AD/BEECH 36/27 Amdt 1 - Flight Controls

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Legislation au F2006B03881 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 36 (Bonanza) Series Aeroplanes

 

AD/BEECH 36/27

Amdt 1


Flight Controls 1/79

 

Applicability: All models A36 with S/Nos. E323 and E441 to E954; and all 36 series fitted with rudder and/or elevators shipped from Beech during the period 1 May 1973 and

1 July 1976.

 

Requirement: Action in accordance with Beechcraft SI No. 0629-150, Rev. II.

 

Compliance: Unless already accomplished, within 100 hours time in service after 31 January 1979.

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, were designed to regulate and ensure the safety and efficiency of civil aviation within the country. This legislative instrument addresses the need for consistent and stringent safety standards in the aviation industry, aiming to protect passengers, crew, and the general public from potential hazards. One of the amendments, the AD/BEECH 36/27 Amendment 1, specifically targets the Beechcraft 36 (Bonanza) series aeroplanes, addressing a gap in safety protocols related to flight control components. The policy objective is to ensure that these aircraft meet required safety standards by mandating specific actions, such as those outlined in Beechcraft Service Instruction No. 0629-150, Revision II, to be completed within a stipulated timeframe. This amendment aims to mitigate risks associated with identified flight control issues in certain models of the Beechcraft 36 series, thereby enhancing overall aviation safety.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, applies to Beechcraft 36 (Bonanza) Series Aeroplanes. This legislation is applicable to all models A36 with serial numbers ranging from E323 and E441 to E954, as well as all 36 series aircraft fitted with rudder and/or elevators shipped from Beech during the period 1 May 1973 and 1 July 1976. The directive mandates actions in accordance with Beechcraft Service Information No. 0629-150, Revision II. Compliance is required unless the specified actions have already been carried out, within 100 hours of time in service following 31 January 1979. This regulation extends across the Commonwealth of Australia, governing the maintenance and safety standards of the specified aircraft models within the national jurisdiction. The legislation does not specify any exclusions, exemptions, or thresholds, but it may be supplemented or further detailed through subordinate instruments issued by the Civil Aviation Safety Authority.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, detail the Airworthiness Directives for various aircraft, including the Beechcraft 36 (Bonanza) Series Aeroplanes. The directive AD/BEECH 36/27 Amendment 1, issued on 1 July 1979, pertains to the flight controls of certain Beechcraft 36 models (section 1). It applies to all models A36 with serial numbers (S/Nos.) E323 and E441 to E954, as well as to all 36 series aeroplanes equipped with rudders and/or elevators shipped from Beech during the period from 1 May 1973 to 1 July 1976. The directive requires compliance with Beechcraft Service Instruction No. 0629-150, Revision II (section 1). This means that the specified aircraft must undergo specific actions as outlined in the service instruction to ensure continued airworthiness. The compliance period for these actions is set within 100 hours of time in service after 31 January 1979, unless the actions have already been completed (section 3). Entities governed by this directive must ensure that the specified maintenance and inspection actions are carried out within the stipulated timeframe. This involves adhering to the detailed procedures laid out in the Beechcraft service instruction, which may include inspections, repairs, or modifications to the flight control components. It is crucial for operators of these aircraft to keep accurate records of when these actions were performed to demonstrate compliance with the regulation. Failure to comply with the requirements of this Airworthiness Directive can result in serious consequences. The Civil Aviation Safety Authority (CASA) may take enforcement actions against non-compliant aircraft or operators. This could include grounding of the aircraft, fines, or other penalties as determined by CASA. The exact penalties are not specified in the directive itself but are outlined in the broader Civil Aviation Regulations, which may include significant financial penalties and legal repercussions for non-compliance.

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Administrative Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
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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.