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 55/2 Rib in Area Adjacent to Rudder Torque Tube 8/61
Applicability: Model 95-55 with S/Nos. TC-1 to TC-137. Requirement: Action in accordance with Beechcraft SB 95-55 No. 4. Compliance: Before 1 September 1971.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, serve to regulate civil aviation operations, safety, and other related matters within Australia. One specific piece of legislation, the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, was introduced to ensure that civil aircraft are maintained and operated in a safe condition, thereby addressing the need for stringent oversight and compliance with safety standards in the aviation sector. This directive, specifically AD/BEECH 55/2 concerning the Beechcraft 55, 58 and 95-55 (Baron) Series Aeroplanes, targets the issue of rib integrity in the area adjacent to the rudder torque tube. The policy objective is to maintain the airworthiness of these aircraft by enforcing specific maintenance actions as outlined in the directive.
The legislation mandates that for model 95-55 with serial numbers TC-1 to TC-137, compliance with Beechcraft Service Bulletin 95-55 No. 4 must be achieved before 1 September 1971, ensuring that these aircraft remain safe for operation. The directive underscores the importance of adhering to manufacturer guidelines to uphold the highest standards of aviation safety, reflecting the overarching aim of the Civil Aviation Regulations to protect public safety and ensure the reliability of civil aviation activities in Australia.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, sets out the requirements for airworthiness directives under the authority of the Civil Aviation Safety Authority (CASA). The regulation concerns Beechcraft 55, 58, and 95-55 (Baron) Series Aeroplanes, with a particular focus on AD/BEECH 55/2, which pertains to a rib in the area adjacent to the rudder torque tube. This directive applies to Model 95-55 aeroplanes with serial numbers TC-1 to TC-137. The requirement outlined in this directive mandates compliance with Beechcraft Service Bulletin 95-55 No. 4, and it stipulates that any necessary action must be taken before 1 September 1971. This regulation ensures that the specified aircraft meet the necessary safety standards and are maintained in a state of airworthiness, thereby safeguarding the integrity and safety of air travel within Australian and international airspace.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, establish the requirements for airworthiness directives for various aircraft models, including the Beechcraft 55, 58 and 95-55 (Baron) series aeroplanes. In this context, AD/BEECH 55/2 pertains to the rib in the area adjacent to the rudder torque tube (paragraph 1). This directive applies to Model 95-55 with serial numbers TC-1 to TC-137 (paragraph 2). The requirement is for action to be taken in accordance with Beechcraft Service Bulletin (SB) 95-55 No. 4 (paragraph 3). Compliance with this directive must be achieved before 1 September 1971 (paragraph 4).
The obligations under this airworthiness directive involve ensuring that the specified Beechcraft 95-55 aeroplanes with the given serial numbers undergo the necessary action as outlined in Beechcraft SB 95-55 No. 4. This action aims to maintain the structural integrity and safety of the aircraft by addressing the rib in the area adjacent to the rudder torque tube. Operators and owners of the affected aircraft must ensure that the required modifications or inspections are completed in accordance with the specified service bulletin and before the stipulated compliance date.
Failure to comply with AD/BEECH 55/2 could result in significant legal and safety repercussions. The Civil Aviation Safety Authority (CASA) has the authority to enforce compliance with airworthiness directives. Non-compliance may lead to enforcement actions, which could include grounding of the aircraft until the required actions are completed, fines, or other penalties as prescribed under the Civil Aviation Act 1988. Additionally, operators may face civil liability for any accidents or incidents that result from non-compliance with airworthiness directives. The specific penalties for non-compliance are not detailed in the provided text, but they are generally in line with the regulatory framework governing aviation safety in Australia.