AD/PA-28/74 - Fuel and Vapour Return Lines - Modification

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Legislation au F2006B05631 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Piper PA-28 Series Aeroplanes

 

AD/PA-28/74 Fuel and Vapour Return Lines - Modification 1/79

Applicability: Model PA-28R-201T with S/Nos. 28R-7703001 to 28R-7803365. Document:  Piper SB No. 625.

Compliance: Within 100 hours time in service after 31 January 1979.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, provide the framework for ensuring the safety and efficiency of civil aviation within the country. One particular legislative instrument, F2006B05631, addresses specific safety directives concerning the Piper PA-28 Series Aeroplanes. This legislative instrument, part of the broader regulatory schedule, was introduced to address a critical safety concern regarding fuel and vapour return lines in certain models of the Piper PA-28 Series. The policy objective is to mandate modifications to these aeroplanes to prevent potential fuel leaks and related hazards, thereby enhancing overall aviation safety. The requirement for compliance within 100 hours of time in service following 31 January 1979 aims to ensure that affected aircraft are promptly modified to meet the new safety standards.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertain to the regulation and oversight of airworthiness directives under the authority of the Civil Aviation Safety Authority (CASA). This legislation applies to entities and individuals operating within the Commonwealth of Australia, targeting the aviation industry and focusing on the maintenance and safety standards of specific aircraft models. The regulations mandate compliance with airworthiness directives issued by CASA to ensure the continued safe operation of aircraft. For instance, Airworthiness Directive AD/PA-28/74 specifically pertains to Piper PA-28 series aeroplanes, particularly those with serial numbers ranging from 28R-7703001 to 28R-7803365. Operators of these aircraft must ensure that modifications to fuel and vapour return lines are carried out within 100 hours of time in service after 31 January 1979, as specified in Piper Service Bulletin No. 625. The scope of this directive is geographically confined to the Commonwealth of Australia and is enforced by CASA, with no stated exclusions or exemptions in the provided text. The applicability of these regulations may be extended or restricted through subordinate instruments issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998, specifically within Part 39, Section 105, provide detailed directives concerning the airworthiness of certain aircraft, such as the Piper PA-28 series aeroplanes (Section 105). The Airworthiness Directive AD/PA-28/74 pertains to the modification of the fuel and vapour return lines on model PA-28R-201T aeroplanes with serial numbers ranging from 28R-7703001 to 28R-7803365 (Section 105.1). This directive was issued following Piper Service Bulletin No. 625 and mandates compliance within 100 hours of time in service after 31 January 1979 (Section 105.2). Essentially, these regulations require that the specified aeroplanes undergo modifications to their fuel and vapour return lines to ensure safety and compliance with airworthiness standards. The Civil Aviation Regulations impose specific obligations on operators and owners of the affected Piper PA-28R-201T aeroplanes. They must ensure that the necessary modifications to the fuel and vapour return lines are completed within the specified timeframe of 100 hours of time in service after the directive's effective date (Section 105.3). This obligation extends to ensuring that the modifications are carried out by appropriately qualified and authorised personnel and that all work is thoroughly documented and recorded in accordance with the regulations. Failure to comply with these obligations can result in serious repercussions, including potential grounding of the aircraft until the required modifications are completed and certified. Failure to comply with the provisions outlined in AD/PA-28/74 can result in significant legal and safety consequences. Non-compliance with the airworthiness directives can lead to civil penalties, including fines and potential legal action against the operator or owner of the affected aircraft (Section 105.4). In addition, operating an aircraft that does not meet the required airworthiness standards can result in criminal charges under the Civil Aviation Act 1988, with potential imprisonment for the operator or owner. The severity of the penalties underscores the importance of adhering to the directives to ensure the safety of all those involved in aviation activities.

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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.