AD/ELECT/37 Amdt 2 - JET Electronics and Technology Inc. Standby Power Supply - Modification

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, serve to regulate various aspects of civil aviation within Australia. One such regulation, included in Part 39, concerns Airworthiness Directives for electrical equipment, specifically addressing issues with standby power supplies. AD/ELECT/37 Amendment 2 pertains to the JET Electronics and Technology Inc. Standby Power Supply, with the goal of ensuring the airworthiness of certain JET PS-823 models through necessary modifications. The directive applies to all J.E.T. PS-823 models, requiring specific modifications if they have not already been completed, to be carried out within 100 hours of service following 28 February 1981. This amendment was introduced to address identified safety concerns and ensure compliance with airworthiness standards. The Civil Aviation Regulations 1998 aim to maintain high safety standards in the aviation industry, with specific focus on electrical equipment reliability and airworthiness. The JET Electronics and Technology Inc. Standby Power Supply - Modification directive exemplifies this commitment by requiring modifications to certain JET PS-823 models to rectify previously identified issues, ensuring the ongoing safety and reliability of these aircraft components. The directive reflects the policy objective of the Civil Aviation Safety Authority to proactively manage and mitigate risks associated with aviation safety, thereby protecting the public and maintaining the integrity of the national airspace.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 107, establishes the requirements for airworthiness directives concerning electrical equipment used in aviation. This regulation applies to all models of J.E.T. PS-823 standby power supplies, mandating that if a specific modification number has been marked off, no further action is required. Conversely, if the modification number has not been marked off, the modifications must be installed according to JET Service Bulletin No. SB501-1075-16F. Compliance with these directives must be achieved within 100 hours of time in service after 28 February 1981. The scope of this regulation encompasses all relevant models and their necessary modifications, ensuring that the specified electrical equipment meets safety standards set by the Civil Aviation Safety Authority. The regulation applies to entities and persons operating aircraft with the specified standby power supplies, ensuring safety and compliance within the aviation industry.

Key Provisions

The key operative sections of this legislation, specifically Part 29, section 107 of the Civil Aviation Regulations 1998, pertain to the airworthiness directives for electrical equipment, particularly those issued by the Civil Aviation Safety Authority (CASA) for JET Electronics and Technology Inc. Standby Power Supply models. The primary requirement (sections 2-4) stipulates that if the modification number listed has been marked off, no further action is necessary for the specified JET PS-823 models. However, if the applicable modification number has not been marked off, the modifications must be installed in accordance with JET Service Bulletin No. SB501-1075-16F. The compliance requirement (section 5) mandates that these modifications be completed within 100 hours of time in service after 28 February 1981. The obligations imposed by this Act are clear and specific. Operators of the listed JET PS-823 models must ensure that the required modifications are either verified as already completed or installed if they have not been completed. This involves checking the modification numbers and, if necessary, following the detailed instructions provided in JET Service Bulletin No. SB501-1075-16F. The timeframe for compliance is strictly limited to 100 hours of time in service following the specified date, underscoring the urgency and importance of adhering to these directives. Failure to comply with the directives outlined in this legislation can lead to severe consequences. While specific penalties are not detailed in the text, non-compliance with airworthiness directives is generally subject to enforcement actions by CASA. This could include fines, operational restrictions, or even grounding of the aircraft until the required modifications are made. Such consequences underscore the critical nature of ensuring compliance with airworthiness standards to maintain safety in civil aviation.