AD/AC/8 - Power Brake Valve - Modification

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Legislation au F2006B02140 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes

 

AD/AC/8 Power Brake Valve - Modification NK

Applicability: All models: /Nos. 75, 91 to 650 and all other employing nose wheel steering. Document:              Aero Commander SB No. 48.

Compliance: Forthwith.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve as a crucial framework for ensuring the safety and efficiency of civil aviation in the country. One such legislative instrument, F2006B02140, pertains specifically to the safety of certain models of twin commander aeroplanes, namely the Gulfstream/Rockwell/Aerocommander 500, 600, and 700 series. This legislative instrument was introduced to address specific safety concerns related to the power brake valve in these aircraft, particularly those employing nose wheel steering. The overarching objective is to mandate modifications to enhance the operational safety of these aeroplanes, ensuring they meet the stringent safety standards set by the Civil Aviation Safety Authority (CASA). This directive is part of a broader schedule of airworthiness directives aimed at maintaining high safety standards within the Australian civil aviation sector.

Scope and Application

The Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, specifically Part 39 - 105 of the Civil Aviation Regulations 1998, applies to all Twin Commander (Gulfstream/Rockwell/Aerocommander 500, 600, and 700) series aeroplanes, including all models and serial numbers from 75, 91 to 650, as well as any other aircraft that use nose wheel steering. This directive mandates a modification to the power brake valve to ensure compliance with the standards set by Aero Commander Service Bulletin No. 48. The directive requires immediate action, stipulating that the compliance must be achieved forthwith. The directive is applicable across the Commonwealth of Australia, and while it does not specify exclusions or exemptions, its scope is clearly defined by the specified aircraft models and serial numbers. The directive's application can be extended or further detailed through subordinate instruments, ensuring the ongoing safety and regulatory compliance of the affected aircraft.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, encompasses a Schedule of Airworthiness Directives (ADs) that mandate certain modifications and compliance measures for aircraft types to ensure safety and operational standards. One such directive is AD/AC/8, which pertains to the Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600, and 700) series aeroplanes. Section 39.105 requires the modification of the power brake valve for these aircraft models, particularly for those employing nose wheel steering. This modification is to be carried out in accordance with Aero Commander Service Bulletin No. 48. The directive stipulates that compliance must be immediate, referred to as "forthwith" in the regulation. The obligations under this AD impose a clear requirement on the operators and owners of Twin Commander aircraft to ensure that the specified modification to the power brake valve is completed without delay. This involves following the detailed instructions provided in Aero Commander Service Bulletin No. 48, which is recognised as the authoritative document for this modification. Operators must conduct the modification and verify that it has been correctly and thoroughly implemented before continuing with flights. The regulation's immediate compliance directive underscores the importance of the modification for safety reasons, making it a non-negotiable requirement. Failure to comply with the provisions of AD/AC/8 can result in serious legal consequences. The Civil Aviation Regulations 1998 do not specify exact penalties within this particular directive, but non-compliance with airworthiness directives generally can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions may include grounding of the aircraft, fines, or more severe penalties if the non-compliance results in an incident or accident. The potential criminal or civil liabilities for operators who fail to adhere to airworthiness directives can be substantial, reflecting the high stakes involved in ensuring aircraft safety.

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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.