COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 65 and 70 (Queen Air) Series Aeroplanes
AD/BEECH 65/33
Amdt 1
Placard - Emergency Engine Shut-Down Procedure
3/89
Applicability: Model 65 with S/Nos L-1, L-2, L-6, LF-7, LF-8 and LC-1 to LC-239.
Model A65 & A65-8200 with S/Nos LC-240 to LC-335.
Models 65-80, 65-A80, 65-A80-8800 and 65-B80 with S/Nos LD-1 to LD-456.
Model 65-88 with S/Nos LP-1 to LP-47. Model 70 with S/Nos LB-1 through LB-35.
Requirement: Action in accordance with Beechcraft SI No 0509-016. Compliance: Within 25 hours’ time in service after 23 August 1972. Background: Amendment 1 consolidates Queen Air series 65 and 70 Aircraft.
Overview
The Civil Aviation Regulations 1998, specifically in Part 39 - 105 under the Civil Aviation Safety Authority's schedule of airworthiness directives, was enacted to ensure the safe operation of aircraft within Australian airspace. This legislative instrument addresses the need for stringent compliance with airworthiness directives to maintain safety standards for aircraft operations. The regulations are enforced by the Civil Aviation Safety Authority, whose policy objective is to ensure the safety and efficiency of civil aviation in Australia. This particular directive, AD/BEECH 65/33 Amendment 1, pertains to the Beechcraft 65 and 70 series aeroplanes, requiring action in accordance with specific maintenance instructions to ensure safe engine operation, thereby addressing potential safety gaps associated with these aircraft models.
The regulations are enacted by the Australian Parliament and are designed to provide a comprehensive framework for the regulation of civil aviation in Australia, ensuring that all aircraft meet the necessary safety standards before being allowed to operate.
Scope and Application
The Civil Aviation Regulations 1998, specifically PART 39 - 105, includes an Airworthiness Directive concerning Beechcraft 65 and 70 (Queen Air) Series Aeroplanes, applicable to particular serial numbers of these models. This regulation applies to specific serial numbers within the Beechcraft 65 series, including models with serial numbers L-1 through LB-35, and mandates compliance with Beechcraft Service Instruction No. 0509-016. The directive requires action to be taken within 25 hours’ time in service after 23 August 1972. The scope of this regulation is limited to these identified serial numbers and does not extend to other aircraft models or serial numbers not specified. The directive is applicable nationwide and is enforced by the Civil Aviation Safety Authority, ensuring that the specified Beechcraft aircraft meet the required safety standards.
Key Provisions
The Civil Aviation Regulations 1998, specifically within Part 39 and under the schedule of Airworthiness Directives, includes provisions for the Beechcraft 65 and 70 (Queen Air) Series Aeroplanes. The directive AD/BEECH 65/33 Amendment 1, dated 3 August 1989, mandates the placement of a placard detailing the emergency engine shut-down procedure. This directive applies to specific serial numbers of the Model 65 and Model 70 aircraft, as listed within the applicability section of the legislation. The action required under this directive involves adhering to the instructions outlined in Beechcraft Service Information No 0509-016, with compliance necessary within 25 hours of the aircraft’s time in service after 23 August 1972.
The Act imposes obligations on the operators and owners of the specified Beechcraft 65 and 70 models. These parties must ensure that the emergency engine shut-down procedure placard is correctly installed as per the referenced service information. This requirement aims to maintain the safety and operational standards of the aircraft. Compliance with the directive involves meticulous adherence to the stipulated timelines and procedures, ensuring that the aircraft meets the regulatory standards set by the Civil Aviation Safety Authority. Operators must verify that the placard is visible and accessible to the crew at all times, and that the emergency procedure detailed in the placard is well understood by the operating personnel.
Failure to comply with the requirements outlined in AD/BEECH 65/33 Amendment 1 can result in significant legal consequences. Although the specific penalties are not detailed within the directive, non-compliance with airworthiness directives is generally considered a serious offence under the Civil Aviation Act 1988. Violations could lead to enforcement actions by the Civil Aviation Safety Authority, including fines, suspension or revocation of the aircraft’s operating certificate, and potential criminal charges if the non-compliance is deemed to have caused or contributed to an aviation accident or incident. It is essential for operators to rigorously follow the directive to avoid these severe repercussions and to uphold the safety and integrity of their operations.