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 65/11 Alternator Field Circuit Breaker - Inspection
and Relocation
4/68
Applicability: Models 65 and A65 with S/Nos. LC-143 to LC-270, except LC-243, that are equipped with alternators. Models 65-80, 65-A80 & 65-B80 with S/Nos. LD-13 to LD-350 & LD-352, that are equipped with alternators. Model 65-80 prior to S/Nos. LD-13 that have complied with Model 65-80 SB No. 2.
Document: Beechcraft SB No. 67-28. Compliance: Before 1 June 1968.
Overview
The Civil Aviation Regulations 1998 (Cth), specifically under Part 39 - 105, were enacted to establish and maintain safety standards within the civil aviation sector in Australia. This regulation was introduced to address the need for consistent and rigorous safety protocols to protect the public, ensure the safe operation of aircraft, and maintain the integrity of the civil aviation system. The policy objective of this legislation is to ensure that all aircraft, operators, and personnel meet the highest standards of safety and reliability, thereby preventing accidents and enhancing the overall safety of air travel. Enacted by the Commonwealth Parliament, these regulations are overseen by the Civil Aviation Safety Authority (CASA) to ensure compliance and enforce safety directives.
One particular directive, AD/BEECH 65/11, pertains to the inspection and relocation of the alternator field circuit breaker in specific models of Beechcraft 65 and 70 (Queen Air) series aeroplanes. This directive applies to certain serial numbers and model variations equipped with alternators, aiming to address potential safety risks associated with the alternator field circuit breaker. The directive mandates compliance before 1 June 1968, as outlined in Beechcraft Service Bulletin No. 67-28. The enactment of such directives under the Civil Aviation Regulations 1998 (Cth) ensures that aircraft meet necessary safety standards, ultimately contributing to the overarching goal of maintaining high safety levels within Australia's civil aviation framework.
Scope and Application
The Civil Aviation Regulations 1998, as amended by the Legislative Instrument F2006B04116, apply to specific models of Beechcraft 65 and 70 (Queen Air) Series Aeroplanes, focusing on the inspection and relocation of the alternator field circuit breaker as detailed in Airworthiness Directive AD/BEECH 65/11. This legislation mandates that models 65 and A65 with serial numbers (S/Nos.) ranging from LC-143 to LC-270, excluding LC-243, and models 65-80, 65-A80, and 65-B80 with S/Nos. from LD-13 to LD-350 and LD-352, all of which are equipped with alternators, must adhere to the specified directive. Moreover, the directive also applies to Model 65-80 aircraft prior to S/Nos. LD-13 that have complied with Model 65-80 Service Bulletin No. 2. This requirement is to be completed in accordance with Beechcraft Service Bulletin No. 67-28, with compliance necessary before 1 June 1968. The regulation is specifically targeted at ensuring the safety and airworthiness of these particular aircraft models within the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes the Airworthiness Directives (AD) issued by the Civil Aviation Safety Authority (CASA). This section pertains to the Beechcraft 65 and 70 (Queen Air) Series Aeroplanes, particularly focusing on the AD/BEECH 65/11 which mandates the inspection and relocation of the alternator field circuit breaker. This directive applies to certain models of the Beechcraft 65 and A65 series, specifically those with serial numbers within the specified ranges, and models 65-80, 65-A80, and 65-B80 with certain serial numbers, provided they are equipped with alternators (Section 105.4/68).
Under these regulations, the key requirement is for the inspection and, if necessary, the relocation of the alternator field circuit breaker as detailed in Beechcraft Service Bulletin No. 67-28. Compliance with this directive must be achieved before 1 June 1968. This inspection and relocation ensure that the electrical system's safety and reliability are maintained, preventing potential malfunctions that could compromise flight safety. The directive is aimed at addressing specific technical issues identified with the alternator field circuit breaker in the specified models, thus ensuring continued airworthiness.
The obligations imposed by this directive are stringent. Operators and owners of the affected aircraft models must ensure that the inspection and necessary modifications are performed by qualified personnel in accordance with the specifications outlined in Beechcraft SB No. 67-28. Documentation of compliance must be maintained, and it is the operator's responsibility to verify that the aircraft meets the airworthiness standards set forth by CASA. Failure to comply with the directive can result in severe consequences.
Breach of the requirements stipulated in AD/BEECH 65/11 can lead to serious legal and operational repercussions. Under the Civil Aviation Act 1988, non-compliance can be considered an offence. The penalties for such breaches may include substantial fines and, in severe cases, imprisonment. Specifically, the maximum penalty for an individual found guilty of contravening an airworthiness directive can be up to $210,000 and/or imprisonment for up to five years, while corporations may face even higher fines, up to $1,050,000. These severe penalties underscore the importance of strict adherence to CASA's directives to ensure the safety and integrity of civil aviation operations.