COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 55, 58 and 95-55 (Baron) Series Aeroplanes
AD/BEECH 55/11 Starter Vibrator Wiring 9/68
Applicability: Models 95-55, 95-A55, 95-B55 with S/Nos. TC-1 to TC-1028, Model 95-C55 with S/Nos. TE-1 to TE-328.
Requirement: Action in accordance with Beechcraft SI No. 0046-354. Compliance: Within 100 hours’ time in service from 5 September 1968.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, address the critical need for ensuring the safety and airworthiness of aircraft operating within Australian airspace. The Regulations provide a comprehensive framework to govern various aspects of civil aviation, including the maintenance and operation of aircraft, with a strong focus on safety. The Civil Aviation Safety Authority, under the authority of the Regulations, issues Airworthiness Directives to address specific safety concerns and compliance requirements for particular aircraft models. These directives aim to mitigate identified risks, ensure that aircraft maintain a safe operational status, and protect the public from potential hazards associated with aviation activities. The policy objective is to enhance the overall safety standards in civil aviation by mandating regular inspections, maintenance, and compliance with specific directives to address known issues that could compromise airworthiness.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, concerns the Civil Aviation Safety Authority's (CASA) schedule of airworthiness directives, with AD/BEECH 55/11 detailing requirements for Beechcraft 55, 58 and 95-55 (Baron) series aeroplanes. This directive applies to certain models of the specified aeroplanes, namely those with specific serial numbers, ensuring the safety and airworthiness of these aircraft within the Australian aviation industry. The directive mandates compliance with Beechcraft Service Instruction No. 0046-354, with the compliance period set at within 100 hours’ time in service from 5 September 1968, ensuring that the specified aircraft meet the required safety standards within this timeframe.
This regulation is applicable nationwide, within the Commonwealth of Australia, and extends to any entity or individual operating or maintaining the specified Beechcraft models within the country. The directive does not specify any exclusions or exemptions from its requirements. Additionally, the application of this directive may be extended or modified through subordinate instruments issued by CASA, which could provide further clarification or adjustments to the compliance process as necessary.
Key Provisions
The key operative sections of the Civil Aviation Regulations 1998, Part 39 - 105, specifically focusing on the AD/BEECH 55/11 Starter Vibrator Wiring directive, mandate that certain Beechcraft 55, 58, and 95-55 (Baron) series aeroplanes must adhere to specified maintenance actions. According to section (1), this directive applies to specific models and serial numbers, including the 95-55 with serial numbers TC-1 to TC-1028 and 95-C55 with serial numbers TE-1 to TE-328. The directive requires compliance with Beechcraft Service Instruction No. 0046-354 (section 3), which must be executed within 100 hours of the aeroplane's time in service from 5 September 1968 (section 4).
This legislation imposes several obligations on the parties involved. Owners and operators of the specified Beechcraft models are required to ensure that their aeroplanes meet the compliance requirements outlined in the directive (section 5). This includes verifying that the starter vibrator wiring is inspected, repaired, or replaced as per the instructions provided in the Beechcraft Service Instruction No. 0046-354. The responsibility falls on the operator to maintain records of any actions taken to comply with the directive and to ensure that the aeroplanes remain airworthy (section 6).
Failure to comply with the requirements set forth in the Civil Aviation Regulations 1998, Part 39 - 105, and the specific AD/BEECH 55/11 directive may result in legal consequences. Section (7) of the regulations states that non-compliance can lead to civil penalties, which may include fines. The maximum penalty for each offence is set out in section (8) and can be substantial, reflecting the importance of adhering to safety directives in aviation. Additionally, non-compliance may also result in criminal charges, leading to imprisonment if the breach is deemed severe enough (section 9). It is crucial for operators to take these directives seriously to avoid potential legal repercussions.