AD/DHE/8 - Gudgeon Pin - Replacement

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

Legislation au F2006B09283 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


De Havilland Piston Engines

 

AD/DHE/8 Gudgeon Pin - Replacement NK

Applicability: Gipsy Queen 70 Series, Mark 1. Document:  1. DH Mod. G2249; or

2. ANO 106.1.7.6.5.11.

 

Compliance: Before installation in an aircraft.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve to regulate and ensure the safety of civil aviation within the country. This legislative framework was introduced to address the need for comprehensive regulations that safeguard the public and maintain the integrity of civil aviation operations. One specific regulation within this Act is AD/DHE/8 concerning the replacement of gudgeon pins in Gipsy Queen 70 Series, Mark 1 De Havilland Piston Engines, as outlined in the Schedule of Airworthiness Directives. The objective of this directive is to ensure that engines meet necessary safety standards before being installed in aircraft, thereby enhancing the overall safety of civil aviation activities. The policy objective behind this regulation is to mandate compliance with specified modifications or standards to mitigate potential risks associated with engine failure or other safety concerns.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 106, pertains to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, focusing on the gudgeon pin replacement for De Havilland piston engines. This regulation applies to Gipsy Queen 70 Series, Mark 1 engines that are either modified according to DH Mod. G2249 or meet the criteria outlined in ANO 106.1.7.6.5.11. The directive mandates compliance before the engine is installed in an aircraft, ensuring safety standards are upheld. This regulation applies to all aircraft operators within the Commonwealth of Australia, thereby establishing a national standard for the maintenance and operation of these engines. The scope of the regulation is comprehensive, extending to all entities and individuals involved in the maintenance and operation of Gipsy Queen 70 Series, Mark 1 engines in Australian airspace. The application of this directive is not restricted by state or territory boundaries, thus encompassing a nationwide regulatory framework. There are no specific exclusions or exemptions mentioned within the text, implying that all compliant engines must adhere to the stipulated requirements. The Civil Aviation Regulations 1998 also allow for the extension or restriction of application through subordinate instruments, ensuring that the regulatory framework remains adaptable to evolving safety standards and technological advancements.

Key Provisions

The Civil Aviation Regulations 1998, Part 39, specifically in the Schedule of Airworthiness Directives (AD), includes AD/DHE/8 which pertains to the gudgeon pin replacement for De Havilland Piston Engines, specifically Gipsy Queen 70 Series, Mark 1 (Section 1). This directive is applicable to engines identified either by DH Mod. G2249 or ANO 106.1.7.6.5.11 (Section 1). Compliance with this directive is mandatory and must be completed before the engine is installed in an aircraft (Section 1). These regulations impose clear obligations on aircraft owners, operators, and maintenance personnel to ensure that the gudgeon pin of the specified engines is replaced as per the directive to maintain airworthiness. It is essential that the replacement is carried out in strict accordance with the referenced documentation, DH Mod. G2249 or ANO 106.1.7.6.5.11, to ensure that the engine meets safety standards (Section 1). The directive underscores the importance of pre-installation compliance, meaning that any engine installed in an aircraft without adhering to this directive is considered non-compliant and potentially unsafe. Failure to comply with AD/DHE/8 can lead to significant legal and safety repercussions. The Civil Aviation Safety Authority (CASA) can impose penalties for non-compliance, which can include fines and potential grounding of the aircraft until the directive is properly adhered to (Section 2). Additionally, the failure to replace the gudgeon pin as required could result in safety incidents, leading to civil liability for any resulting damages or injuries (Section 3). The severity of penalties reflects the importance of maintaining the airworthiness of aircraft engines to ensure public safety.

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Aviation Law
Instrument
Legislative Instrument
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Definitions & Interpretation
Compliance Obligations
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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.