COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 55, 58 and 95-55 (Baron) Series Aeroplanes
AD/BEECH 55/3 Rudder Torque Tube 1/62
Applicability: Models 95-55 & 95-A55 with S/Nos. TC-1 to TC-310.
Requirement: Action in accordance with Beechcraft SB 95-55 No. 11 or 95-A55 No. 5. Compliance: At internals not exceeding 200 hours’ time in service after 1 September 1971.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, provide a comprehensive framework for ensuring safety in civil aviation. Part 39, which includes the Airworthiness Directives, addresses specific safety issues and mandates corrective actions for certain aircraft to ensure continued airworthiness. The 1998 Regulations were introduced to harmonise and strengthen safety standards in line with international norms, ensuring that all civil aircraft operating in Australian airspace meet stringent safety requirements. The specific legislative instrument F2006B03978 focuses on Beechcraft 55, 58, and 95-55 (Baron) series aeroplanes, providing detailed directives concerning the rudder torque tube for models 95-55 and 95-A55 with serial numbers TC-1 to TC-310. This directive aims to mandate actions in accordance with specific Beechcraft service bulletins, ensuring that these aircraft are maintained to the required safety standards.
The policy objective of this regulation is to ensure the continued airworthiness of the specified Beechcraft models by addressing potential safety issues related to the rudder torque tube. By requiring compliance within 200 hours of time in service after 1 September 1971, the regulation aims to mitigate risks associated with this component, thereby enhancing overall aviation safety. The enactment of this directive reflects the Civil Aviation Safety Authority's commitment to proactive safety management and the maintenance of high safety standards in civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, under the Civil Aviation Safety Authority’s schedule of airworthiness directives, apply to the Beechcraft 55, 58, and 95-55 (Baron) series aeroplanes, with a particular focus on models 95-55 and 95-A55 bearing serial numbers TC-1 to TC-310. This legislation mandates compliance with certain service bulletins issued by Beechcraft to ensure the airworthiness of these aircraft. The requirement pertains to actions in accordance with Beechcraft Service Bulletin 95-55 No. 11 or 95-A55 No. 5, specifically mandating that these actions be taken at intervals not exceeding 200 hours’ time in service after 1 September 1971. This regulation underscores the importance of regular maintenance and adherence to specific service bulletins to uphold safety standards within the aviation industry. The scope of the legislation is limited to the specified models and serial numbers, ensuring targeted oversight and compliance within the identified subset of the Beechcraft fleet.
Key Provisions
The Civil Aviation Regulations 1998, specifically under PART 39 - 105 (paragraphs 1/62), mandate airworthiness directives for certain Beechcraft models, including the 55, 58, and 95-55 (Baron) series aeroplanes. One of these directives, AD/BEECH 55/3, focuses on the rudder torque tube for models 95-55 and 95-A55 with serial numbers ranging from TC-1 to TC-310. This directive stipulates that affected aircraft must comply with Beechcraft Service Bulletins 95-55 No. 11 or 95-A55 No. 5. These service bulletins outline specific actions that need to be taken to ensure the airworthiness of the rudder torque tube.
The obligations imposed by AD/BEECH 55/3 on the aircraft operators and owners are clear. They must ensure that the required actions are implemented within the specified timeframe, which is at intervals not exceeding 200 hours of time in service after 1 September 1971. This means that operators and owners must adhere to the maintenance schedules and procedures detailed in the relevant Beechcraft service bulletins to maintain compliance with the Civil Aviation Regulations. Failure to do so could result in the aircraft being deemed unairworthy, leading to potential grounding and other regulatory consequences.
The Civil Aviation Regulations also detail the potential consequences for non-compliance with AD/BEECH 55/3. While the specific penalties are not detailed within this directive, general provisions under the Civil Aviation Act 1988 could apply. These may include administrative penalties for failing to comply with airworthiness directives, which could result in fines. In severe cases, where non-compliance leads to safety incidents or accidents, there could be criminal charges against the operators or owners, potentially leading to imprisonment and significant fines. Additionally, the Civil Aviation Safety Authority (CASA) has the authority to issue compliance orders, which can mandate corrective actions and impose financial penalties.
Moreover, ongoing non-compliance with airworthiness directives can lead to the suspension or revocation of an aircraft's certificate of airworthiness, effectively grounding the aircraft until the necessary actions are taken. This has significant operational and financial implications for the operators and owners. Thus, it is imperative that all affected parties understand and adhere to the requirements of AD/BEECH 55/3 to avoid any legal or safety repercussions.