COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 400 Series Aeroplanes
AD/CESSNA 400/8 Fuel Lines - Modification and Inspection 4/69
Applicability: All model 401, 401A and 402 with S/Nos. 401-0001 to 401-0322 and 401A-0001 to 401A-0010 and 402-0001 to 402-0319.
Document: Cessna SL ME68-27.
Compliance: Within 100 hours time in service after 21 May 1969.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, form a crucial component of the legislative framework governing civil aviation within the country. Among various provisions, Part 39, specifically addressing airworthiness directives, plays an essential role in ensuring the safety of aircraft operations. One such directive is AD/CESSNA 400/8, which pertains to the modification and inspection of fuel lines for certain Cessna 400 series aeroplanes. This directive was introduced to address safety concerns related to fuel line integrity, aiming to mitigate risks of fuel leaks that could potentially lead to catastrophic failures or accidents. The policy objective is to maintain the highest standards of safety in civil aviation by mandating specific compliance measures for identified aircraft models.
The AD/CESSNA 400/8 directive applies to all model 401, 401A, and 402 Cessna aeroplanes with specified serial numbers, requiring compliance within 100 hours of time in service after the directive's issuance on 21 May 1969. This legislative instrument, under the authority of the Civil Aviation Safety Authority, mandates modifications and inspections to ensure that the fuel lines meet the required safety standards. By implementing these measures, the legislation aims to enhance the overall safety profile of the affected aircraft, thereby protecting both the passengers and crew from potential hazards associated with compromised fuel line systems.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, issued under the authority of the Civil Aviation Safety Authority, mandates the compliance of certain Cessna 400 Series aeroplanes with Airworthiness Directives. This legislation applies to all model 401, 401A, and 402 Cessna aeroplanes within specified serial number ranges, imposing a requirement for modification and inspection of fuel lines. Compliance with these directives must be achieved within 100 hours of time in service following the issue date of 21 May 1969. The scope of the legislation is geographically and jurisdictionally confined to the Commonwealth of Australia, with enforcement by the Civil Aviation Safety Authority. There are no stated exclusions or exemptions within the text, and compliance thresholds are strictly defined by the time in service parameter. This legislation extends its application through the use of subordinate instruments such as the referenced document Cessna SL ME68-27, which provides detailed guidance on the required modifications and inspection procedures.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes Airworthiness Directives (ADs) that mandate the compliance of certain aircraft models with specific safety requirements. One such AD is AD/CESSNA 400/8, which pertains to the modification and inspection of fuel lines in Cessna 400 Series Aeroplanes, namely models 401, 401A, and 402. The applicability of this directive extends to specific serial numbers within these models, as detailed in the regulation (sections 39 - 105). The document that outlines these requirements is identified as Cessna SL ME68-27, and compliance must be achieved within 100 hours of time in service after 21 May 1969.
Entities governed by this AD are required to ensure that the fuel lines of the specified Cessna 400 Series Aeroplanes are modified and inspected according to the standards outlined in the referenced document. This involves a thorough examination and, if necessary, the modification of the fuel lines to prevent any potential safety hazards. The regulation sets forth clear timelines for compliance, mandating that these actions be completed within a specified period following the directive's publication date.
Failure to comply with the provisions of AD/CESSNA 400/8 can result in significant consequences. Under the Civil Aviation Regulations, non-compliance with an AD is considered a breach of safety regulations. Such breaches may lead to enforcement actions by the Civil Aviation Safety Authority (CASA). The penalties for non-compliance can include substantial fines, and in severe cases, the grounding of the affected aircraft until the required modifications and inspections are completed. The exact penalties are determined based on the severity of the breach and are outlined in the broader Civil Aviation Regulations.
It is important for entities and individuals governed by this AD to adhere strictly to the stipulated requirements and deadlines. Non-compliance not only risks the safety of the aircraft and its passengers but also subjects the operators to potential legal and financial repercussions. Therefore, it is imperative to ensure that all modifications and inspections are carried out in a timely and thorough manner to avoid any adverse consequences.