COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beagle B121 (Pup) Series Aeroplanes
AD/BEA 121/13 Internal Door Lock Operating Handle 9/72
Applicability: All models.
Requirement: Action in accordance with Beagle SB No. B121/23. Compliance: Within 100 hours time in service after 29 September 1972.
Overview
The Civil Aviation Regulations 1998, as amended by F2006B03577, is an Australian legislative instrument enacted to address safety concerns in civil aviation, particularly in relation to the airworthiness of aircraft. This regulation was introduced by the Australian Government to ensure that all civil aircraft operating within Australia adhere to stringent safety standards, thus protecting passengers, crew, and the general public. The regulations were enacted by the Australian Parliament, with a clear policy objective of maintaining and improving the safety of civil aviation through rigorous oversight and the enforcement of airworthiness directives.
One specific instance of this is evident in Airworthiness Directive AD/BEA 121/13, which pertains to Beagle B121 (Pup) Series Aeroplanes and mandates action concerning the internal door lock operating handle. This directive requires compliance within 100 hours of time in service after 29 September 1972, as specified in Beagle Service Bulletin No. B121/23. This directive exemplifies the Civil Aviation Regulations’ commitment to addressing and rectifying potential safety hazards through precise and timely actions.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Airworthiness Directives for Beagle B121 (Pup) Series Aeroplanes, and encompasses the AD/BEA 121/13 concerning the internal door lock operating handle. This directive applies universally to all models of the Beagle B121 series aeroplanes, ensuring that all operators and owners of these aircraft comply with the specified requirements. The mandate requires action in accordance with Beagle Service Bulletin No. B121/23, with compliance expected within 100 hours of time in service following 29 September 1972. The directive is part of the broader framework established by the Civil Aviation Safety Authority (CASA) and operates under the jurisdictional purview of the Commonwealth of Australia, thereby extending its regulatory reach across the entire nation.
While the primary focus of this directive is the enhancement of safety standards for the Beagle B121 (Pup) Series Aeroplanes, it is pertinent to note that its application is governed by the overarching Civil Aviation Regulations 1998. These regulations may be supplemented or further detailed through subordinate instruments issued by CASA, ensuring that the implementation and enforcement of the airworthiness directives are consistent and comprehensive. Any exclusions, exemptions, or thresholds pertinent to this directive are detailed within the broader regulatory framework and the specific service bulletin referenced.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39, Subpart 105, include Airworthiness Directives that govern the maintenance and operation of aircraft within Australia. One such directive, AD/BEA 121/13, pertains to the Beagle B121 (Pup) series aeroplanes. This directive mandates that all models of the Beagle B121 aeroplanes must comply with specific maintenance actions as outlined in Beagle Service Bulletin No. B121/23 concerning the internal door lock operating handle. The requirement under this directive is that any action must be taken within 100 hours of time in service after the date of 29 September 1972. This means that the compliance window for the specified maintenance action begins 100 hours after this date.
The obligations imposed by AD/BEA 121/13 are clear: aircraft operators and maintenance personnel must ensure that the internal door lock operating handle of the Beagle B121 aeroplanes is serviced or replaced as per the instructions detailed in Beagle Service Bulletin No. B121/23. Failure to adhere to these maintenance requirements can result in the aircraft not meeting the necessary airworthiness standards, potentially leading to safety issues. The compliance must be documented and verified by authorised personnel to ensure that the aircraft remains in a safe and airworthy condition.
In terms of consequences for non-compliance, AD/BEA 121/13 does not explicitly state the penalties for breach. However, general provisions under the Civil Aviation Regulations 1998 and the Civil Aviation Act 1988 apply. Non-compliance with airworthiness directives can lead to enforcement actions such as fines and potential prosecution under civil or criminal law. The severity of penalties can vary depending on the nature and extent of the breach, with potential civil penalties including fines up to several thousand Australian dollars. In more severe cases, criminal charges may be brought against individuals or companies, leading to heavier fines and possible imprisonment. It is essential for operators and maintenance personnel to adhere to these directives to avoid any legal repercussions and to ensure the safety of air travel.