AD/PA-28/63 - Fuel Filler Cap - Inspection and Replacement

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, aim to ensure the safety and efficiency of civil aviation within the country. Specifically, Part 39 of these regulations addresses various aspects of airworthiness directives, including maintenance and operational requirements for aircraft. One such directive, AD/PA-28/63, pertains to the Piper PA-28 Series aeroplanes, focusing on the inspection and replacement of fuel filler caps. This directive was introduced to address safety concerns related to the integrity and functionality of fuel filler caps in certain model series, thereby mitigating risks associated with fuel system failures. The regulation applies to model PA-28-235 with serial numbers ranging from 28-10001 to 28-11236, requiring compliance within 100 hours of time in service after 31 July 1977. The overarching policy objective is to enhance aviation safety by ensuring that aircraft meet stringent maintenance standards.

Scope and Application

The Civil Aviation Regulations 1998, as amended, under Part 39 - 105 of the Civil Aviation Safety Authority (CASA) schedule of Airworthiness Directives, specifically addresses the maintenance and inspection requirements for the Piper PA-28 Series aeroplanes, more precisely the model PA-28-235 with serial numbers ranging from 28-10001 to 28-11236. This regulation applies to the aircraft operators, maintenance technicians, and other relevant entities responsible for the upkeep and operation of these specific aircraft models within Australia. The directive mandates compliance within 100 hours of time in service following the publication date of 31 July 1977, thereby ensuring the aircraft meet necessary safety standards. The geographic reach of this regulation is national, applying uniformly across the Commonwealth of Australia. There are no stated exclusions or exemptions within the provided text, and the directive does not explicitly mention extensions or restrictions through subordinate instruments.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 - 105 concerning the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, mandates specific requirements for the Piper PA-28 Series Aeroplanes. Section 39-105(1) of the regulations specifies the applicability of AD/PA-28/63, which pertains to fuel filler caps on the Model PA-28-235 with serial numbers ranging from 28-10001 to 28-101236. The directive requires compliance within 100 hours of time in service after 31 July 1977, as detailed in Piper Service Bulletin No. 571, Part B. This directive imposes a clear obligation on the owners or operators of the specified Piper PA-28-235 aircraft to inspect and, if necessary, replace the fuel filler caps. The inspection must be conducted within the specified timeframe to ensure compliance with safety standards. Failure to adhere to this requirement may result in the aircraft being deemed unairworthy, leading to potential grounding and operational disruptions. Operators must ensure that all maintenance and inspection activities are meticulously documented and meet the stringent safety criteria set out by the Civil Aviation Safety Authority. In terms of enforcement and consequences, non-compliance with AD/PA-28/63 can lead to significant legal and operational repercussions. Under Section 97 of the Civil Aviation Act 1988, operators who fail to comply with airworthiness directives can face civil penalties, including fines. The maximum penalty for non-compliance can be substantial, reflecting the seriousness of neglecting safety directives. Additionally, continued operation of a non-compliant aircraft may result in enforcement actions by the Civil Aviation Safety Authority, which can include directives to rectify the issue, suspension of the aircraft’s certificate of airworthiness, or even prosecution under criminal law for severe breaches that endanger safety.