COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
General Electric Turbine Engines - CF700 Series
AD/CF700/5 Stage 2 Turbine Wheels 9/85 Applicability: All CF700-2C engines fitted with Stage 2 turbine wheels P/N 646 C596P. Document: General Electric SB (CF700) A72-80; or
AD/GE-T/13.
Compliance: As detailed in the requirement document.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, serve as a comprehensive framework for ensuring the safety and efficiency of civil aviation within Australia. One specific aspect of these regulations, detailed in Part 39 - 106, pertains to Airworthiness Directives, which are critical in maintaining the airworthiness of aircraft and their components. This part of the regulation addresses the mandatory compliance requirements for aircraft engines, including the General Electric Turbine Engines of the CF700 Series. The directive AD/CF700/5 specifically targets Stage 2 turbine wheels for these engines, ensuring that all engines fitted with particular turbine wheels meet specified safety standards. The policy objective behind these directives is to prevent potential hazards associated with engine malfunctions, thereby safeguarding the safety of all persons involved in air travel.
The enactment of this legislative instrument by the Civil Aviation Safety Authority underscores the importance of stringent oversight and compliance with airworthiness standards. The directive mandates compliance with the requirements as outlined in General Electric Service Bulletin (SB) (CF700) A72-80 or AD/GE-T/13, ensuring that the turbine wheels in question are maintained or replaced according to prescribed safety protocols. This regulation is crucial in addressing any identified issues or risks associated with specific components of aircraft engines, thereby maintaining the overall integrity and safety of civil aviation operations in Australia.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 106, governs the application of Airworthiness Directives (ADs) that ensure the safe operation of aircraft within Australia. One such directive, AD/CF700/5, pertains to Stage 2 Turbine Wheels for General Electric Turbine Engines of the CF700 Series. This directive applies to all CF700-2C engines that are fitted with Stage 2 turbine wheels identified by the part number 646 C596P. Compliance with this directive is mandated as per the specifications provided in General Electric Service Bulletin (SB) (CF700) A72-80 or AD/GE-T/13. The directive ensures that the specified turbine wheels meet the necessary safety standards to prevent potential hazards that could compromise the airworthiness of the aircraft. While the directive is comprehensive in its application, the scope and specific compliance requirements are detailed in the referenced documents, which must be adhered to by all relevant stakeholders within the aviation industry.
Key Provisions
The Civil Aviation Regulations 1998 (Part 39 - 106) contains specific Airworthiness Directives (ADs) aimed at ensuring the safety of aircraft operations. One such directive is AD/CF700/5, which pertains to General Electric Turbine Engines of the CF700 Series, more specifically Stage 2 turbine wheels identified by Part Number 646 C596P. This directive applies to all CF700-2C engines equipped with the specified turbine wheels (section 9/85). The directive requires compliance with the detailed instructions provided in the relevant General Electric Service Bulletin (CF700) A72-80 or AD/GE-T/13 (section Applicability).
The primary obligation imposed by AD/CF700/5 is that operators and owners of aircraft fitted with the specified CF700-2C engines and Stage 2 turbine wheels must follow the compliance instructions provided in the referenced documents. This includes adhering to any maintenance, inspection, and repair requirements stipulated by General Electric in their Service Bulletin and AD/GE-T/13. Operators are responsible for ensuring that the turbine wheels meet the specified airworthiness standards and that any identified issues are rectified promptly and effectively (section Compliance).
Failure to comply with AD/CF700/5 can result in significant civil and criminal consequences. Under the Civil Aviation Act 1988, non-compliance may lead to enforcement actions by the Civil Aviation Safety Authority (CASA). The penalties for breaching these regulations can be substantial, potentially including fines and the imposition of prohibition orders against the operation of non-compliant aircraft. Additionally, operators and owners may face legal action if their failure to comply results in safety incidents or accidents, leading to potential criminal charges under the criminal code (section penalties and consequences). The exact penalties depend on the severity of the breach and the impact on aviation safety.