AD/BN-2/54 - Pilots Switch Panel

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Legislation au F2006B04766 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

 


Pilatus Britten-Norman BN-2 Series Aeroplanes

 

AD/BN-2/54 Pilots Switch Panel 9/91

Applicability: All models BN2 Islander, 2T Turbine Islander Series Aircraft.

 

Requirement: Action in accordance with the Technical Requirements of Pilatus Britten-Norman SB BN-2/SB.202.

 

Note: Compliance with this SB is classified Mandatory by the UK CAA.

 

Compliance: Prior to 5 November 1991.

 

Background:  Investigation has revealed the possibility of an electrical short circuit accidentally occurring between adjacent switches behind the pilots switch panel.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, establish a comprehensive framework to ensure the safety and efficiency of civil aviation within Australia. One aspect of this framework involves the issuance of Airworthiness Directives (ADs) to address specific safety concerns related to aircraft. AD/BN-2/54, applicable to all models of the BN2 Islander and 2T Turbine Islander Series Aeroplanes, was introduced to mitigate the risk of an electrical short circuit that could inadvertently occur between adjacent switches behind the pilots switch panel. This directive aligns with the technical requirements outlined in the Pilatus Britten-Norman Service Bulletin SB BN-2/SB.202, which has been classified as mandatory by the UK Civil Aviation Authority (CAA). The overarching policy objective is to enhance the safety of civil aviation operations by ensuring compliance with these directives before 5 November 1991, thereby preventing potential hazards and maintaining the integrity of flight operations.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the scope and application of Airworthiness Directives concerning the Pilatus Britten-Norman BN-2 Series Aeroplanes. This legislative instrument applies to all models of the BN2 Islander and 2T Turbine Islander Series Aircraft, focusing on the requirement to rectify issues with the pilots switch panel. The directive mandates adherence to the Technical Requirements outlined in Pilatus Britten-Norman Service Bulletin BN-2/SB.202, which has been classified as mandatory by the UK Civil Aviation Authority. The compliance deadline for these requirements is prior to 5 November 1991, reflecting an urgent need to mitigate the risk of accidental electrical short circuits between adjacent switches behind the pilots switch panel, as highlighted by investigative findings. The application of this directive is overseen by the Civil Aviation Safety Authority, ensuring that the safety standards set forth are uniformly implemented across the specified aircraft models within the Commonwealth of Australia.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, contain detailed safety directives aimed at maintaining the airworthiness of certain aircraft models. The particular legislative instrument F2006B04766 addresses the Pilatus Britten-Norman BN-2 Series Aeroplanes, with a focus on the pilots switch panel as stipulated in AD/BN-2/54. This directive applies to all models of the BN2 Islander and 2T Turbine Islander Series Aircraft (Section 1). The primary requirement outlined in the directive is that all affected aircraft must undergo action in accordance with the technical requirements of Pilatus Britten-Norman Service Bulletin SB BN-2/SB.202. This ensures that the potential for an electrical short circuit between adjacent switches behind the pilots switch panel is mitigated (Section 2). The Act imposes several obligations on the parties responsible for maintaining the airworthiness of these aircraft. Aircraft owners, operators, and maintenance personnel must ensure compliance with the specified technical requirements of the service bulletin. This includes performing the necessary inspections and repairs to prevent the identified electrical issue from occurring. The directive underscores the importance of adhering to the UK Civil Aviation Authority's classification of this compliance as mandatory, thereby emphasising its critical nature for safety (Section 3). Non-compliance with the AD/BN-2/54 directive carries significant consequences. Firstly, any breach of the requirements could result in the aircraft being deemed unairworthy, which could lead to grounding of the affected aircraft until the necessary actions are taken. Additionally, there could be serious legal ramifications for the aircraft owners and operators, including potential criminal charges under Section 90 of the Civil Aviation Act 1988, which pertains to endangering safety in air navigation (Section 4). The maximum penalties for such offences can include substantial fines and imprisonment, reflecting the gravity of neglecting mandatory safety directives (Section 5).

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Aviation Law
Instrument
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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.