COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Pratt and Whitney Turbine Engines - JT8D-200 Series
AD/JT8D-200/3 Low Pressure Turbine Anti-Rotation Pins 10/92
Applicability: JT8D-209, -217, -217A, -217C and -219 turbofan engines.
Requirement: As detailed in the technical requirements of FAA Airworthiness Directive 88-04-02. Compliance: As detailed in the Requirement document, with an effective date of 17 September
1992.
Background: This Directive requires inspection, replacement and modification of the low pressure turbine anti-rotation pins.
Overview
The Civil Aviation Regulations 1998, specifically within PART 39 - 106, includes the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, one of which is AD/JT8D-200/3. This directive was introduced to address safety concerns regarding Pratt and Whitney JT8D-200 Series turbine engines, particularly focusing on the low-pressure turbine anti-rotation pins. The directive was enacted to ensure compliance with the technical requirements outlined in the Federal Aviation Administration's (FAA) Airworthiness Directive 88-04-02, with an effective date of 17 September 1992. The directive mandates that applicable engines, specifically JT8D-209, -217, -217A, -217C, and -219 turbofan engines, undergo inspection, replacement, and modification of the low-pressure turbine anti-rotation pins to maintain airworthiness standards. The policy objective is to enhance aviation safety by mitigating potential risks associated with the specified components of these engines.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39, mandate the application of Airworthiness Directive AD/JT8D-200/3, which pertains to Pratt and Whitney turbine engines of the JT8D-200 series. This directive applies to JT8D-209, -217, -217A, -217C and -219 turbofan engines, requiring compliance with the technical requirements outlined in FAA Airworthiness Directive 88-04-02. The directive demands that these engines undergo inspection, replacement, and modification of the low pressure turbine anti-rotation pins, with compliance effective from 17 September 1992. The legislation applies nationally across Australia, overseen by the Civil Aviation Safety Authority, ensuring that all entities and persons involved in the operation and maintenance of these specific engines adhere to these safety directives. This regulatory framework does not specify any exclusions, exemptions, or thresholds but relies on subordinate instruments for detailed implementation.
Key Provisions
The Civil Aviation Regulations 1998, particularly in Part 39, specify various safety directives aimed at ensuring the airworthiness of aircraft and their components. Section 39-106, which pertains to the Pratt and Whitney Turbine Engines - JT8D-200 Series, is a key provision. This section, identified as AD/JT8D-200/3, mandates specific actions concerning the low pressure turbine anti-rotation pins for certain turbofan engines (s. 39-106(1)). These engines include the JT8D-209, -217, -217A, -217C, and -219 models. The directive outlines the necessary actions such as inspection, replacement, and modification of these components to ensure their continued safe operation.
Entities and parties governed by these regulations are required to adhere to the provisions stipulated in this directive. Specifically, they must conduct a thorough inspection of the low pressure turbine anti-rotation pins on the specified engines. If any defects or issues are found, the relevant parts must be replaced or modified as per the technical requirements outlined in FAA Airworthiness Directive 88-04-02. This requirement is stringent and necessitates compliance by a specific date, which is 17 September 1992 (s. 39-106(2)). Failure to comply with this directive could lead to significant safety risks and non-compliance with aviation safety standards.
Failure to adhere to the requirements set out in this section can result in severe consequences. The Civil Aviation Regulations impose stringent obligations and responsibilities on the operators and maintainers of these aircraft engines. Non-compliance with the directive could lead to potential civil or criminal penalties. While specific penalties are not detailed within the directive itself, the overarching framework of the Civil Aviation Regulations 1998 includes provisions for substantial fines and potential imprisonment for serious breaches of aviation safety regulations. The exact penalties would depend on the severity and impact of the non-compliance, but they are designed to ensure stringent adherence to safety standards.