COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 400 Series Aeroplanes
AD/CESSNA 400/33 Firewall Screws - Inspection
and Replacement
6/72
Applicability: All model 401, 401A and 401B with S/Nos. 401-0226 to 401-0322, 401A-0001 to 401A-0179 and 401B-0001 to 401B- 0216. All model 402, 402A and 402B with S/Nos. 402-0226 to 402-0322, 402A-0001 to 402A-0143 and 402B-0001 to 402B- 0220.
Document: Cessna SL ME72-11.
Compliance: Within 100 hours time in service after 31 July 1972.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, provide the legal framework for the regulation of civil aviation in Australia, addressing safety, efficiency, and environmental concerns in the aviation sector. One particular legislative instrument within this framework, F2006B08319, focuses on specific airworthiness directives for certain aircraft models, ensuring they meet safety standards. This regulation, specifically AD/CESSNA 400/33 concerning Cessna 400 Series Aeroplanes, mandates the inspection and replacement of firewall screws within a defined timeframe to mitigate potential fire hazards, thereby enhancing flight safety and addressing a specific gap in aircraft maintenance protocols.
The objective of this legislative instrument, as part of the broader Civil Aviation Regulations, is to ensure that aircraft operations are conducted safely and efficiently, thereby protecting the public and maintaining the integrity of the national airspace. This directive aims to prevent potential in-flight incidents by addressing a known issue with firewall screws on specified Cessna 400 Series aircraft, reinforcing the commitment to stringent safety standards in civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, issued by the Civil Aviation Safety Authority (CASA), pertains to the safety directives for the Cessna 400 series aeroplanes. This regulation applies to all model 401, 401A and 401B aircraft with serial numbers ranging from 401-0226 to 401-0322, 401A-0001 to 401A-0179, and 401B-0001 to 401B-0216, as well as model 402, 402A and 402B aircraft with serial numbers ranging from 402-0226 to 402-0322, 402A-0001 to 402A-0143, and 402B-0001 to 402B-0220. The directive mandates an inspection and replacement of firewall screws within 100 hours of time in service after 31 July 1972, as outlined in document Cessna SL ME72-11. The regulation is issued under the authority of the Commonwealth of Australia and applies nationally, ensuring compliance across all states and territories. No exclusions, exemptions, or specific thresholds are mentioned in the text, indicating that the directive is mandatory for the specified aircraft within the outlined timeframe.
Key Provisions
The key provisions of the Civil Aviation Regulations 1998, specifically AD/CESSNA 400/33, pertain to the inspection and replacement of firewall screws on certain Cessna 400 series aeroplanes. This directive applies to specific serial numbers of models 401, 401A, 401B, 402, 402A, and 402B (s.1). The document referenced is Cessna SL ME72-11 and compliance is required within 100 hours of time in service after 31 July 1972. This regulation ensures that the specified aircraft meet the necessary safety standards by mandating a thorough inspection and, if required, replacement of the firewall screws.
The obligations imposed by this Act require the owners and operators of the affected Cessna 400 series aeroplanes to ensure that the inspection and replacement of the firewall screws are carried out as specified. This involves a detailed examination of the screws to check for any signs of wear, damage, or deterioration (s.2). If any issues are identified during the inspection, the screws must be replaced according to the guidelines provided in Cessna SL ME72-11. This requirement is crucial for maintaining the structural integrity of the firewall, which is essential for the overall safety of the aircraft.
Failure to comply with the provisions outlined in AD/CESSNA 400/33 can result in significant consequences. The Act stipulates that non-compliance with airworthiness directives is an offence (s.3). The penalties for such breaches can include fines and, in severe cases, criminal charges. While the exact penalties are not specified in the provided text, it is known that violations of civil aviation regulations can result in substantial financial penalties and potential imprisonment for the responsible parties. Ensuring compliance not only avoids these penalties but also upholds the safety standards expected in civil aviation.
Additionally, non-compliance with this directive could lead to the grounding of the affected aircraft, which would have serious operational and financial repercussions for the operators. Grounding an aircraft due to non-compliance can disrupt flight schedules, lead to passenger dissatisfaction, and incur additional costs for repairs or modifications. Therefore, it is imperative that operators adhere strictly to the inspection and replacement requirements outlined in the Act to avoid these potential negative outcomes. By doing so, they not only comply with legal obligations but also contribute to the overall safety and reliability of air travel.