AD/RAD/28 - Garrett Rescue 88A Crash Locator Beacon

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B06489 Not in force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Radio Communication and Navigation Equipment

 

AD/RAD/28 Garrett Rescue 88A Crash Locator Beacon 2/76

Applicability: All Rescue 88A CLB installations in which the remote switch option is fitted.

 

Requirement: Disconnect, insulate and tie back the remote control plug from the beacon and install a protective cap over the beacon socket.

 

Compliance: Within 10 hour time in service after 14 January 1976.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, play a crucial role in ensuring the safety and efficiency of the country's aviation industry. Among these regulations, Part 39 – 107, specifically Airworthiness Directives concerning radio communication and navigation equipment, addresses the safety issues related to the Garrett Rescue 88A Crash Locator Beacon. This legislation was introduced to mitigate the risk of accidental activation of the beacon, which could potentially compromise flight safety by interfering with critical radio communication and navigation systems. The directive mandates the disconnection, insulation, and secure fastening of the remote control plug from the beacon, along with the installation of a protective cap over the beacon socket, to prevent unintended beacon activation. The Civil Aviation Safety Authority oversees the compliance with this directive, ensuring that all applicable installations adhere to the specified safety measures within a stipulated timeframe.

Scope and Application

The Civil Aviation Regulations 1998, as amended, apply to all entities and individuals involved in civil aviation operations within Australia. Specifically, Part 39 - 107, which concerns airworthiness directives, mandates the implementation of safety measures to ensure the reliability and safety of aircraft and their equipment. In this context, AD/RAD/28 pertains to the Garrett Rescue 88A Crash Locator Beacon and applies to all installations of this specific model that include a remote switch option. The requirement outlined in this directive mandates the disconnection, insulation, and securing of the remote control plug from the beacon, along with the installation of a protective cap over the beacon socket. Compliance with this directive must be achieved within 10 hours of the beacon being in service after 14 January 1976. The directive is enforceable across the entirety of Australian territory, reflecting the national scope of the Civil Aviation Regulations 1998. While the primary focus is on ensuring the safety of aviation operations, the Act allows for some flexibility through subordinate instruments that may extend or restrict the application of these regulations in certain circumstances.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39, Section 107, mandates the application of Airworthiness Directives (AD) for the maintenance and operation of aircraft in Australia. Section 107, pertaining to AD/RAD/28, focuses on the Garrett Rescue 88A Crash Locator Beacon (CLB). The directive applies to all installations of the Rescue 88A CLB that include the remote switch option (Section 2/76). The primary requirement outlined in this directive is to disconnect, insulate, and tie back the remote control plug from the beacon, and to install a protective cap over the beacon socket (Section 2/76). Compliance with these requirements must be achieved within 10 hours of time in service after 14 January 1976. Operators of aircraft equipped with the Garrett Rescue 88A CLB with a remote switch option must ensure adherence to these safety measures. This includes taking the necessary steps to disconnect and insulate the remote control plug and installing a protective cap over the beacon socket to prevent any accidental activation or interference that could compromise the safety of the aircraft and its occupants (Section 2/76). The directive underscores the importance of timely compliance, as operators must complete these actions within 10 hours of the specified date to ensure that the aircraft remains airworthy. Failure to comply with the requirements of AD/RAD/28 can have serious implications. Section 2/76 stipulates that the directive is enforceable, and non-compliance could lead to significant safety risks. The Civil Aviation Safety Authority (CASA) has the authority to enforce these directives, and failure to adhere to them could result in penalties or other enforcement actions. Ensuring compliance is not only a legal obligation but also a critical measure to maintain the safety standards required by the Civil Aviation Regulations 1998. In terms of penalties and consequences, Section 2/76 of AD/RAD/28 does not explicitly state the maximum penalties for non-compliance. However, under the broader framework of the Civil Aviation Regulations 1998, violations of airworthiness directives can lead to substantial fines and potential criminal charges. The severity of the penalties can vary depending on the nature and impact of the non-compliance, with serious infractions potentially leading to significant financial penalties and other enforcement actions by CASA. Operators must, therefore, take the directive seriously and ensure full compliance to avoid any adverse legal or safety consequences.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.