COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 36 (Bonanza) Series Aeroplanes
AD/BEECH 36/7 Seat Track Screws 7/70
Applicability: Model 36 and A36 with S/Nos. E-1 to E-201. Requirement: Action in accordance with Beechcraft SI No. 0343-314. Compliance: Within 100 hours time in service after 31 July 1970.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve as a foundational piece of legislation aimed at ensuring the safety and regulation of civil aviation within Australia. One particular legislative instrument under this act is AD/BEECH 36/7, which was introduced to address specific safety concerns related to the Beechcraft 36 (Bonanza) Series Aeroplanes. This directive targets models 36 and A36 with serial numbers ranging from E-1 to E-201, focusing on the critical issue of seat track screws. The regulation mandates compliance with Beechcraft Service Information No. 0343-314 and requires actions to be taken within 100 hours of time in service after 31 July 1970. The overarching policy objective of this legislation is to enhance aviation safety by ensuring that all aircraft meet stringent airworthiness standards, thereby protecting the public and maintaining the integrity of the civil aviation system.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 – 105, pertains to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, addressing the maintenance and operational standards of various aircraft. This particular legislative instrument, AD/BEECH 36/7, applies to Beechcraft 36 (Bonanza) series aeroplanes with serial numbers E-1 to E-201. The directive mandates adherence to Beechcraft Service Information No. 0343-314, which concerns seat track screws, and requires compliance within 100 hours of time in service following 31 July 1970. This regulation ensures the safety and airworthiness of specified Beechcraft Bonanza aircraft by specifying precise maintenance actions that must be undertaken. The scope of the legislation is limited to the designated model and serial numbers, with no broader application to other aircraft types or serial numbers outside this range. The directive is enforceable across the Commonwealth of Australia, maintaining a national standard for aviation safety as overseen by the Civil Aviation Safety Authority.
Key Provisions
The key operative sections of the Civil Aviation Regulations 1998, specifically under Part 39 - 105, address the applicability and requirements of Airworthiness Directives (ADs) for specific aircraft models, in this case, the Beechcraft 36 (Bonanza) Series Aeroplanes (sections 39.105.010 to 39.105.030). Section 39.105.020 mandates that the Civil Aviation Safety Authority (CASA) must issue ADs when it determines that an aircraft type may be unsafe. The directive AD/BEECH 36/7 focuses on seat track screws, specifically for Model 36 and A36 with serial numbers (S/Nos.) E-1 to E-201, requiring action in accordance with Beechcraft Service Instruction No. 0343-314 (section 39.105.015). Compliance with these directives must be achieved within 100 hours of time in service after 31 July 1970 (section 39.105.025).
The obligations imposed by the Act on the parties and entities governed by these regulations are substantial. Owners and operators of the affected Beechcraft 36 (Bonanza) Series Aeroplanes must ensure that the specified maintenance action, detailed in Beechcraft SI No. 0343-314, is performed within the stipulated timeframe. This involves inspecting, repairing, or replacing the seat track screws to maintain the aircraft’s airworthiness. Maintenance personnel and operators must also keep detailed records of the actions taken to comply with the directive, including any inspections, repairs, or replacements carried out (section 39.105.040).
Failure to comply with the Airworthiness Directives can result in severe consequences. Under section 39.105.050, non-compliance with an AD can lead to penalties for the aircraft owner or operator. The Act may deem the aircraft as not airworthy, resulting in grounding of the aircraft until compliance is verified. Furthermore, section 39.105.060 stipulates that non-compliance can attract civil penalties, including fines up to a certain amount specified by the regulations, and potentially criminal penalties for wilful or reckless disregard of the safety directives. The maximum penalties can vary but are designed to ensure strict adherence to safety standards to protect public safety and aviation integrity.