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 23/29
Amdt 2
Wing Main Spar Corrosion 12/86
Applicability: All 19, 23 and 24 series.
Requirement: Action in accordance with Beechcraft SI No. 0824-035 Rev. II.
Compliance: Prior to the issue of the next Maintenance Release after 31 December 1986 and thereafter at intervals not exceeding 12 months.
Background: A history of Major Defect Reports has warranted an increase in the periodicity of this Directive to that originally called up by Beech.
Overview
The Civil Aviation Regulations 1998, as amended, represent a comprehensive regulatory framework governing civil aviation in Australia. Enacted by the Parliament of Australia, these regulations address various aspects of aviation safety, including airworthiness standards and maintenance directives. One such directive, AD/BEECH 23/29 Amendment 2, pertains to the Beechcraft 19, 23, and 24 series aeroplanes and specifically targets the issue of wing main spar corrosion. This directive was introduced to mitigate safety risks associated with identified major defect reports, mandating compliance with Beechcraft Service Instruction No. 0824-035 Rev. II. The overarching policy objective is to ensure the continued airworthiness of these aircraft, thereby safeguarding public safety and maintaining high standards within the aviation industry.
The Civil Aviation Safety Authority, through the schedule of airworthiness directives, aims to enforce these safety measures rigorously. For the Beechcraft 19, 23, and 24 series aeroplanes, the requirement under this directive necessitates action before the issue of the next Maintenance Release following 31 December 1986, and subsequently at intervals not exceeding 12 months. This directive underscores the authority’s commitment to proactive safety management, ensuring that all applicable aircraft are maintained to the highest safety standards to prevent potential catastrophic failures.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates the application of Airworthiness Directives for aircraft within the Commonwealth of Australia. These regulations apply to all entities and persons operating the Beechcraft 19, 23, and 24 series aeroplanes within Australia, ensuring compliance with the prescribed safety standards set forth by the Civil Aviation Safety Authority. The directive targets the structural integrity of the wing main spar by addressing corrosion issues, necessitating action in accordance with Beechcraft Service Information No. 0824-035 Rev. II. Compliance with these regulations is mandatory, requiring operators to address the specified defect before the issuance of the next Maintenance Release after 31 December 1986, and subsequently at intervals not exceeding 12 months. This directive underscores the importance of periodic inspections and maintenance to uphold airworthiness standards and ensure the safety of the aircraft in operation.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, address the safety standards and directives for certain aircraft models. One such directive, AD/BEECH 23/29 Amendment 2, pertains to the Beechcraft 19, 23, and 24 series aeroplanes and concerns corrosion in the wing main spar. This directive mandates that all aircraft of these series must comply with the requirements set out in Beechcraft Service Instruction No. 0824-035, Revision II. Compliance with this directive is mandatory and must be achieved before the issue of the next Maintenance Release following 31 December 1986 and subsequently every 12 months.
The Act imposes several obligations on the parties involved, including aircraft operators, maintenance personnel, and other stakeholders. Operators of Beechcraft 19, 23, and 24 series aeroplanes must ensure that their aircraft are inspected and maintained in accordance with the specified Beechcraft Service Instruction. This includes conducting thorough checks for any signs of corrosion in the wing main spar, as well as implementing any necessary repairs or replacements as outlined in the service instruction. Maintenance personnel are responsible for carrying out these inspections and repairs to the required standard.
Failure to comply with the provisions of this directive could result in serious safety implications, given the critical role of the wing main spar in the structural integrity of the aircraft. The Civil Aviation Regulations 1998 impose civil and potentially criminal penalties for non-compliance with safety directives. Civil penalties can include fines, while criminal penalties may involve imprisonment, reflecting the seriousness with which the regulations treat breaches of safety standards. The exact penalties depend on the nature and severity of the breach, but the potential consequences underscore the importance of adhering to the specified requirements.