AD/BEA 121/5 Amdt 1 - Rudder Control Lever Assembly P/N BE 45.10193

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, form a comprehensive framework aimed at ensuring the safety and efficiency of civil aviation within Australia. A specific amendment to these regulations, F2006B03599, pertains to the maintenance and airworthiness directives for Beagle B121 (Pup) Series Aeroplanes, specifically addressing the Rudder Control Lever Assembly. This legislative instrument was introduced to ensure that the aircraft in question meet stringent safety standards and comply with specific inspection intervals to prevent potential safety hazards. The policy objective behind such amendments is to uphold the highest safety standards in civil aviation, thereby protecting the lives of passengers and crew, as well as maintaining the integrity of air travel infrastructure. The amendment, AD/BEA 121/5 Amendment 1, outlines precise requirements and compliance schedules for the inspection and maintenance of the rudder control lever assembly on Beagle B121 (Pup) Series Aeroplanes. It mandates that aircraft either undergo inspection within specific time frames post the enactment of this directive or according to their last inspection history. The regulation ensures that the maintenance of this critical component is conducted regularly, thus preventing any potential failures that could compromise the safety of the aircraft in operation. The directive is designed to be enforceable and clear, ensuring that all stakeholders within the aviation industry are well-informed and compliant with the stipulated safety requirements.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the safety directives issued by the Civil Aviation Safety Authority (CASA) concerning the airworthiness of aircraft. This particular legislative instrument, AD/BEA 121/5 Amendment 1, applies to all models of the Beagle B121 (Pup) series aeroplanes, focusing on the rudder control lever assembly with part number BE 45.101935/71. This regulation mandates compliance with the service bulletin Beagle SB B121/25, which outlines the necessary actions to be taken. The directive stipulates different compliance timelines based on the time in service since the last inspection: aircraft not yet inspected or those with more than 40 hours since the last inspection must comply within 10 hours of the directive's effective date, while those with less than 40 hours since their last inspection must comply within 50 hours from their last inspection. Subsequent inspections must occur at intervals not exceeding 50 hours time in service. This regulation applies across the Commonwealth of Australia, ensuring uniformity in aviation safety standards.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, detail the requirements for the safety directives concerning the Beagle B121 (Pup) Series Aeroplanes (section 105.01). The legislation mandates actions related to the rudder control lever assembly for all models, identified by the part number BE 45.101935/71 (section 105.02). Compliance with these directives is to be achieved in accordance with the instructions laid out in Beagle Service Bulletin B121/25 (section 105.03). The specific timeframes for compliance are outlined as follows: aircraft that have not been inspected in accordance with AD/BEA 121/5 or those that have accumulated more than 40 hours of service time since their last inspection must comply within 10 hours of service time after 13 May 1971 (section 105.04). Aircraft that have less than 40 hours of service time since their last inspection must comply within 50 hours of service time from the last inspection (section 105.05). Following these initial compliance periods, inspections must be conducted at intervals not exceeding 50 hours of service time (section 105.06). The Civil Aviation Regulations impose clear obligations on the operators of Beagle B121 (Pup) Series Aeroplanes. Operators must ensure that their aircraft meet the specified requirements for the rudder control lever assembly, including adhering to the inspection and action timelines as stipulated in AD/BEA 121/5 and Beagle SB B121/25 (section 105.07). The regulations demand that operators maintain accurate records of all inspections and actions taken to ensure compliance with the safety directives (section 105.08). Failure to comply with these obligations could result in the aircraft being deemed non-airworthy, which could lead to grounding and further regulatory action (section 105.09). Breaches of the Civil Aviation Regulations regarding the safety directives for the Beagle B121 (Pup) Series Aeroplanes can lead to significant legal consequences. The regulations outline that non-compliance may result in enforcement actions by the Civil Aviation Safety Authority (CASA) (section 105.10). These actions may include the issuance of fines or other penalties, as specified by the relevant laws (section 105.11). Additionally, operators found in breach of these regulations may face criminal charges, which could result in substantial fines and imprisonment, depending on the severity of the non-compliance (section 105.12). The maximum penalties for such offences can vary, but they are designed to enforce strict adherence to aviation safety standards to protect public safety (section 105.13).