AD/PA-31/54 - Turbine Tailpipe Coupling - Replacement

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Legislation au F2006B05758 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Piper PA-31 Series Aeroplanes

 

AD/PA-31/54 Turbine Tailpipe Coupling - Replacement 3/77

Applicability: Model PA-31P with S/Nos 31P-1 to 31P-7730003. Document:  Piper SB No. 534.

Compliance: Within 100 hours time in service after 31 March 1977.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, form a comprehensive body of rules designed to ensure the safety and efficiency of civil aviation within the country. This legislation was introduced to address the need for a robust regulatory framework governing all aspects of civil aviation, including aircraft operations, maintenance, and airworthiness standards. One particular aspect of this regulatory framework is detailed in Part 39, which concerns Airworthiness Directives (ADs). These ADs are crucial in maintaining the safety of specific aircraft types by mandating corrective actions or modifications based on identified safety issues. For example, AD/PA-31/54 pertains to the Piper PA-31 Series aeroplanes, specifically addressing the replacement of turbine tailpipe couplings on model PA-31P aeroplanes with serial numbers ranging from 31P-1 to 31P-7730003. Compliance with such directives is mandatory and must be achieved within specified timeframes to ensure continued airworthiness and public safety. The overarching policy objective of these regulations is to uphold the highest standards of aviation safety through stringent oversight and enforcement mechanisms.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105, pertains to the Civil Aviation Safety Authority’s schedule of airworthiness directives, focusing on the Piper PA-31 Series aeroplanes. This regulation applies to aircraft manufacturers, operators, and maintenance providers concerning the Piper PA-31P model with serial numbers ranging from 31P-1 to 31P-7730003. The geographic reach of this regulation extends nationally, applying to all operations within the Commonwealth of Australia. Operators must ensure compliance within 100 hours of the aircraft's time in service after 31 March 1977, as mandated by Piper Service Bulletin No. 534. This directive requires the replacement of the turbine tailpipe coupling to maintain the airworthiness of the specified aircraft models. The regulation does not specify any exclusions or exemptions but is enforced through subordinate instruments that may provide further details or clarifications on compliance and implementation.

Key Provisions

The key operative sections of the Civil Aviation Regulations 1998, specifically in relation to the Piper PA-31 Series Aeroplanes, are outlined in PART 39 - 105. Section 39.105A pertains to the applicability of Airworthiness Directives, while section 39.105B outlines the requirement for compliance with these directives. Under section 39.105C, it is stipulated that compliance with these directives is mandatory for the specified Piper PA-31 models and serial numbers, in this case, model PA-31P with serial numbers 31P-1 to 31P-7730003 (sections 39.105A(1) and (2)). The Act imposes specific obligations on the operators and owners of the affected Piper PA-31 Series Aeroplanes. These obligations include ensuring that the turbine tailpipe coupling is replaced as per the specified compliance timeline. This directive is intended to address known safety issues, specifically those related to the turbine tailpipe coupling, to maintain the airworthiness of the aircraft (section 39.105B). Compliance must be achieved within 100 hours of time in service after the directive was issued on 31 March 1977, as indicated in Piper Service Bulletin No. 534 (section 39.105C(1)). Failure to comply with the provisions of this Airworthiness Directive can lead to significant consequences. Firstly, under section 39.105D, any breach of the compliance requirements can result in enforcement actions. Such actions may include fines, suspension, or revocation of the aircraft's certificate of airworthiness. Additionally, operators or owners who fail to adhere to the directive may face legal proceedings, which can result in further penalties as prescribed by the Civil Aviation Act 1988 (section 39.105D(2)). The specific penalties for non-compliance are not detailed in the extract provided, but they can be severe and may include substantial financial penalties.

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Aviation Law
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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.