AD/ARTOUSTE/2 - Oil and Fuel Lines - Replacement and Support

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

Legislation au F2006B02463 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

 


Turbomeca Turbine Engines - Artouste Series

 

AD/ARTOUSTE/2 Oil and Fuel Lines - Replacement NK

and Support

 

Applicability: All Artouste 111B.

 

Document: 1. Turbomeca Service No. 79.218.0050; or

 

2. AD/TURB-T/7. Compliance: Before 30 April 1974.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Government, are a comprehensive set of rules designed to ensure the safety and efficiency of civil aviation within Australia. One of the specific amendments within this expansive regulatory framework is found in Part 39 - 106, which pertains to the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives. This particular legislative instrument, F2006B02463, addresses the critical issue of ensuring the airworthiness of aircraft engines, specifically targeting the Turbomeca Artouste Series engines. The policy objective of this directive is to mandate the replacement of oil and fuel lines to mitigate risks associated with degradation and ensure continued safe operation of affected aircraft. The enactment of this regulation by the Australian Government, through the Civil Aviation Safety Authority, underscores a commitment to maintaining stringent safety standards in civil aviation. By issuing Airworthiness Directive AD/ARTOUSTE/2, CASA aims to address the identified problem of potential failures in the oil and fuel lines of the Artouste 111B engines, which, if left unaddressed, could compromise the structural integrity and operational safety of the aircraft. The directive requires compliance by a specific date, highlighting the urgency and importance of adhering to these safety standards.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 106, apply to all entities and persons operating aircraft in Australia that are equipped with Artouste 111B turbine engines, which are part of the Turbomeca Turbine Engines - Artouste Series. These regulations mandate the replacement of oil and fuel lines on these engines, referencing Turbomeca Service No. 79.218.0050 or AD/TURB-T/7, and require compliance before 30 April 1974. The regulations are enforced by the Civil Aviation Safety Authority and have a national reach, extending to all aircraft operators within Australia's jurisdiction. The scope of these regulations includes ensuring the airworthiness of the specified engine types, with no explicit exclusions or exemptions mentioned in the provided text, though the applicability of subordinate instruments may extend or modify the application of these directives.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39, subsection 106, outlines the Civil Aviation Safety Authority’s (CASA) schedule of airworthiness directives for various aircraft components and systems. Within this framework, AD/ARTOUSTE/2 pertains to the replacement and support of oil and fuel lines for Turbomeca Artouste Series engines, particularly the Artouste 111B model (subsection 106). This airworthiness directive is applicable to all aircraft utilising the specified engine type. The directive is documented under Turbomeca Service Number 79.218.0050 or AD/TURB-T/7 and requires compliance before 30 April 1974. The obligations imposed by this airworthiness directive are clear and specific. Aircraft operators must ensure that the oil and fuel lines for the specified Turbomeca Artouste 111B engines are replaced or supported according to the directive's requirements. This involves adhering to the guidelines set out in the referenced Turbomeca Service Number 79.218.0050 or AD/TURB-T/7. Compliance must be achieved prior to the deadline of 30 April 1974, ensuring that any identified safety risks are mitigated in a timely manner. Failure to comply with these directives could result in significant safety hazards and potential non-compliance with aviation safety standards. In terms of consequences for non-compliance, the Civil Aviation Regulations 1998 do not explicitly state the penalties for breaching this airworthiness directive. However, general aviation regulations provide a framework for potential civil and criminal penalties. Non-compliance with airworthiness directives can lead to enforcement actions by CASA, which may include fines, operational restrictions, or even grounding of the aircraft. The severity of the penalties would depend on the specific circumstances and the extent of the non-compliance. In extreme cases, where non-compliance leads to an aviation incident or accident, the consequences could be more severe, including criminal charges against individuals responsible for the oversight or operation of the non-compliant aircraft.

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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.