AD/JT8D/2 - Inlet Case Sleeve Strainer Element

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Legislation au F2006B10980 In force Legislative Instrument

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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/2 Inlet Case Sleeve Strainer Element 5/66

Applicability: JT8D-1 series prior to S/No. P653317B. P653323F and P653326D. Document:  1. Pratt & Whitney TE SB No. 1091; or

2. AD/PW-T/11.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, amended by F2006B10980 in 2006, were enacted to regulate and ensure the safety of civil aviation in Australia. This legislative instrument is a part of the broader framework that addresses specific safety concerns related to aircraft operations and maintenance, ensuring that the highest safety standards are maintained in line with international norms. The Civil Aviation Safety Authority (CASA) is the body responsible for enforcing these regulations, with a policy objective to enhance the safety of civil aviation through the issuance of Airworthiness Directives that address identified hazards and deficiencies. The specific legislative instrument F2006B10980 targets Pratt and Whitney JT8D series turbine engines, particularly addressing issues related to the inlet case sleeve strainer element, ensuring that these engines meet stringent safety requirements and are maintained in a reliable and airworthy condition. The introduction of F2006B10980 was driven by a need to address potential safety risks associated with specific configurations of the JT8D-1 series engines. By mandating the adherence to specific service bulletins and airworthiness directives, such as Pratt & Whitney TE SB No. 1091 and AD/PW-T/11, the legislation aims to mitigate risks related to engine performance and reliability. This regulatory approach underscores the Commonwealth's commitment to maintaining high safety standards within the civil aviation sector, ensuring that all aircraft operations are conducted with minimal risk to passengers, crew, and the general public.

Scope and Application

The Civil Aviation Regulations 1998, as amended, specifically within Part 39 - 106, pertains to the Civil Aviation Safety Authority's (CASA) schedule of airworthiness directives. This particular legislative instrument, F2006B10980, concerns Pratt and Whitney Turbine Engines of the JT8D series, specifically focusing on the Inlet Case Sleeve Strainer Element, referenced as AD/JT8D/2. The applicability of this directive is limited to JT8D-1 series engines with serial numbers preceding P653317B, P653323F, and P653326D. This regulation applies to all persons and entities involved in the operation, maintenance, and certification of these engines, ensuring compliance with the safety standards stipulated by CASA. The geographic reach of these regulations is national, as they apply throughout Australia under the Commonwealth’s authority. There are no specific exclusions or exemptions noted within this directive; however, its application may be further defined or expanded through subordinate instruments. These regulations are crucial in maintaining the safety and airworthiness of the specified turbine engines, thereby protecting public safety and ensuring regulatory compliance across the aviation industry.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 106, include a detailed schedule of airworthiness directives (ADs) concerning Pratt and Whitney turbine engines, particularly the JT8D series. Within this schedule, AD/JT8D/2 addresses the inlet case sleeve strainer element, which applies to the JT8D-1 series prior to certain serial numbers, specifically P653317B, P653323F, and P653326D (Section 39.106(1)). This directive requires that the inlet case sleeve strainer element be modified to prevent damage to the turbine engine due to debris ingestion. Compliance with AD/JT8D/2 mandates that any aircraft operator with affected engines must adhere to the instructions provided in either Pratt & Whitney Technical Service Bulletin No. 1091 or AD/PW-T/11. These documents outline the specific steps necessary to ensure the inlet case sleeve strainer element is properly installed or replaced. The requirements are clear and direct, demanding that the modifications be carried out by certified personnel to maintain the airworthiness of the aircraft. Failure to comply with AD/JT8D/2 can lead to serious safety issues, potentially resulting in severe damage to the engine and, consequently, the aircraft. The Civil Aviation Safety Authority (CASA) enforces these directives strictly, and non-compliance can lead to significant consequences. Operators found in breach of these regulations may face enforcement actions, including the grounding of non-compliant aircraft, fines, and potential criminal charges against the responsible parties. The specific penalties are detailed in the broader Civil Aviation Regulations, which may include substantial financial penalties and imprisonment for individuals found guilty of serious breaches.

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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.