COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Robin Aviation Series Aeroplanes
AD/ROBIN/17 Safety Harness Link 7/92
Applicability: ATL, all types.
Requirement: Action in accordance with ROBIN SA SB No.6 Rev 1.
Note: DGAC AD 89-075(A) R1 refers.
Compliance: Unless already accomplished; Within 50 hours time in service after 25 June 1992. Background: The DGAC requires modification action in order to prevent the nut of the quick-
disconnect link to unscrew.
Overview
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, include Airworthiness Directives aimed at maintaining safety standards in civil aviation. One such directive, AD/ROBIN/17, was enacted to address a specific issue with the Robin Aviation Series Aeroplanes, particularly concerning the safety harness link. The legislation was introduced to ensure the nut of the quick-disconnect link does not unscrew, which could compromise safety. This directive was enacted by the Civil Aviation Safety Authority, following the requirements set by the DGAC AD 89-075(A) R1, to ensure that all applicable aircraft meet the specified safety standards. The objective of this regulation is to mandate compliance within 50 hours of the aircraft being in service after 25 June 1992, unless the action has already been completed. This proactive measure underscores the commitment to maintaining the highest safety standards in civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, as part of the Commonwealth of Australia's legislative framework, govern a range of civil aviation activities, including the issuance of Airworthiness Directives (ADs). Specifically, PART 39 - 105 applies to all types of Robin Aviation Series aeroplanes, ensuring that these aircraft meet the necessary safety standards. AD/ROBIN/17 pertains to the requirement for a safety harness link modification to prevent the nut of the quick-disconnect link from unscrewing, an issue identified through safety concerns and referenced in DGAC AD 89-07-5(A) R1. This directive applies to all Robin Aviation Series aeroplanes and mandates compliance within 50 hours of time in service following 25 June 1992, unless the required modification has already been completed. This regulation underscores the importance of adhering to specified safety measures to maintain operational standards and ensure the safety of all personnel involved.
The Civil Aviation Regulations extend to the entire Commonwealth of Australia, enforcing a uniform standard across all states and territories. The scope of this specific directive is limited to aircraft types covered under the Robin Aviation Series, and there are no stated exclusions or exemptions. The application of these regulations is further extended and detailed through subordinate instruments, which provide additional guidance and specific procedural requirements for compliance.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes detailed provisions governing the safety and airworthiness of aircraft, including Robin Aviation series aeroplanes. One such provision is AD/ROBIN/17, which pertains to the safety harness link (section 39-105). This directive mandates that all ATL types must take action in accordance with Robin SA SB No.6 Rev 1. The directive's purpose is to ensure that the nut of the quick-disconnect link does not unscrew, which could lead to safety issues. The action is required unless it has already been completed and must be carried out within 50 hours of time in service after 25 June 1992.
Entities governed by these regulations must adhere to the requirements set out in AD/ROBIN/17. This includes ensuring that modifications are made to the safety harness link as specified in Robin SA SB No.6 Rev 1. Operators must ensure that these modifications are completed within the stipulated timeframe, which is within 50 hours of time in service after the specified date of 25 June 1992. Failure to comply with these directives could result in significant safety risks and potential non-compliance with aviation safety standards.
Failure to comply with the safety directives outlined in AD/ROBIN/17 may result in various consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce compliance and may take action against entities that do not adhere to the regulations. The specific consequences for non-compliance can vary but may include fines, enforcement actions, or even the grounding of the aircraft until the required modifications are made. The potential penalties underscore the importance of adhering to the safety directives to maintain the airworthiness of the aircraft and ensure the safety of all personnel involved.