COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 36 (Bonanza) Series Aeroplanes
AD/BEECH 36/18
Amdt 1
Landing Gear Shock Strut Position 1/74
Applicability: All model A36 with S/Nos. E-425 to E-475 except E-431. Requirement: Action in accordance with Beechcraft SI No. 612-200.
Compliance: Within 100 hours time in service after 31 January 1974 unless already accomplished.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve to govern civil aviation safety across the country, ensuring that aviation practices and aircraft maintain high safety standards. This legislative instrument, specifically addressing Part 39 - 105, focuses on the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives for certain aircraft types. One such directive pertains to Beechcraft 36 (Bonanza) Series Aeroplanes, aiming to rectify specific safety concerns through mandatory compliance. The policy objective is to enhance aviation safety by mandating corrective actions for identified issues, thus mitigating risks associated with aircraft operation.
The particular airworthiness directive AD/BEECH 36/18 Amendment 1 concerns the landing gear shock strut position for model A36 aircraft with specific serial numbers. The directive requires compliance with Beechcraft Service Information No. 612-200, which must be achieved within 100 hours of time in service following 31 January 1974, unless the action has already been taken. This measure was introduced to address identified safety issues, ensuring the continued airworthiness and safe operation of the specified aircraft fleet.
Scope and Application
The Civil Aviation Safety Authority's Airworthiness Directives under the Civil Aviation Regulations 1998, specifically PART 39 - 105, address the maintenance and operational safety of specific aircraft models. This particular directive, AD/BEECH 36/18 Amendment 1, pertains to the Beechcraft 36 (Bonanza) Series Aeroplanes, focusing on the landing gear shock strut position. The directive applies to all model A36 aircraft with serial numbers ranging from E-425 to E-475, with the exception of serial number E-431. Compliance with this directive is mandatory and must be achieved within 100 hours of time in service following 31 January 1974, unless the required action has already been completed. The directive mandates adherence to Beechcraft Service Instruction No. 612-200 to ensure the airworthiness of the specified aircraft. The scope of this legislation is clearly defined to ensure that the designated aircraft models maintain their airworthiness according to the outlined requirements and timeframes.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39 - 105, mandates the issue of Airworthiness Directives (AD) to ensure the safety and airworthiness of aircraft. In this context, AD/BEECH 36/18 Amendment 1 pertains to the Beechcraft 36 (Bonanza) Series Aeroplanes, specifically those with serial numbers E-425 to E-475, excluding serial number E-431. The directive requires action in accordance with Beechcraft Service Information No. 612-200, which addresses the landing gear shock strut position (section 1/74). This action must be taken within 100 hours of time in service after 31 January 1974, unless the requirement has already been met.
The obligations imposed by this AD are clear and direct. Aircraft operators must ensure that the specified action regarding the landing gear shock strut position is carried out in accordance with the provided service information. The directive stipulates a timeframe of 100 hours of service following the specified date, which is 31 January 1974, unless the action has already been completed. Compliance with these requirements is essential to maintaining the airworthiness of the affected Beechcraft 36 aeroplanes.
Failure to comply with the AD/BEECH 36/18 Amendment 1 could lead to serious safety implications and potential regulatory consequences. The Civil Aviation Safety Authority (CASA) enforces these directives rigorously, and non-compliance can result in the grounding of the aircraft until the required action is taken. While the specific penalties for non-compliance are not detailed within the AD itself, CASA has the authority to impose fines, issue enforcement notices, or take other regulatory actions under the Civil Aviation Act 1988. These actions are intended to ensure that aircraft remain in a safe and airworthy condition, protecting both the operators and the public.