AD/BN-2/79 - FHL Landing Gear Units

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Legislation au F2006B04792 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


AIRWORTHINESS DIRECTIVE


For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.


 

Pilatus Britten-Norman BN-2 Series Aeroplanes

 

AD/BN-2/79 FHL Landing Gear Units 10/2003 DM

 

Applicability: All BN2, BN2A, BN2B, BN2T, BN2T-4R, and BN2T-4S series Islander aircraft fitted with FHL Landing Gear.

 

Requirement: Action in accordance with B-N Group Limited Service Bulletin SB 298.

 

Compliance: As specified in the Requirement document, with a Requirement document effective date of 20 August 2003.

 

This Airworthiness Directive becomes effective on 13 August 2003.

 

Background: The UK CAA and FHL have determined that there is no method or procedure for recording the fatigue lives on FHL landing gear. This Directive introduces fatigue lives to landing gear and landing gear components.


David Villiers

Delegate of the Civil Aviation Safety Authority 7 August 2003

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 13 August 2003.

 

 


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Overview

The Civil Aviation Safety Regulations 1998 (CASR 1998) were enacted to regulate civil aviation safety in Australia, aiming to ensure the highest standards of airworthiness and operational safety in the aviation sector. One of the significant legislative instruments under this regulation is the Airworthiness Directive (AD) concerning the Pilatus Britten-Norman BN-2 Series Aeroplanes, specifically AD/BN-2/79, issued by the Civil Aviation Safety Authority (CASA) in 2003. This AD addresses the identified safety concern related to the FHL Landing Gear Units on BN-2 series Islander aircraft. The directive was introduced to correct an unsafe condition concerning the recording of fatigue lives on FHL landing gear, as determined by the UK Civil Aviation Authority and FHL. The policy objective of this AD is to mandate the implementation of specific actions as outlined in the requirement section to ensure compliance with the Service Bulletin SB 298, aiming to maintain the airworthiness and safety standards of the affected aircraft.

Scope and Application

The Civil Aviation Safety Regulations 1998, as outlined in the legislative instrument F2006B04792, pertain to the safety of civil aviation within Australia. Specifically, this Airworthiness Directive (AD) applies to all Pilatus Britten-Norman BN-2 Series Islander aircraft, including the BN2, BN2A, BN2B, BN2T, BN2T-4R, and BN2T-4S variants, that are equipped with FHL landing gear units. This AD mandates that corrective action, detailed in the directive, must be undertaken to address identified safety concerns. The directive is issued under the authority of the Civil Aviation Safety Authority (CASA) and becomes effective on the specified compliance date, in this case, 13 August 2003. The directive requires adherence to the B-N Group Limited Service Bulletin SB 298, which outlines the specific actions necessary to ensure the aircraft meet the requisite safety standards. This regulatory action is part of the broader framework of the Civil Aviation Safety Regulations, which establish the safety standards and requirements for aircraft operations within Australia.

Key Provisions

The Civil Aviation Safety Regulations 1998, particularly Part 39-105, outlines the requirements for issuing Airworthiness Directives (AD) by the Civil Aviation Safety Authority (CASA). Section 39.1(1) provides the authority for CASA to issue these directives, which are critical for ensuring that specific aircraft or aeronautical products meet safety standards. In this context, AD/BN-2/79 pertains to the Pilatus Britten-Norman BN-2 Series Aeroplanes, specifically those equipped with FHL Landing Gear. The directive mandates actions necessary to address unsafe conditions identified in these aircraft, as detailed in the requirement section. The AD/BN-2/79 requires that the specified action, in accordance with B-N Group Limited Service Bulletin SB 298, be undertaken for BN2, BN2A, BN2B, BN2T, BN2T-4R, and BN2T-4S series Islander aircraft equipped with FHL Landing Gear. This action is necessary to correct the identified unsafe condition. The requirement is that the action must be carried out in the circumstances and manner specified within the directive and must comply with the instructions provided in the requirement section. The compliance timeline is set out in the directive, with an effective date of 20 August 2003, and the directive itself becomes effective on 13 August 2003. The obligations imposed by this AD are clear and specific. Operators of the affected aircraft must ensure that the actions outlined in SB 298 are performed. This includes maintaining accurate records of the fatigue lives of the landing gear and its components, as determined by the UK Civil Aviation Authority (CAA) and FHL. The directive is designed to rectify the identified issue of inadequate recording methods for the fatigue lives of the FHL landing gear. Compliance with this AD is mandatory, and failure to adhere to the specified requirements may result in safety risks and potential non-compliance with aviation safety regulations. Failure to comply with the Airworthiness Directive can lead to serious consequences. Civil Aviation Safety Regulations may impose penalties for non-compliance, which can include fines, enforcement actions, or even grounding of the aircraft. The exact penalties are not specified in the directive but are governed by the broader framework of the Civil Aviation Safety Regulations. These penalties can be substantial and may also include criminal charges in cases where the non-compliance results in serious safety incidents or accidents. Therefore, it is imperative for operators to strictly adhere to the AD to avoid any legal repercussions and ensure the continued airworthiness of their aircraft.

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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.