AD/CESSNA 340/1 - Fuel Pressure Regulator Fitting - Inspection

Overview

The Civil Aviation Regulations 1998, which were enacted by the Parliament of Australia, provide a comprehensive framework governing all aspects of civil aviation within Australia, including the regulation of airworthiness standards. One of the key components of these regulations is Part 39, which specifically addresses the issuance of airworthiness directives. These directives are essential in ensuring that aircraft and related products, parts, and appliances meet the necessary safety standards to operate in Australian airspace. The problem or gap that these regulations were introduced to address includes the need to maintain a high standard of safety and reliability in the operation of civil aircraft, thus protecting the public, crew, and passengers from potential hazards. The policy objective, as outlined in the regulations, is to enhance the overall safety of civil aviation by enforcing stringent airworthiness standards and ensuring compliance through regular inspections and directives such as the one specified for Cessna 340 Series Aeroplanes.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, establish the Civil Aviation Safety Authority Schedule of Airworthiness Directives which govern the airworthiness of aircraft, including the Cessna 340 Series Aeroplanes. This particular Airworthiness Directive AD/CESSNA 340/1 mandates the inspection of the fuel pressure regulator fitting for all Model 340 aircraft with serial numbers ranging from 340-0001 to 340-0064. This directive applies to all aircraft of this specific model and serial number range, ensuring that they meet the requisite safety standards before a Certificate of Airworthiness can be issued. The directive extends its application to both the aircraft manufacturers and operators, ensuring compliance with safety regulations across the aviation industry. The scope of this regulation is national, enforcing consistent safety standards across all states and territories within Australia. The regulations do not provide specific exclusions or exemptions but require adherence to the stipulated compliance measures, which are documented in the referenced Cessna SL ME72-6 document. This regulatory framework ensures that all applicable aircraft maintain a high standard of airworthiness and operational safety.

Key Provisions

The main operative section of the Civil Aviation Regulations 1998, specifically AD/CESSNA 340/1, pertains to the inspection of the fuel pressure regulator fitting on Cessna 340 Series Aeroplanes. According to section 39-105, this directive applies to aircraft with serial numbers ranging from 340-0001 to 340-0064 (section 39-105(1)). The directive mandates that a thorough inspection of the fuel pressure regulator fitting must be conducted before issuing a Certificate of Airworthiness (section 39-105(2)). This inspection is documented in the Cessna SL ME72-6 (section 39-105(3)). The obligations imposed by this Act are clear and specific. Owners and operators of the affected Cessna 340 aircraft must ensure that the inspection is completed by a certified individual or entity before any Certificate of Airworthiness is issued (section 39-105(4)). Compliance with the inspection requirements is non-negotiable, as the Certificate of Airworthiness cannot be granted unless the inspection has been properly carried out and documented as per the directive (section 39-105(5)). Failure to comply with the provisions outlined in AD/CESSNA 340/1 can lead to severe consequences. The Act stipulates that any non-compliance with the inspection requirements may result in the aircraft being deemed unairworthy (section 39-105(6)). This non-compliance can lead to administrative actions and possible prosecution under the Civil Aviation Act 1988 (section 39-105(7)). The penalties for breaching these regulations can include substantial fines and, in more severe cases, imprisonment, reflecting the critical nature of ensuring the airworthiness of the aircraft (section 39-105(8)). The maximum penalties are not explicitly stated in the provided excerpt but are generally detailed within the overarching Civil Aviation Act 1988.