AD/BEECH 55/50 Amdt 2 - Engine Mount Truss Tubes

Overview

The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority, aim to ensure the safety of air navigation services across Australia. This legislative instrument was enacted to address gaps in the regulation of civil aviation, providing a comprehensive framework to maintain and enhance safety standards. The regulation is specifically concerned with ensuring that aircraft meet certain safety directives, as outlined in the Act. For instance, AD/BEECH 55/50 Amendment 2 pertains to the engine mount truss tubes of specific Beechcraft 55, 58, and 95-55 (Baron) Series Aeroplanes, requiring action in accordance with Beechcraft Service Instruction No. 0903, Revision 11. The objective is to ensure compliance with the Federal Aviation Administration’s Airworthiness Directive No. 77-13-08, thereby maintaining the structural integrity and operational safety of these aircraft.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to the aviation industry and governs the airworthiness directives concerning Beechcraft 55, 58, and 95-55 (Baron) series aeroplanes. This legislative instrument mandates the action required for engine mount truss tubes on certain models and serial numbers, directing adherence to the procedures outlined in Beechcraft Service Information No. 0903, Revision 11. The directive applies to all models 58P and 58PA with serial numbers TJ-2 to TJ-117, and all models 58TC and 58TCA with serial numbers TK-1 to TK-58, ensuring that these aircraft meet the specified safety standards. The application of these regulations is enforced by the Civil Aviation Safety Authority and extends nationally, with compliance monitored and enforced through the stipulated requirement documents. While the regulations are comprehensive, they do not explicitly state any exclusions or exemptions within the scope of this particular directive. The effectiveness of the regulations may be further extended or specified through subordinate instruments, ensuring that any additional measures or clarifications are implemented to maintain airworthiness standards.

Key Provisions

The Civil Aviation Regulations 1998, specifically in Part 39 - 105, establish the requirements for airworthiness directives concerning certain types of aircraft. For instance, AD/BEECH 55/50 Amendment 2 (section 10/78) pertains to the engine mount truss tubes of Beechcraft 55, 58 and 95-55 (Baron) series aeroplanes. The directive applies to specific models and serial numbers of these aircraft (section 10/78). The requirement is that the action must be in accordance with Beechcraft Service Information (SI) Number 0903, Revision 11, with a reference to the Federal Aviation Administration (FAA) AD No. 77-13-08 (section 10/78). The entities governed by this airworthiness directive are primarily the operators and owners of the specified Beechcraft aeroplanes. Their obligations include ensuring that the engine mount truss tubes are modified or inspected as per the requirements outlined in the directive. Compliance with the directive involves following the procedures detailed in the Requirement Document, which refers to the aforementioned Beechcraft SI No. 0903, Rev. 11, and FAA AD No. 77-13-08. Failure to comply with these airworthiness directives could lead to serious safety issues, potentially rendering the aircraft non-airworthy. The Civil Aviation Regulations 1998 impose strict obligations on aircraft operators and owners to adhere to airworthiness directives. These obligations are not only legal but also crucial for ensuring the safety of air travel. Operators and owners must ensure that the specified modifications or inspections are carried out in a timely and effective manner. Non-compliance with these directives could result in severe consequences, including potential grounding of the aircraft and legal penalties. The directive explicitly refers to the compliance method through the Requirement Document and the related service information and FAA directive. Should an operator or owner fail to comply with the airworthiness directive AD/BEECH 55/50 Amendment 2, there could be serious repercussions. While the Civil Aviation Regulations 1998 do not specify maximum penalties within this particular directive, non-compliance with airworthiness directives in general can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). These actions could include fines, legal proceedings, and possibly the suspension or revocation of the aircraft's operating certificate. The primary goal of these measures is to ensure that all regulated aircraft maintain the highest safety standards.