AD/BEECH 35/47 - Turbocharger Wastegate

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Legislation au F2006B03843 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 35 (Bonanza) Series Aeroplanes

 

AD/BEECH 35/47 Turbocharger Wastegate 6/75

Applicability: All model V35TC, V35A-TC and V35B-TC with S/Nos. as listed in Beechcraft SI No. 0710-245, also all model S35, V35, V35A and V35B fitted with Continental TSIO-520-D engines in accordance with STC SA 1035 WE or Beech Drawing No. 35-010023.

 

Requirement: Action in accordance with Beechcraft SI No. 0710-245.

 

Note: FAA AD 75-01-07 refers.

 

Compliance: Within 100 hours time in service after 30 June 1975.

 

Overview

The Civil Aviation Regulations 1998, amended by the legislative instrument F2006B03843, are designed to ensure the safety and airworthiness of civil aircraft within Australian airspace. This particular legislative instrument, issued by the Civil Aviation Safety Authority (CASA), addresses the safety concerns associated with the turbocharger wastegate in Beechcraft 35 (Bonanza) series aeroplanes, particularly those equipped with specific engine models. The policy objective behind this directive is to mitigate the risks associated with turbocharger malfunction, which can lead to significant engine performance issues and potentially dangerous flight conditions. Compliance with this regulation is mandatory for all specified aircraft models and engine types, and requires corrective actions to be taken within 100 hours of the aircraft being in service after 30 June 1975, as outlined in the referenced Beechcraft Service Information (SI) number 0710-245. This directive aligns with similar measures taken by the Federal Aviation Administration (FAA) in the United States, as indicated by FAA AD 75-01-07.

Scope and Application

The Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically AD/BEECH 35/47 concerning the turbocharger wastegate of Beechcraft 35 (Bonanza) Series Aeroplanes, applies to all model V35TC, V35A-TC, and V35B-TC aircraft with serial numbers as listed in Beechcraft Service Instruction No. 0710-245, as well as to all model S35, V35, V35A, and V35B aircraft fitted with Continental TSIO-520-D engines as per STC SA 1035 WE or Beech Drawing No. 35-010023. This directive mandates compliance with the actions outlined in Beechcraft Service Instruction No. 0710-245, referencing the Federal Aviation Administration's AD 75-01-07. The requirement is to implement the specified action within 100 hours of the aircraft being in service after 30 June 1975. The scope of this directive is confined to the particular models and serial numbers of Beechcraft 35 (Bonanza) Series aeroplanes as defined, and it does not extend to other aircraft types or models unless explicitly stated.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, specifically in Part 39 - 105 concerning the Civil Aviation Safety Authority's Schedule of Airworthiness Directives for the Beechcraft 35 (Bonanza) Series Aeroplanes, require compliance with the specified action outlined in Beechcraft Service Instruction (SI) No. 0710-245 (section 1). This applies to all model V35TC, V35A-TC, and V35B-TC with specific serial numbers listed in the service instruction, as well as all models S35, V35, V35A, and V35B fitted with Continental TSIO-520-D engines in accordance with Supplemental Type Certificate (STC) SA 1035 WE or Beech Drawing No. 35-010023. The directive mandates that the action must be completed within 100 hours of time in service after 30 June 1975. The Act imposes specific obligations on the parties or entities it governs. Aircraft operators must ensure that their Beechcraft 35 (Bonanza) Series Aeroplanes meet the requirements stipulated in the directive. This involves adhering to the detailed instructions provided in Beechcraft SI No. 0710-245, which may include inspections, repairs, or modifications to the turbocharger wastegate. Compliance with these requirements is critical to maintaining the airworthiness of the aircraft and ensuring the safety of all passengers and crew onboard. Failure to comply with the airworthiness directives set out in the Civil Aviation Regulations 1998 can lead to serious consequences. If an operator does not adhere to the specified actions within the required timeframe, they may face enforcement actions from the Civil Aviation Safety Authority (CASA). These actions could include fines, penalties, or even the grounding of the affected aircraft until the required compliance is achieved. The exact penalties for non-compliance are not specified in the directive but can be severe under aviation safety regulations. In terms of potential criminal and civil consequences, non-compliance with airworthiness directives can result in significant legal ramifications. Criminal charges may be brought against individuals or companies responsible for the oversight of the aircraft, potentially leading to imprisonment or substantial fines. Civil liabilities could also arise, with operators facing compensation claims from affected parties in the event of accidents or incidents resulting from non-compliance. The directive refers to FAA AD 75-01-07, indicating that the requirements and standards set forth are consistent with those established by the Federal Aviation Administration in the United States. This cross-reference ensures that the regulations align with international safety standards, providing a unified approach to maintaining airworthiness across jurisdictions. The adherence to these directives is essential for ensuring the safety and reliability of Beechcraft 35 (Bonanza) Series Aeroplanes in operation.

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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.