COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Pratt and Whitney Turbine Engines - JT8D Series
AD/JT8D/8 Second Stage Fan Blade Pin Rivets 7/76
Applicability: All JT8D-9, -11, -15 and -17 engines containing second stage fan blade pin P/N 520456, rivet P/N 520457 and bushing P/N 520458.
Document: 1. FAA AD 76-12-06 : Amendment 39-2639; or
2. AD/PW-T/36.
Compliance: As detailed in the Requirement Document.
Overview
The Civil Aviation Regulations 1998, specifically Part 39, is a critical piece of Australian legislation designed to maintain the highest standards of safety within the civil aviation sector. Enacted in 1998, this regulation was introduced to address the need for a comprehensive and authoritative framework governing civil aviation operations, ensuring that all aspects of aircraft maintenance, operations, and personnel are held to stringent safety and compliance standards. The regulation is overseen by the Civil Aviation Safety Authority (CASA), with the overarching policy objective being to safeguard the public by ensuring that civil aviation activities are conducted in a manner that minimises risk and promotes safety. The policy aims to achieve this through the establishment of mandatory safety directives, such as those pertaining to specific aircraft components like the Pratt and Whitney Turbine Engines - JT8D Series, as detailed in the Airworthiness Directives Schedule.
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 Pratt and Whitney turbine engines of the JT8D series. This legislation applies to all JT8D-9, -11, -15, and -17 engines that contain specific components, namely the second stage fan blade pin part number 520456, rivet part number 520457, and bushing part number 520458. The regulation mandates compliance with the detailed requirements set forth in either FAA AD 76-12-06, as amended by Amendment 39-2639, or AD/PW-T/36, ensuring that these components meet specified airworthiness standards. The reach of this regulation is nationwide, as it is a Commonwealth law enforced by the Civil Aviation Safety Authority. There are no stated exclusions or exemptions within the text, implying that all affected engines must comply with the directives unless otherwise specified through subordinate instruments.
Key Provisions
The main operative sections of the Civil Aviation Regulations 1998 (Part 39, Section 106) focus on the Pratt and Whitney Turbine Engines, specifically the JT8D Series, and provide directives to ensure airworthiness standards are met. Section 106 AD/JT8D/8 outlines the requirements for second stage fan blade pin rivets on JT8D-9, -11, -15, and -17 engines. These engines must contain specific parts: second stage fan blade pin P/N 520456, rivet P/N 520457, and bushing P/N 520458. The compliance is guided by FAA AD 76-12-06: Amendment 39-2639 or AD/PW-T/36. These directives are integral for maintaining the structural integrity and safety of the aircraft engines.
The obligations and requirements imposed by this Act include ensuring that the specified Pratt and Whitney engines are fitted with the correct parts and meet the standards outlined in the referenced documents. Operators and owners of these engines must verify that the components are present and in good condition, and they must adhere to the maintenance and inspection protocols as detailed in the FAA AD 76-12-06 and AD/PW-T/36. Failure to comply with these directives could result in the engines being deemed non-airworthy, potentially grounding the aircraft until the necessary actions are taken.
In terms of civil and criminal consequences, the Civil Aviation Safety Authority (CASA) has the authority to enforce compliance with these airworthiness directives. Non-compliance can lead to significant penalties, including fines and potential criminal charges. The specific maximum penalties for breaches are not detailed within the referenced sections but are governed by broader civil aviation laws. Operators found in breach may face substantial financial penalties, and in severe cases, criminal prosecution could result, leading to imprisonment for those found responsible for non-compliance.
It is crucial for all parties governed by these regulations to understand and implement the required directives to avoid legal repercussions and ensure the safety of the aircraft and its passengers. The directives are designed to prevent mechanical failures that could result from the use of incorrect or substandard components, thereby maintaining the highest safety standards in civil aviation.