulations 1998, as amended, form a comprehensive set of rules and directives governing the safety and operation of civil aircraft within Australia. One particular legislative instrument, F2006B03732, addresses airworthiness directives for specific aircraft models, including the Beechcraft 19, 23, and 24 series aeroplanes. Enacted by the Australian Government, this regulation was introduced to ensure that all civil aircraft meet specific safety standards and operational requirements. The overarching policy objective is to enhance aviation safety by requiring compliance with detailed maintenance and operational protocols, thereby mitigating the risk of in-flight incidents. This legislation is administered by the Civil Aviation Safety Authority (CASA), which is tasked with enforcing these regulations to protect the public and ensure the highest standards of aviation safety.
Scope and Application
The Civil Aviation Regulations 1998, as amended, and specifically PART 39 - 105, establish the regulatory framework for airworthiness directives under the authority of the Civil Aviation Safety Authority (CASA). This particular legislative instrument pertains to Beechcraft 19, 23 and 24 series aeroplanes, with the aim of ensuring their continued airworthiness through specific maintenance and structural requirements. The directive applies to all models of these aircraft with serial numbers as referenced in Beechcraft Service Information (SI) No. 0042-031, Rev. 2. The regulation mandates compliance with the actions detailed in the aforementioned Beechcraft SI, ensuring that the specified modifications and inspections are performed according to the requirement document. The application of this legislation is national in scope, affecting all operators and owners of the specified Beechcraft models within the Commonwealth of Australia. The legislation does not explicitly state exclusions or exemptions, implying that all applicable aircraft must adhere to the directives without exception. The scope of this legislative instrument may be extended or further defined through subordinate instruments issued by CASA.
Key Provisions
The Civil Aviation Regulations 1998 (Regulations) under Part 39 - 105, specifically AD/BEECH 23/14 Amendment 2, pertains to the front fuselage wing attachment of Beechcraft 19, 23 and 24 series aeroplanes. This directive applies to all models with serial numbers referenced in Beechcraft Service Information (SI) No. 0042-031, Revision 2 (Section 1). The main requirement is that any actions taken must adhere to the guidance provided in the aforementioned SI No. 0042-031, Revision 2. Compliance with this directive involves following the instructions detailed in the requirement document, ensuring that the structural integrity of the front fuselage wing attachment is maintained to meet safety standards.
The obligations imposed by this directive on the relevant parties include ensuring that the aircraft maintenance and inspection activities are carried out strictly in accordance with the specifications laid out in SI No. 0042-031, Revision 2. This involves not only the initial inspection and any necessary repairs but also maintaining comprehensive records of all actions taken. The directive necessitates that any identified issues are resolved in a timely manner, and that all work is performed by qualified personnel who are certified to carry out such tasks. This ensures that the safety and airworthiness of the aircraft are upheld throughout the operation of the aeroplanes.
Failure to comply with the provisions set forth in AD/BEECH 23/14 Amendment 2 may result in significant consequences. Civil and criminal penalties could be imposed for non-compliance. The severity of these penalties can vary depending on the nature and extent of the breach, but they are intended to enforce adherence to the safety directives established by the Civil Aviation Regulations. The potential penalties underscore the importance of strict compliance with the outlined safety requirements to avoid legal repercussions.