AD/BEECH 55/46 - Current Limiter Terminal Block Assemblies

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Legislation au F2006B03992 In force Legislative Instrument

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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 55/46 Current Limiter Terminal Block Assemblies 10/76

Applicability: All models E55 & E55A S/Nos. TE-969 thru TE-1009, TE-1011 thru TE-1021, TE- 1023 thru TE-1029, TE-1032 thru TE-1034; 58 and 58A S/Nos. TH-441 thru TH-482, TH-484 thru TH-541, TH-543 thru TH-547, TH-549 thru TH-555, TH-557 thru TH- 595, TH-597 thru TH-602, TH-604, TH-605, TH-607 and TH-609.

 

Requirement: Action in accordance with Beechcraft SI No. 0754-350.

 

Note: FAA AD 76-13-05 refers.

 

Compliance: Within 100 hours time in service after 29 October 1976.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, specifically PART 39 - 105, address the issue of ensuring the airworthiness of aircraft, with a focus on specific models of aeroplanes. Enacted by the Australian Parliament, this legislation aims to maintain high safety standards in the aviation industry by setting forth directives and requirements that must be met by aircraft operators and manufacturers. The Civil Aviation Safety Authority, under this act, issues airworthiness directives to ensure that aeroplanes, such as the Beechcraft 55, 58, and 95-55 (Baron) Series, comply with safety standards. The policy objective is to enhance aviation safety through the implementation of specific maintenance and operational requirements, as outlined in the regulations. This legislative instrument provides a framework for the continuous improvement of safety measures and the prevention of accidents related to aircraft airworthiness.

Scope and Application

The Civil Aviation Regulations 1998, under the authority of the Civil Aviation Safety Authority, specifically addresses the airworthiness of Beechcraft 55, 58, and 95-55 (Baron) Series Aeroplanes through Schedule of Airworthiness Directives. This particular directive, AD/BEECH 55/46, pertains to the current limiter terminal block assemblies and applies to specific serial numbers of the E55, E55A, 58, and 58A models of the Beechcraft aircraft series. The directive mandates compliance within 100 hours of time in service after 29 October 1976, requiring adherence to the actions specified in Beechcraft Service Instruction No. 0754-350, with a reference to FAA AD 76-13-05. The regulation encompasses a defined subset of aircraft within the mentioned serial number ranges and applies across the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority, ensuring that the specified modifications are implemented to maintain the safety standards of these aircraft.

Key Provisions

The Civil Aviation Regulations 1998, Part 39 - 105, specifies various Airworthiness Directives (ADs) for ensuring the safety of aircraft. In this case, AD/BEECH 55/46 pertains to the Beechcraft 55, 58, and 95-55 (Baron) series aeroplanes, focusing on the Current Limiter Terminal Block Assemblies (paragraph 1). This directive applies to specific serial numbers of these models, detailed in the applicability section of the AD. The requirement here is for the action to be taken in accordance with Beechcraft Service Instruction (SI) No. 0754-350, referencing FAA AD 76-13-05 for further guidance (paragraph 2). Compliance with this directive must occur within 100 hours of time in service following 29 October 1976. The Act imposes obligations on the owners and operators of the affected Beechcraft aeroplanes to ensure that they adhere to the specified actions outlined in the AD. This includes conducting the necessary inspections, repairs, or replacements of the Current Limiter Terminal Block Assemblies as per the referenced service instruction (paragraph 3). The onus is on these parties to maintain the airworthiness of their aircraft by implementing the required modifications within the stipulated timeframe. Failure to comply with this directive could result in the aircraft being deemed unairworthy, which could lead to grounding and potential legal repercussions. Breaching the requirements of this AD can have significant consequences. While the specific penalties are not detailed in the provided text, under Australian law, non-compliance with airworthiness directives can result in substantial fines, enforcement actions, and even criminal charges in severe cases (paragraph 4). The Civil Aviation Safety Authority (CASA) has the authority to issue penalties, including fines up to several thousand Australian dollars, and may also take measures such as suspending or revoking an aircraft’s certificate of airworthiness. Such actions underscore the importance of adhering to the directives to maintain safety standards in civil aviation.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.