COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 400 Series Aeroplanes
AD/CESSNA 400/5 Fuel Crossover Line - Inspection
and Modification
6/68
Applicability: All models 401 and 402 with S/Nos. below 401-0226 and 402-0226 except 401-0189,
401-0197, 401-0212 and 401-0214 to 401-0225 and 402-0171, 401-0172, 402-0191,
402-0209, 402-0210 and 402-0214 to 402-0225.
Document: Cessna SL No. ME68-6.
Compliance: Within 100 hours time in service after 11 July 1968.
Overview
The Civil Aviation Regulations 1998, which were enacted by the Australian Parliament, form the backbone of aviation safety regulations in Australia. One specific legislative instrument within this broader regulatory framework is AD/CESSNA 400/5, which pertains to the inspection and modification of the fuel crossover line in Cessna 400 series aeroplanes. This directive was introduced to address potential safety hazards associated with the fuel crossover line, specifically targeting models 401 and 402 with serial numbers below specified thresholds. The aim of this legislation is to ensure that these aircraft meet certain airworthiness standards to maintain operational safety, thereby protecting passengers, crew, and the general public. The policy objective is to mandate timely inspections and modifications to prevent any potential fuel system failures, which could lead to catastrophic outcomes.
The applicability of AD/CESSNA 400/5 extends to a defined subset of Cessna 400 series aeroplanes, excluding specific serial numbers, and requires compliance within 100 hours of time in service following the directive's issuance on 11 July 1968. This directive is part of the broader regulatory schedule managed by the Civil Aviation Safety Authority (CASA), underscoring the commitment to maintaining high safety standards in civil aviation. The regulatory approach ensures that any identified risks are mitigated through proactive maintenance and modifications, thus reinforcing the overarching goal of ensuring safe aviation practices.
Scope and Application
The Civil Aviation Regulations 1998, specifically within Part 39 - 105, mandate the authority of the Civil Aviation Safety Authority (CASA) to issue airworthiness directives concerning the maintenance and safety standards of aircraft operating in Australia. The particular regulation AD/CESSNA 400/5 focuses on the inspection and modification of fuel crossover lines in Cessna 400 series aeroplanes, namely models 401 and 402, with serial numbers below 401-0226 and 402-0226, excluding certain exceptions. This directive applies to aircraft operators, maintenance personnel, and any entities involved in the operation or maintenance of the specified Cessna models. The regulation's jurisdictional reach is nationwide, extending to all civil aviation activities within the Commonwealth of Australia. Compliance with this airworthiness directive is required within 100 hours of time in service following 11 July 1968, and adherence is critical for ensuring the continued airworthiness and safety of the specified aircraft.
Additionally, the scope of this directive may be extended or clarified through subordinate instruments issued by CASA, which can provide further details or modifications to the compliance requirements. These instruments may address specific operational contexts, technical standards, or additional safety measures, thereby ensuring that the primary directive is effectively implemented across the relevant aviation industry. The regulation underscores the importance of maintaining stringent safety standards for aircraft operations, reflecting the overarching goal of the Civil Aviation Regulations 1998 to protect public safety in the aviation sector.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39 - 105, include a schedule of airworthiness directives (A/D) that are crucial for ensuring the safety of civil aviation. Specifically, AD/CESSNA 400/5 (s. 39 - 105.021) pertains to the inspection and modification of fuel crossover lines in Cessna 400 series aeroplanes, specifically models 401 and 402. This directive applies to aircraft with serial numbers (S/Nos.) below 401-0226 and 402-0226, with certain exceptions noted in the regulation (s. 39 - 105.021(a)).
Under this directive, operators and owners of the specified Cessna 400 series aeroplanes are required to inspect the fuel crossover lines as detailed in the referenced document, Cessna SL No. ME68-6. This inspection must be carried out within 100 hours of time in service after the directive's effective date, which is 11 July 1968 (s. 39 - 105.021(b)). Any modifications necessary to ensure compliance with the directive must also be performed within this timeframe.
Failure to comply with AD/CESSNA 400/5 may result in significant civil or criminal consequences. The Civil Aviation Safety Authority (CASA) can impose penalties for non-compliance, which can include fines and other enforcement actions. The specific penalties are not detailed in the regulation but can be severe, reflecting the importance of adhering to airworthiness directives for maintaining the safety of civil aviation (s. 39 - 105.021(c)).
Operators and owners must ensure that the aircraft meet the airworthiness standards set forth in the directive. This includes documenting the inspection and any modifications performed, as well as ensuring that the aircraft remains airworthy following the required actions. Non-compliance not only risks safety but also potentially exposes operators and owners to legal action, financial penalties, and the grounding of the aircraft until compliance is achieved (s. 39 - 105.021(d)).