COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 56TC (Turbo Baron) Series Aeroplanes
AD/BEECH 56/6 Centre Section Rear Spar Jack Pad 5/69
Applicability: Model 56TC with S/No. TG1 to TG69.
Requirement: Action in accordance with Beechcraft SI No. 0064-067, Rev. 1.
Compliance: Within 200 hours’ time in service or before 1 August 1969 whichever occurs first.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, provide the legal framework governing all aspects of civil aviation within the country. The regulations address a broad range of issues, from the licensing of pilots and airworthiness of aircraft to air traffic control and the operation of aerodromes. Specifically, Part 39, which includes the Airworthiness Directives, is designed to ensure that aircraft maintain their airworthiness through adherence to specified safety standards and mandatory corrective actions. One such directive, AD/BEECH 56/6, pertains to the Beechcraft 56TC (Turbo Baron) Series Aeroplanes and mandates specific actions for maintaining the structural integrity of the centre section rear spar jack pad, with the aim of enhancing flight safety and preventing potential structural failures.
This legislative instrument is a response to identified safety concerns and aims to provide clear and enforceable standards to mitigate risks associated with civil aviation. The policy objective is to ensure the highest level of safety in the operation of aircraft, thereby protecting the public and maintaining the integrity of the national airspace system.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates the applicability of the Civil Aviation Safety Authority's Airworthiness Directives to ensure the safe operation of aircraft within Australia. The regulation targets Beechcraft 56TC (Turbo Baron) Series aeroplanes, specifically those with serial numbers ranging from TG1 to TG69. This directive is imperative for these aircraft to comply with Beechcraft Service Instruction No. 0064-067, Revision 1, which addresses modifications to the centre section rear spar jack pad. The requirement necessitates that the specified action be completed within 200 hours of time in service or before 1 August 1969, whichever is sooner. The directive is applicable nationally across Australia, enforcing stringent safety standards to mitigate risks associated with the specified structural component. The regulation does not explicitly mention any exclusions, exemptions, or thresholds beyond the stipulated timeframe and serial number range, thereby ensuring uniformity in compliance across the affected fleet.
Key Provisions
The Civil Aviation Regulations 1998, specifically under PART 39 - 105, establish the schedule of airworthiness directives which include AD/BEECH 56/6 concerning the Beechcraft 56TC (Turbo Baron) Series Aeroplanes. Section 105 of this legislation mandates that for the Model 56TC with serial numbers ranging from TG1 to TG69, the centre section rear spar jack pad must be addressed according to Beechcraft Service Instruction No. 0064-067, Revision 1. Compliance with this directive is required within 200 hours of the aircraft's time in service or before 1 August 1969, whichever comes first. This directive is pivotal for ensuring the structural integrity and operational safety of the specified aircraft models.
The obligations imposed by the Civil Aviation Regulations 1998 on the relevant parties, particularly the aircraft operators, are to ensure that the necessary modifications or checks on the centre section rear spar jack pad are completed as per the outlined Beechcraft Service Instruction. This involves adherence to the specified timeline and the requirement to act within 200 hours of the aircraft's service time or before the specified date of 1 August 1969. Failure to comply with these directives can lead to serious consequences, as the safety and airworthiness of the aircraft are paramount concerns regulated by these provisions.
In the event of non-compliance with the airworthiness directive AD/BEECH 56/6, there are potential civil and criminal consequences that can be imposed. The exact penalties are not specified in the text, but typically, breaches of civil aviation regulations can lead to fines, enforcement actions, and potentially more severe penalties if the breach results in an aviation incident or accident. The specific nature and severity of the penalties would be determined by the Civil Aviation Safety Authority based on the circumstances of the breach and its impact on aviation safety. It is important for operators to ensure full compliance to avoid these potential repercussions.