AD/CESSNA 400/32 - Fuel Pressure Regulator Fitting - Inspection

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, address the regulation of civil aviation within Australia, ensuring safety and compliance with international standards. This particular legislative instrument, F2006B08318, focuses on the Cessna 400 Series Aeroplanes, specifically mandating an inspection directive for the fuel pressure regulator fitting on model 414 with serial numbers ranging from 414-0001 to 414-0265. This directive aims to maintain the airworthiness of these aircraft by ensuring that the fuel pressure regulator fittings are inspected within 10 hours of time in service after 2 June 1972. The policy objective underpinning this legislation is to enhance aviation safety and reliability by addressing potential mechanical issues that could compromise flight operations.

Scope and Application

The Civil Aviation Regulations 1998, as amended, and specifically Part 39 - 105, pertain to the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, which are regulatory requirements aimed at ensuring the safe operation of aircraft. In this context, AD/CESSNA 400/32 mandates that the fuel pressure regulator fitting of Cessna 400 series aeroplanes, particularly those with serial numbers ranging from 414-0001 to 414-0265, must be inspected within 10 hours of time in service after 2 June 1972. This directive applies to operators of these specific aircraft models and necessitates compliance with the detailed inspection requirements outlined in the referenced document, Cessna SL ME72-6. This legislative instrument has a national reach within Australia, governed by the Commonwealth, and is enforceable under the Civil Aviation Act 1988. No exclusions, exemptions, or thresholds are specified in the directive itself, though CASA may issue further clarifications or modifications through subordinate instruments.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, contain specific provisions that pertain to the airworthiness directives for aircraft, particularly focusing on the Cessna 400 series aeroplanes. Section AD/CESSNA 400/32 addresses a critical aspect of the aircraft's operational safety by mandating an inspection of the fuel pressure regulator fitting for model 414 with serial numbers ranging from 414-0001 to 414-0265. The directive necessitates that this inspection be conducted within 10 hours of time in service following the date of 2 June 1972 (section AD/CESSNA 400/32). The compliance document for this inspection is identified as Cessna SL ME72-6. These regulations impose clear obligations on the parties involved, specifically on aircraft operators and maintenance personnel. They must ensure that the required inspection is carried out in accordance with the stipulated timeframe, as outlined in the directive. The necessity for adherence to this regulation is to maintain the aircraft's airworthiness and ensure safety during flight operations. Failure to comply with these provisions can lead to serious consequences, including potential aircraft malfunctions and safety hazards. Under the Civil Aviation Regulations 1998, non-compliance with the airworthiness directives can result in various penalties. While specific maximum penalties are not detailed in the provided excerpt, breaches of such safety regulations can lead to significant civil or criminal liabilities. The severity of the penalties may depend on the extent of the non-compliance and the resulting impact on aviation safety. It is essential for all stakeholders to understand and adhere to these regulations to avoid legal repercussions and ensure the highest standards of safety in aviation operations.