COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 19, 23 and 24 Series Aeroplanes
AD/BEECH 23/12 Attachment of ADF Noise Suppressor Capacitor
6/67
Applicability: Model A23-24 with S/Nos. MA-2, 3, 5, 9, 11, 24, 29, 31, 32, 33, 35, 44, 61, 64, 66,
69, 71, 72, 76, 77, 81, 83, 89, 90, 102, 104, 105, 107, 108, 109, 111, 115,131 and 134.
Requirement: Action in accordance with Beechcraft SB No. 66-65. Compliance: Before 1 September 1971.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, were established to ensure the safety and efficiency of civil aviation within the country. This legislation includes specific directives aimed at maintaining airworthiness standards across all civil aviation activities. Part 39 of these regulations, which deals with airworthiness directives, was introduced to address potential safety issues by requiring aircraft owners and operators to comply with specific maintenance and modification requirements. One such directive is AD/BEECH 23/12, which pertains to the attachment of an ADF noise suppressor capacitor for certain models of Beechcraft aeroplanes, specifically those with serial numbers listed in the directive. This directive aims to ensure that these aircraft meet necessary safety standards by requiring compliance with specific manufacturer service bulletins.
The legislative instrument F2006B03730, specifically addressing the Beechcraft 19, 23, and 24 series aeroplanes, was introduced to enhance safety through the mandatory attachment of an ADF noise suppressor capacitor. This requirement is intended to mitigate specific operational risks associated with the aircraft's avionics. The policy objective behind this directive is to maintain the highest safety standards within Australia's civil aviation sector, ensuring that aircraft are operated in a manner that minimises potential hazards. Compliance with these directives is crucial for the continued airworthiness and operational safety of the affected aircraft.
Scope and Application
The Civil Aviation Regulations 1998, as detailed in Part 39 - 105 of the Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically targets the Beechcraft 19, 23, and 24 series aeroplanes. This legislation applies to the Model A23-24 with specific serial numbers listed within the directive AD/BEECH 23/12, which pertains to the attachment of the ADF Noise Suppressor Capacitor. The regulation mandates compliance with Beechcraft Service Bulletin No. 66-65, and requires that the specified action be completed prior to 1 September 1971. This directive is binding on the operators and owners of the affected aircraft, ensuring that safety standards are adhered to within the Australian civil aviation sector. The jurisdictional reach of these regulations is governed by the Commonwealth of Australia, and the Civil Aviation Safety Authority enforces compliance across the national airspace. There are no stated exclusions or exemptions within this specific directive, and the application extends to the specified aircraft models and serial numbers only.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105, under the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, includes provisions that govern the airworthiness of certain aircraft models. One such directive, AD/BEECH 23/12, applies to Beechcraft 19, 23, and 24 series aeroplanes. This directive mandates that certain model A23-24 aircraft, identified by specific serial numbers, must have an attachment of an ADF (Automatic Direction Finder) Noise Suppressor Capacitor (Section 39-105). This requirement is outlined in Beechcraft Service Bulletin No. 66-65, and compliance must be achieved before 1 September 1971.
The obligations imposed by this directive are clear and direct. Aircraft operators and owners of the specified Beechcraft A23-24 models must ensure that the ADF Noise Suppressor Capacitor is correctly installed on their aircraft. This involves following the detailed instructions provided in the aforementioned Beechcraft Service Bulletin No. 66-65. Failure to comply with these instructions can result in the aircraft not meeting the required airworthiness standards set by CASA, potentially leading to regulatory issues or grounding of the aircraft.
In terms of consequences, non-compliance with the AD/BEECH 23/12 directive can result in significant penalties and repercussions. Under the Civil Aviation Regulations 1998, failure to adhere to an Airworthiness Directive can lead to both civil and criminal liabilities. Civil penalties may include fines and other regulatory actions enforced by CASA. If the non-compliance is deemed to have endangered safety, it can also lead to criminal charges, with potential penalties including substantial fines and imprisonment. The exact penalties depend on the severity of the non-compliance and any resultant harm or risk to aviation safety.