AD/CESSNA 205/6 Amdt 2 - Auxiliary Fuel Pump Electrical System

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, provide a comprehensive framework for ensuring the safety and efficiency of civil aviation operations across the country. A significant aspect of these regulations is the Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically Part 39 - 105, which addresses mandatory safety directives for particular aircraft types. One such directive is AD/CESSNA 205/6 Amendment 2, which pertains to the auxiliary fuel pump electrical system of the Cessna 205 (210-5) Series Aeroplanes. This directive was introduced to address potential safety risks associated with the auxiliary fuel pump electrical system in certain models of Cessna aircraft, ensuring that they remain airworthy and compliant with safety standards. The overarching policy objective of this regulation is to maintain the highest safety standards within Australia's civil aviation sector by mandating specific actions and compliance timelines for identified safety concerns. The enactment of this airworthiness directive by the Civil Aviation Safety Authority under the authority granted by the Civil Aviation Regulations 1998 aims to ensure that all affected aircraft are subject to necessary modifications or inspections within a specified period. For the Cessna 205 and 205A models with serial numbers ranging from 205-0001 to 205-0577, compliance with the requirements outlined in Cessna Service Letters SL SE69-9 or SL SE70-25 is mandatory, with a compliance deadline set at 100 hours of time in service after 29 August 1969. This directive exemplifies the regulatory body's commitment to proactive safety management by addressing potential hazards before they can impact flight safety.

Scope and Application

The Civil Aviation Regulations 1998, under the jurisdiction of the Civil Aviation Safety Authority, mandate the issuance of Airworthiness Directives to ensure the safety of aircraft in operation. Specifically, Part 39 - 105 applies to the Cessna 205 (210-5) Series Aeroplanes, with the directive AD/CESSNA 205/6 Amendment 2 focusing on the auxiliary fuel pump electrical system. This directive applies to Model 205 and 205A aircraft with serial numbers ranging from 205-0001 to 205-0577, necessitating compliance within 100 hours of time in service following 29 August 1969. Compliance with this directive is to be achieved by adhering to the specifications outlined in Cessna Service Letters SE69-9 or SE70-25. This regulation is applicable nationally, overseen by the Commonwealth of Australia, and there are no stated exclusions or exemptions within the provided text. The scope of the directive is specific to the mentioned model and serial number range, and further application or restrictions may be delineated through subordinate instruments.

Key Provisions

The Civil Aviation Regulations 1998, specifically within Part 39, Section 105, provide detailed directives concerning the airworthiness of aircraft, including the Cessna 205 (210-5) series aeroplanes. The primary operative sections in this regard are AD/CESSNA 205/6 Amendment 2, which focuses on the auxiliary fuel pump electrical system. This section applies to Model 205 and 205A aircraft with serial numbers ranging from 205-0001 to 205-0577. The requirement outlined in this amendment mandates that aircraft owners or operators must adhere to either Cessna Service Letter (SL) SE69-9 or Cessna SL SE70-25, which detail the necessary actions to ensure compliance with airworthiness standards. Compliance with these directives must be achieved within 100 hours of time in service following 29 August 1969. The Act imposes several obligations on the parties and entities it governs. Primarily, aircraft owners or operators must ensure that the specified maintenance actions are carried out in accordance with the directives provided by Cessna. This involves either implementing the procedures outlined in SL SE69-9 or SL SE70-25, depending on the specific circumstances and recommendations provided by Cessna. It is imperative that these actions are completed within the stipulated timeframe to maintain the airworthiness of the aircraft. Furthermore, it is the responsibility of the operator to keep accurate records of any work performed to comply with these directives, as well as to ensure that all personnel involved in the maintenance process are adequately trained and qualified. Failure to comply with the requirements set forth in these airworthiness directives can result in significant consequences. Under the Civil Aviation Regulations, non-compliance may lead to enforcement actions, including the potential grounding of the aircraft until the necessary actions are completed. In addition to administrative penalties, there are also potential civil and criminal consequences for serious breaches. For instance, if non-compliance is found to have contributed to an accident or incident, the responsible party could face criminal charges. The maximum penalties for such offences can be severe, including substantial fines and imprisonment, reflecting the seriousness with which aviation safety is treated under Australian law.