COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
De Havilland Piston Engines
AD/DHE/5 Sun Gear Distance Piece - Modification NK
Applicability: Gipsy Queen 70 series modified to Mod. G1213. Document: 1. DH Mod. G1329; or
2. ANO 106.1.7.6.5.6.
Compliance: Before installation in an aircraft.
Overview
The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority, was enacted to establish a comprehensive regulatory framework for civil aviation safety in Australia. Among its many provisions, Part 39 addresses airworthiness directives which are critical for maintaining the safety and airworthiness of aircraft. The specific legislative instrument F2006B09280, concerning the modification of Sun Gear Distance Pieces in De Havilland Piston Engines of the Gipsy Queen 70 series modified to Mod. G1213, was introduced to address a particular safety concern identified with these engines. The directive aims to ensure compliance with safety standards before the engines are installed in aircraft, thereby contributing to the overarching policy objective of maintaining high safety standards in civil aviation. The legislative instrument was enacted by the relevant authority within the Australian government to ensure adherence to these safety protocols.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 106 concerning Airworthiness Directives, sets out stringent requirements for ensuring the safety and airworthiness of aircraft operating in Australian airspace. This includes the detailed Airworthiness Directive AD/DHE/5 which pertains to Sun Gear Distance Piece modifications on De Havilland Gipsy Queen 70 series engines, particularly those modified to Mod. G1213. The directive applies to any person or entity involved in the maintenance, modification, or operation of such aircraft engines, ensuring compliance with the specified standards before the engine is installed in an aircraft. The directive applies nationally, under the jurisdiction of the Civil Aviation Safety Authority, and it is applicable regardless of where the aircraft is registered or operated within Australia.
The scope of AD/DHE/5 is precise, focusing solely on engines that meet the described modifications and specifications, such as those listed as DH Mod. G1329 or referenced in ANO 106.1.7.6.5.6. The directive does not explicitly outline exclusions or exemptions but requires compliance with the specified modifications to maintain airworthiness. The directive's application can be extended or clarified through subordinate instruments issued by the Civil Aviation Safety Authority, ensuring that all relevant parties are aware of their obligations and the necessary compliance steps.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 106, includes a series of airworthiness directives to ensure the safety and compliance of various aircraft components. One such directive, AD/DHE/5, addresses a modification to the sun gear distance piece for De Havilland piston engines, particularly for Gipsy Queen 70 series engines modified to Mod. G1213 (section 1). This directive requires that the sun gear distance piece be modified in accordance with either document DH Mod. G1329 or ANO 106.1.7.6.5.6 before it can be installed in an aircraft (section 2).
Entities governed by these regulations must adhere to the specified modifications to ensure the airworthiness of the engines. Specifically, they must ensure that any Gipsy Queen 70 series engine modified to Mod. G1213 has its sun gear distance piece modified as per the directive before it is installed in an aircraft. This requirement is crucial for maintaining the safety standards mandated by the Civil Aviation Safety Authority (CASA).
Failure to comply with the provisions of these airworthiness directives can result in serious consequences. CASA has the authority to enforce compliance, and non-compliance may lead to penalties. Although the specific penalties are not detailed in the text, the general expectation is that non-compliance could result in fines, operational restrictions, or even the grounding of aircraft until the required modifications are made. The overarching intent is to ensure that all aircraft operate within the safety standards set by the regulatory body to protect public safety and maintain the integrity of the aviation industry.