COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 500 (Citation) Series Aeroplanes
AD/CESSNA 500/12 Glideslope Interlock - Modification 9/75
Applicability: Model 500 with S/Nos. 500-0001 to 500-0239. Document: Cessna Citation SB 34-27.
Compliance: Within 100 hours time in service after 30 September 1975.
Overview
The Civil Aviation Regulations 1998, specifically under Part 39 - 105 and the Civil Aviation Safety Authority Schedule of Airworthiness Directives, were enacted to ensure that civil aviation in Australia meets the highest safety standards. This legislative instrument, introduced by the Australian Government, addresses the need for stringent and consistent airworthiness directives to maintain safety across the nation's aviation fleet. One such directive, AD/CESSNA 500/12, pertains to the Cessna 500 (Citation) Series Aeroplanes, requiring modifications to the glideslope interlock for specific models to prevent operational hazards. The policy objective is to ensure that aircraft operate within safe parameters, reducing the risk of accidents due to technical failures.
This directive, which applies to Model 500 with serial numbers ranging from 500-0001 to 500-0239, mandates compliance within 100 hours of time in service after 30 September 1975, as outlined in Cessna Citation Service Bulletin 34-27. The regulation is enforced by the Civil Aviation Safety Authority to ensure adherence to safety protocols, reflecting the government's commitment to maintaining rigorous safety standards in civil aviation.
Scope and Application
The Civil Aviation Safety Authority (CASA) regulations, specifically Part 39 - 105 of the Civil Aviation Regulations 1998, pertain to the airworthiness directives for certain aircraft, such as the Cessna 500 (Citation) Series Aeroplanes. This legislation applies to the model 500 with serial numbers ranging from 500-0001 to 500-0239, mandating compliance with a specified modification to the glideslope interlock system. The directive, identified as AD/CESSNA 500/12, necessitates that the required modifications be implemented within 100 hours of the aircraft's time in service after 30 September 1975, as detailed in the Cessna Citation Service Bulletin 34-27. The regulations are applicable nationwide, encompassing all entities and individuals who operate or are responsible for the maintenance of these specific aircraft within Australia's jurisdiction. The legislation extends its reach to ensure compliance with the stated directives, without any specified exclusions or exemptions within the provided excerpt, thus maintaining stringent safety standards for the operation of these aircraft.
Key Provisions
The Civil Aviation Safety Authority (CASA) has issued an Airworthiness Directive (AD) concerning Cessna 500 (Citation) series aeroplanes, specifically model 500 with serial numbers 500-0001 to 500-0239. This AD, identified as AD/CESSNA 500/12, pertains to the modification of the glideslope interlock (Section 1). This modification is intended to address potential safety issues and ensure the continued airworthiness of the affected aircraft (Section 2). Compliance with this directive is required within 100 hours of time in service after 30 September 1975, and the specific instructions can be found in Cessna Citation Service Bulletin 34-27 (Section 3).
The AD imposes specific obligations on the operators and owners of the affected aircraft. They must ensure that the required modifications to the glideslope interlock are carried out by qualified personnel within the specified timeframe (Section 4). Additionally, operators must document the compliance process, including the completion of the modifications, in the aircraft's maintenance records (Section 5). Failure to comply with these requirements may result in the aircraft being deemed unairworthy and potentially grounded.
Failure to comply with the AD may lead to civil and criminal consequences. Civil penalties can include fines up to a maximum of $27,500 for individuals and $137,500 for corporations, as stipulated under the Civil Aviation Act 1988 (Section 6). Furthermore, operators who fail to comply may face criminal charges, with potential imprisonment for up to two years for individuals and a fine of up to $110,000 for corporations (Section 7). These severe penalties underscore the importance of adhering to the AD to ensure the safety and compliance of the affected aircraft.