AD/PA-44/2 - Fuel Line - Inspection and Modification

Overview

The Civil Aviation Regulations 1998 were enacted to provide a comprehensive regulatory framework governing civil aviation in Australia, ensuring safety and efficiency within the industry. This legislative instrument is part of a broader legislative effort to address gaps in aviation safety standards and to harmonise with international regulations. The enactment was overseen by the Australian Parliament, with the overarching policy objective being the enhancement of civil aviation safety through stringent regulatory oversight and the issuance of specific directives to mitigate identified risks. One such directive, AD/PA-44/2, pertains to the inspection and modification of fuel lines in certain Piper PA-44 (Seminole) series aeroplanes. This directive was introduced to address a specific safety concern related to the fuel lines of these aircraft models, ensuring compliance with safety standards and preventing potential hazards that could compromise flight safety. The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority, include detailed provisions that mandate specific safety measures for aircraft. These regulations are designed to maintain the highest standards of airworthiness and operational safety, reflecting a commitment to public safety and the integrity of the aviation sector. The policy objective behind these regulations is to ensure that all aircraft meet rigorous safety criteria, thereby minimising the risk of accidents and enhancing overall aviation safety. Through the issuance of specific airworthiness directives, such as AD/PA-44/2, the Civil Aviation Safety Authority ensures that identified safety issues are promptly addressed, thereby maintaining the safety and reliability of civil aviation operations in Australia.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105, addresses safety directives for various aircraft types, including the Piper PA-44 (Seminole) series aeroplanes. This particular legislation mandates the inspection and modification of fuel lines for certain models of the PA-44, which applies to specific serial numbers within the model range, as outlined in the Civil Aviation Safety Authority Schedule of Airworthiness Directives. The directive ensures that the aeroplanes meet certain safety standards before certification, thereby safeguarding aviation safety for both operators and passengers. The scope of this regulation is limited to the specified serial numbers, thereby not affecting other models or types of aircraft outside the designated parameters. The jurisdictional reach of these regulations is national, enforced by the Civil Aviation Safety Authority, and they are applicable across all states and territories of Australia, ensuring a consistent approach to aircraft safety. The regulations do not specify any exclusions or exemptions, thereby applying uniformly to the targeted aircraft serial numbers. The applicability of these regulations may be extended or clarified through subordinate instruments, ensuring that the directives remain relevant and effective in maintaining airworthiness standards.

Key Provisions

The Civil Aviation Regulations 1998 (Cth) under Part 39 - 105, specifically the Airworthiness Directive AD/PA-44/2, addresses the inspection and modification of fuel lines in certain Piper PA-44 (Seminole) series aeroplanes (s 1). The directive applies to model PA-44-180 aeroplanes with serial numbers (S/Nos) within specific ranges (s 1). The directive is mandatory and must be complied with before the aeroplane can be certified (s 1). This regulation imposes clear obligations on the owners and operators of the specified Piper PA-44 aircraft. They must inspect the fuel lines and make necessary modifications as outlined in Piper Service Bulletin No. 627 (s 1). This involves a thorough examination of the fuel lines to ensure they meet the required safety standards and making any modifications to correct any deficiencies identified during the inspection (s 1). Failure to comply with these requirements can lead to serious consequences. Failure to comply with the provisions of AD/PA-44/2 can result in severe civil and criminal consequences. Under the Civil Aviation Act 1988 (Cth), non-compliance with an Airworthiness Directive can lead to fines and imprisonment. The maximum penalty for an individual who breaches this directive can include fines of up to $22,200 and imprisonment for up to one year, or both (s 1). Additionally, the aeroplane cannot be certified as airworthy until the required modifications have been completed, which could prevent the aircraft from being operated legally.