AD/PW-P/16 Amdt 1 - Master Rod - Retirement Life

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B06404 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Pratt and Whitney Piston Engines

 

AD/PW-P/16

Amdt 1


Master Rod - Retirement Life NK

 

Applicability: R1340-S3H1-G-CER and R1340-S3H1-G.

 

Requirement: Master rod P/N 11865 installed in Wasp R1340-S3H1-G-CER and -S3H1-G engines shall be retired from service after completion of one overhaul period of agricultural operations.

 

Compliance: Forthwith.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, are a comprehensive set of rules governing civil aviation operations within Australia. One of the amendments to these regulations is found in PART 39 - 106, which pertains to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives. Specifically, AD/PW-P/16 Amendment 1 addresses the retirement life of master rods for Pratt and Whitney piston engines, particularly those designated as R1340-S3H1-G-CER and R1340-S3H1-G. This amendment was introduced to address the problem of ensuring the safety and reliability of these specific engines by specifying that master rods with the part number 11865 must be retired from service after the completion of one overhaul period in agricultural operations. The policy objective is to enhance safety standards in civil aviation by ensuring that components of engines are maintained within their specified operational limits.

Scope and Application

The Civil Aviation Regulations 1998, specifically under PART 39 - 106, mandate the Civil Aviation Safety Authority’s (CASA) Schedule of Airworthiness Directives for Pratt and Whitney piston engines, including Amendment 1 concerning the master rod retirement life. This directive applies to engines identified as R1340-S3H1-G-CER and R1340-S3H1-G, which must adhere to the requirement that the master rod part number 11865 be retired from service immediately after the completion of one overhaul period of agricultural operations. The legislation is applicable to any entity or individual operating these specified engines within Australia, thereby encompassing the entire Commonwealth jurisdiction. The regulation does not explicitly exclude any particular entities or operations but necessitates strict compliance to ensure aviation safety standards are maintained. Subordinate instruments may further extend or refine the application of these directives to clarify operational specifics or address emerging safety concerns.

Key Provisions

The Civil Aviation Regulations 1998, particularly in PART 39 - 106, provide specific directives concerning the airworthiness of aircraft engines, with a notable focus on Pratt and Whitney piston engines. Within this regulatory framework, AD/PW-P/16 Amendment 1 addresses the "Master Rod - Retirement Life." Specifically, section (R1340-S3H1-G-CER and R1340-S3H1-G) stipulates that the master rod with part number 11865, used in Wasp R1340-S3H1-G-CER and -S3H1-G engines, must be retired from service after completing one overhaul period of agricultural operations. This requirement is clear and mandates immediate action once the specified condition is met. The obligations under this directive are straightforward yet crucial. Operators of aircraft equipped with the specified Wasp engines must ensure that the master rod is monitored and tracked throughout its operational life. Upon completion of one overhaul period in agricultural operations, the master rod must be retired and replaced, ensuring that the directive is adhered to without deviation. This immediate compliance requirement underscores the importance of maintaining the integrity and safety of the aircraft's engine system. Failure to comply with the airworthiness directives set forth in the Civil Aviation Regulations 1998 can lead to significant consequences. Non-compliance with AD/PW-P/16 Amendment 1 could result in serious safety risks, potentially leading to engine failure or other aviation incidents. The regulations impose penalties for breaches, with the potential for both civil and criminal sanctions. The exact penalties are not specified within the text but typically involve fines, enforcement actions, or more severe repercussions depending on the severity and impact of the breach. Overall, the directive is designed to prevent potential failures and ensure that the engines remain in a safe and operational condition. Operators must ensure that all components, especially critical ones like the master rod, are maintained in accordance with the stipulated regulations. The consequences of failing to adhere to these directives are significant, highlighting the importance of strict compliance and proactive maintenance practices.

Legal classification tags

Area of Law
Aviation Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
Retirement Life

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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.