AD/BEECH 95/9 Amdt 2 - Control Wheel Adaptor

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Legislation au F2006B04310 In force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Beechcraft 95 (Travelair) Series Aeroplanes

 

AD/BEECH 95/9

Amdt 2

Applicability: All models.


Control Wheel Adaptor 8/72

 

Requirement: Action in accordance with Beechcraft SI No 0254-156, Rev IV. Compliance:  Within 100 hours’ time in service after 31 August 1972.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, form a comprehensive framework governing civil aviation in Australia. One specific legislative instrument under this regulation, F2006B04310, pertains to airworthiness directives for particular aircraft types. This instrument, issued by the Civil Aviation Safety Authority (CASA), aims to ensure the safe operation of aircraft by mandating compliance with specific maintenance and operational standards. The Beechcraft 95 (Travelair) Series Aeroplanes AD/BEECH 95/9 Amendment 2, for instance, addresses the requirement for control wheel adaptors, stipulating adherence to Beechcraft Service Instruction No 0254-156, Revision IV. This directive mandates compliance within 100 hours’ time in service after 31 August 1972, reflecting the policy objective of maintaining stringent safety standards and minimising risks associated with aircraft operations.

Scope and Application

The Civil Aviation Regulations 1998, as amended, specifically under Part 39 - 105, govern the airworthiness directives for various aircraft, including Beechcraft 95 (Travelair) Series Aeroplanes. This legislation applies to all models of the Beechcraft 95 series and mandates compliance with the action specified in Beechcraft Service Information No 0254-156, Rev IV, concerning the control wheel adaptor. The directive requires that this action must be completed within 100 hours’ time in service following 31 August 1972, ensuring that the aircraft maintain the required safety standards. The scope of this regulation is limited to the specified aircraft model and the particular modification noted, and it applies across the Commonwealth of Australia, ensuring a consistent standard of airworthiness throughout the country. No specific exclusions or exemptions are stated within the directive itself, though the application and enforcement might be subject to the broader regulatory framework under which these regulations operate.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998 (CAR) concerning the Beechcraft 95 (Travelair) Series Aeroplanes require adherence to specific airworthiness directives. Notably, AD/BEECH 95/9 Amendment 2 pertains to the control wheel adaptor. Section 39-105 of the CAR mandates that all models of the Beechcraft 95 series must comply with the requirements set forth in Beechcraft Service Instruction (SI) No 0254-156, Revision IV. The directive necessitates action to be taken within 100 hours of time in service after 31 August 1972. This ensures that the control wheel adaptor is appropriately modified or inspected to meet the specified safety standards. The obligations imposed by this legislation on the parties or entities it governs are clear and specific. Operators of Beechcraft 95 series aeroplanes must ensure that the control wheel adaptor is modified or inspected within the stipulated timeframe. This involves following the detailed procedures outlined in the referenced Beechcraft SI No 0254-156, Revision IV. Compliance must be verified and documented to demonstrate adherence to the safety directive, which is crucial for maintaining the airworthiness of the aircraft. Additionally, maintenance personnel must be adequately trained to perform the required modifications or inspections to the standard expected by the Civil Aviation Safety Authority (CASA). Failure to comply with the requirements set out in the airworthiness directives can lead to serious consequences. Under the CAR, non-compliance with airworthiness directives may result in various civil and criminal penalties. The Civil Aviation Act 1988 provides for substantial fines and potential imprisonment for those who breach these regulations. For instance, individuals found guilty of not adhering to the airworthiness directives can face fines of up to $22,200 and/or imprisonment for up to two years. Furthermore, the operator of the aircraft may also face fines of up to $222,000. These penalties underscore the importance of strict compliance with the provisions outlined in the CAR to ensure the safety and integrity of civil aviation operations in Australia.

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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.