COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Instruments and Automatic Pilots
AD/INST/16 King KG 102 Directional Gyro - Modification 6/75
Applicability: King KG 102 directional gyro S/Nos. P1 to P1999. Document: King SB KG 102-6.
Compliance: Before 30 September 1975.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, form a comprehensive legal framework governing civil aviation safety within the country. One particular legislative instrument, F2006B10817, addresses the critical issue of airworthiness directives related to the safety of aviation equipment, specifically targeting the King KG 102 directional gyro. This legislative instrument, introduced by the Civil Aviation Safety Authority (CASA), aims to ensure that all civil aircraft operating in Australia meet the highest safety standards by mandating modifications to the King KG 102 directional gyro for specific serial numbers to prevent potential safety hazards. The policy objective is to mitigate risks associated with the identified equipment, thereby enhancing the overall safety of civil aviation operations within Australia.
Scope and Application
The Civil Aviation Regulations 1998, as detailed in Part 39 - 107, pertains specifically to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, focusing on instruments and automatic pilots. This particular regulation, AD/INST/16, applies to King KG 102 directional gyros with serial numbers ranging from P1 to P1999, requiring compliance in accordance with King SB KG 102-6, and mandates that modifications be completed before 30 September 1975. This legislation is applicable to all aircraft operators and maintenance providers who are responsible for ensuring that their King KG 102 directional gyros meet the specified safety standards. The regulation applies across the entire Commonwealth of Australia, ensuring a uniform approach to aviation safety standards throughout the nation. There are no stated exclusions or exemptions in this directive, implying that all affected gyros must be modified irrespective of other conditions. The regulation’s scope is further extended or restricted through subordinate instruments, ensuring that any additional requirements or clarifications are communicated effectively to all relevant parties.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 107, address the modification requirements for the King KG 102 directional gyro, which applies to serial numbers P1 to P1999. According to section (6/75), compliance with these requirements must be achieved before 30 September 1975, as outlined in the document King SB KG 102-6. This legislative instrument mandates that any owner or operator of an aircraft equipped with the specified King KG 102 directional gyro must ensure that the gyro meets the outlined modification standards. The requirement to comply by the specified date is a critical directive to ensure that all affected aircraft meet safety standards and continue to be airworthy.
The obligations imposed by the Civil Aviation Regulations 1998 for the specified King KG 102 directional gyro include the necessity for aircraft owners and operators to undertake the required modifications as stipulated in the document King SB KG 102-6. This encompasses the timely completion of the modifications before the set deadline of 30 September 1975 to maintain the aircraft's airworthiness. Additionally, the regulations require that all modifications be carried out by appropriately certified personnel, ensuring that the changes are made in accordance with the specified standards and guidelines.
Failure to comply with the Civil Aviation Regulations 1998 regarding the modification of the King KG 102 directional gyro may result in serious consequences. Section 107 of the regulations outlines that non-compliance can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions may include fines, penalties, and potential grounding of the aircraft until compliance is achieved. The maximum penalties for non-compliance are not explicitly stated in the provided text, but it is understood that severe repercussions can ensue, including criminal charges for individuals or corporate entities that persistently violate these safety regulations.