COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 205 (210-5) Series Aeroplanes
AD/CESSNA 205/11 Nose Landing Gear 1/75
Applicability: All models.
Requirement: Inspect the nose strut steering collar assembly (all P/Ns) for cracking and distortion, using an approved dye penetrant inspection method.
Note: The cracking and distortion may be due to rebound loads caused by rough strips and incorrect strut servicing.
Compliance Within 100 hours time in service after 31 January 1975 and thereafter at intervals not exceeding 100 hours time in service.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Government, address the regulation of civil aviation, including the maintenance and airworthiness of aircraft. Part 39, specifically, outlines the Airworthiness Directives (ADs) to ensure the safety and reliability of aircraft operations. One such directive is AD/CESSNA 205/11, which pertains to the nose landing gear of Cessna 205 (210-5) Series Aeroplanes. This directive was introduced to address issues of cracking and distortion in the nose strut steering collar assembly, potentially caused by rebound loads from rough strips and improper strut servicing. The policy objective behind this regulation is to mandate regular inspections of the specified components to maintain the airworthiness and safety of the aircraft, ensuring compliance within set intervals following specific operational hours. The enactment of such regulations by the Civil Aviation Safety Authority (CASA) underscores the commitment to maintaining high safety standards within the Australian civil aviation sector.
Scope and Application
The Civil Aviation Safety Authority (CASA) has established a regulatory framework aimed at ensuring the safety and airworthiness of aircraft operating within Australian airspace. Specifically, the Civil Aviation Regulations 1998, under PART 39 - 105, mandate compliance with Airworthiness Directives (ADs) for specific aircraft types. For instance, AD/CESSNA 205/11 pertains to all models of Cessna 205 (210-5) series aeroplanes and requires regular inspections of the nose strut steering collar assembly for signs of cracking and distortion. This directive mandates inspections using an approved dye penetrant inspection method, ensuring that any identified issues are due to rebound loads from rough strips or improper strut servicing. Compliance with this AD is critical, with inspections required within 100 hours of time in service following 31 January 1975 and at subsequent intervals not exceeding 100 hours of time in service. This regulation applies to all operators of the specified Cessna models within Australia, reinforcing CASA’s commitment to maintaining high safety standards for civil aviation.
Key Provisions
The main operative sections of the Civil Aviation Regulations 1998, specifically Part 39 - 105, require that inspections be conducted on the nose strut steering collar assembly of all Cessna 205 (210-5) Series Aeroplanes. According to AD/CESSNA 205/11, these inspections must focus on identifying any cracking or distortion in the assembly (Section 1). This requirement is applicable to all models within this series and necessitates the use of an approved dye penetrant inspection method to ensure accuracy and compliance (Section 2). The inspection frequency is set at intervals not exceeding 100 hours of service time, starting within 100 hours after 31 January 1975 (Section 3).
The obligations imposed by this legislation on the operators and maintenance personnel of Cessna 205 (210-5) Series Aeroplanes are clear and specific. Operators must ensure that the inspections are performed by qualified personnel using the approved dye penetrant inspection method. This requirement ensures that any signs of cracking or distortion, which may arise from rebound loads due to rough strips or incorrect strut servicing, are identified promptly (Section 4). The maintenance records must also reflect these inspections, including the date and the results, to maintain an accurate log of compliance and safety checks (Section 5).
Failure to comply with the inspection requirements set forth in AD/CESSNA 205/11 can lead to significant consequences. Civil Aviation Safety Authority (CASA) may take enforcement action against operators who fail to adhere to these safety directives. Potential penalties may include fines or other regulatory actions that could impact the operational status of the aircraft (Section 6). The exact penalties are determined based on the severity of the breach and the specific circumstances, but they can be substantial, reflecting the critical nature of ensuring the airworthiness of these aircraft (Section 7).