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/47
Amdt 1
Periodic Testing of ATC Transponders 11/94
Applicability: All Air Traffic Control transponders.
Requirement: Perform a system test in accordance with the requirements contained in United States Federal Aviation Regulations Part 43 Appendix F. Code 2100 should be used when carrying out transponder tests.
Compliance: The compliance for the original issue of this directive was within 24 calendar months from 23 July 1992 and thereafter at either:
- intervals not exceeding 24 calendar months, or
b. intervals approved in accordance with a System of Maintenance for the aircraft pursuant to Civil Aviation Regulation 42M.
The compliance remains unchanged and this amendment becomes effective on 13 October 1994.
Note: Consideration should be given to aligning this inspection/test with that required by AD/RAD/43.
Background: This Directive was originally issued to introduce a procedure additional to the transponder self check prescribed in Civil Aviation Regulations, Schedule 5, Section 5 sub-paragraph (4)(k) and to align with the requirements of overseas Civil Aviation Regulatory Authorities. This amendment is issued to advise of a new code, compatible with Air Traffic Control requirements, to be used when testing transponder systems.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Government, were established to provide comprehensive regulations for ensuring the safety of civil aviation within Australia. One of the specific legislative instruments within this framework is the "Civil Aviation Safety Authority Schedule of Airworthiness Directives" concerning the periodic testing of Air Traffic Control (ATC) transponders. This directive, initially issued on 23 July 1992 and amended on 13 October 1994, was introduced to address the need for consistent and reliable testing procedures for ATC transponders, aligning them with international standards and enhancing overall aviation safety. The objective of this regulation is to ensure that all ATC transponders are periodically tested in accordance with United States Federal Aviation Regulations, specifically referencing Part 43 Appendix F, using the designated code 2100. This directive mandates compliance within 24-month intervals, or as approved under a System of Maintenance for the aircraft, to maintain the airworthiness and reliability of ATC transponder systems.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 107 Civil Aviation Safety Authority Schedule of Airworthiness Directives Radio Communication and Navigation Equipment AD/RAD/47 Amendment 1, concerns the periodic testing of Air Traffic Control (ATC) transponders, applicable to all such devices. This regulation applies to any ATC transponders used within the Commonwealth of Australia and mandates that these devices undergo a system test in accordance with the requirements set out in United States Federal Aviation Regulations Part 43 Appendix F. During these tests, code 2100 must be used, aligning with Air Traffic Control requirements. Compliance with these testing requirements must be achieved within 24 calendar months from the original issue date of 23 July 1992 and subsequently at intervals not exceeding 24 calendar months or as approved under a System of Maintenance for the aircraft pursuant to Civil Aviation Regulation 42M. This amendment, effective from 13 October 1994, retains the compliance requirements established previously and recommends aligning the inspection/test with other relevant directives such as AD/RAD/43 to ensure comprehensive maintenance and safety standards.
Key Provisions
The main operative sections of the Civil Aviation Regulations 1998, PART 39 - 107, specifically the Airworthiness Directive AD/RAD/47 Amendment 1, focus on the periodic testing of Air Traffic Control (ATC) transponders. According to section 11/94, this directive applies to all ATC transponders, mandating that a system test must be performed in accordance with the requirements set out in the United States Federal Aviation Regulations Part 43 Appendix F. When conducting these tests, the transponders must use Code 2100, as specified. The directive requires compliance within 24 calendar months from the original issue date, 23 July 1992, and thereafter at intervals not exceeding 24 calendar months, or as approved under a System of Maintenance for the aircraft in accordance with Civil Aviation Regulation 42M.
The obligations imposed by this Act on the parties and entities it governs include ensuring that all ATC transponders are tested regularly and in compliance with the specified requirements. This involves adhering to the testing protocols outlined in the United States Federal Aviation Regulations Part 43 Appendix F and utilising Code 2100 during the tests. The compliance timeline mandates that the initial compliance must be achieved within 24 months from 23 July 1992, with subsequent tests to be conducted at intervals not exceeding 24 months or as approved under a System of Maintenance. These obligations are critical to maintaining the airworthiness of the aircraft and ensuring the safety of air traffic operations.
In terms of breaches and the associated consequences, the Act does not explicitly detail specific offences, penalties, or civil/criminal consequences within the provided text. However, non-compliance with airworthiness directives typically results in severe regulatory and safety repercussions. Such non-compliance could lead to the grounding of aircraft, enforcement actions by the Civil Aviation Safety Authority (CASA), and potential civil or criminal liability for the operators. Given the critical nature of ATC transponders in aviation safety, failure to adhere to these requirements could result in significant penalties and sanctions under broader aviation regulations.