COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Pratt and Whitney Turbine Engines - JT9D Series
AD/JT9D/15 High Pressure Turbine Airseal 12/86
TX
Applicability: JT9D-7R4D, E models.
Requirement: Carry out the requirements of Pratt and Whitney ASB JT9D-7R4-72-318, Paragraph 2 "Accomplishment Instructions".
Compliance: According to a program agreed to by the Secretary. Effective: 1 December 1986.
Background: This Directive has been issued to require compliance with the Accomplishment Instructions of P.W.A. A.S.B. JT9D-7R4-72-318. The A.S.B. details inspection and modification of the high pressure turbine to preclude cracking of the stage 1-2 airseal.
Overview
The Civil Aviation Regulations 1998, specifically within Part 39, establish a framework to ensure the safety and reliability of civil aviation in Australia. One of the key components of this framework is the issuance of Airworthiness Directives (ADs), which are legally binding requirements that address safety issues in aircraft and engine operation. The particular Airworthiness Directive AD/JT9D/15, introduced in 1986, targets Pratt and Whitney JT9D Series turbine engines, specifically models JT9D-7R4D, E. This directive was enacted by the Civil Aviation Safety Authority (CASA) to address the problem of potential cracking in the high-pressure turbine airseal of these engines, thereby aiming to maintain the highest safety standards in civil aviation. The directive requires compliance with specific instructions outlined in Pratt and Whitney's ASB JT9D-7R4-72-318, Paragraph 2, and mandates an inspection and modification program to prevent such failures, ensuring the continued airworthiness of the affected aircraft.
Scope and Application
The Civil Aviation Regulations 1998, specifically PART 39 - 106, which governs the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, applies to Pratt and Whitney JT9D series turbine engines, particularly models JT9D-7R4D, E. This regulation mandates adherence to the Accomplishment Instructions outlined in Pratt and Whitney ASB JT9D-7R4-72-318, focusing on the inspection and modification of the high-pressure turbine to prevent stage 1-2 airseal cracking. The scope of this legislation is aimed at ensuring the safety and airworthiness of these specific turbine engine models. The Act applies to entities that operate these engines, including airlines and maintenance providers, and requires compliance with the directive as per a program agreed upon by the Secretary. The geographic reach of this regulation is national, covering all operations within Australia, and it does not specify exclusions, exemptions, or thresholds. The application of this regulation can be further defined or extended through subordinate instruments issued by CASA.
Key Provisions
The key operative sections of the Civil Aviation Regulations 1998, Part 39, specifically the Schedule of Airworthiness Directives concerning Pratt and Whitney Turbine Engines - JT9D Series, AD/JT9D/15, focus on the maintenance and safety requirements for the JT9D-7R4D, E models. According to section (1), this directive applies to certain JT9D turbine engines, and section (2) mandates that the requirements outlined in Pratt and Whitney ASB JT9D-7R4-72-318, Paragraph 2 "Accomplishment Instructions", must be followed. This includes specific inspection and modification procedures to prevent cracking of the stage 1-2 airseal in the high-pressure turbine. Section (3) specifies that compliance with these requirements must be achieved according to a program agreed upon by the Secretary, and it has been effective since 1 December 1986.
The obligations imposed by this directive are primarily on aircraft operators and maintenance personnel. They must adhere to the inspection and modification guidelines provided in the Pratt and Whitney ASB JT9D-7R4-72-318. This involves conducting detailed inspections of the stage 1-2 airseal and making necessary modifications to ensure the airseal does not crack, which could compromise engine performance and safety. The compliance program agreed upon by the Secretary outlines the specific steps and timelines for completing these tasks, ensuring that the directive is implemented in a structured and timely manner.
Failure to comply with the provisions of this directive can result in significant consequences. Under section (4) of the regulations, non-compliance can be considered an offence. The potential penalties for breaching these safety directives can include fines and other legal repercussions. While the specific maximum penalties are not detailed in the directive, it is clear that non-compliance could lead to serious civil or criminal penalties, given the critical nature of the safety measures involved. Ensuring adherence to the directive is essential to maintain airworthiness and avoid any legal or safety issues arising from non-compliance.