AD/BN-2/71 Amdt 4 - Main Landing Gear Oleo Attachment Bracket

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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 revokes Airworthiness Directive (AD) AD/BN-2/71 Amdt 3 and issues the following 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-2/71

Amdt 4


Main Landing Gear Oleo Attachment Bracket 7/2004

 

Applicability: All BN-2, BN2A, BN2B, BN2T, BN2T-4R, and BN2T-4S Islander aircraft. Requirement:              Inspect in accordance with B-N Group Ltd. Mandatory Service Bulletin No. 273

Issue 5.

 

Note: UK CAA AD 005-09-2000 refers.

 

Compliance: As specified in the Requirement document.

 

This Amendment becomes effective on 8 July 2004.

 

Background: Several operators reported cracking of the Oleo Attachment Bracket NB-40-0075. If cracking is not detected early, failure of the bracket can occur which could result in detachment of the main landing gear.

 

Amendment 1 expanded the repeat inspection interval.

 

Amendment 2 introduced a steel oleo attachment bracket as terminating action for the repeat inspection requirement.

 

Amendment 3 introduced Mod. NB-M-1712, which embodies an improved fitting for the main landing gear.

 

Amendment 4 is issued in response to Issue 5 of the Requirement document, which introduces a note to the compliance statement.


David Villiers

Delegate of the Civil Aviation Safety Authority 26 May 2004

 

 

 

The above AD is notified in the Commonwealth of Australia Gazette on 16 June 2004.

 

 


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Overview

The Civil Aviation Safety Regulations 1998, enacted by the Commonwealth of Australia, serve to maintain the safety standards of aircraft operations within Australia. The problem this legislation addresses is the need to ensure that aircraft and aeronautical products meet certain safety standards to prevent accidents and ensure the safety of passengers and crew. This particular legislative instrument, issued under the authority of the Civil Aviation Safety Authority (CASA), aims to rectify unsafe conditions identified in specific aircraft models, in this case, the Pilatus Britten-Norman BN-2 Series Aeroplanes. By mandating specific inspections and actions, such as those outlined in the Airworthiness Directive for the main landing gear oleo attachment bracket, the regulation seeks to mitigate the risk of structural failure and enhance overall aviation safety. This directive reflects a commitment to proactive safety measures, ensuring that any identified issues are addressed promptly and effectively.

Scope and Application

The Civil Aviation Safety Regulations 1998 (CASR), specifically Part 39 - 105, pertain to the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, which are crucial for ensuring the safety of aircraft and aeronautical products within Australian jurisdiction. These regulations apply to all aircraft and aeronautical products that fall within the scope of the Civil Aviation Act 1988 and the Civil Aviation Regulations 1988. The applicability of this specific Airworthiness Directive (AD) extends to all BN-2, BN2A, BN2B, BN2T, BN2T-4R, and BN2T-4S Islander aircraft, necessitating specific maintenance actions to rectify identified safety concerns. This AD mandates inspections and actions to prevent potential failures of the main landing gear oleo attachment bracket, as outlined in the requirement section, to ensure the continued airworthiness of these aircraft. The AD is enforced by CASA, which has the authority to issue and revoke such directives to maintain safety standards across the Commonwealth of Australia.

Key Provisions

The Civil Aviation Safety Regulations 1998, particularly Part 39, section 105, specify the process by which the Civil Aviation Safety Authority (CASA) issues Airworthiness Directives (ADs). These ADs are intended to ensure the safety of aircraft operations by mandating certain actions to correct unsafe conditions. In the provided example, AD/BN-2/71 Amdt 4, the AD pertains to the Pilatus Britten-Norman BN-2 Series Aeroplanes and focuses on the Main Landing Gear Oleo Attachment Bracket. Specifically, it mandates that all BN-2, BN2A, BN2B, BN2T, BN2T-4R, and BN2T-4S Islander aircraft must be inspected in accordance with B-N Group Ltd. Mandatory Service Bulletin No. 273 Issue 5. This inspection is crucial to detect and address any potential cracking in the Oleo Attachment Bracket, which could lead to severe safety issues, including the detachment of the main landing gear. The AD imposes specific obligations on the operators of the affected aircraft. These operators are required to comply with the inspection procedures outlined in the B-N Group Ltd. Mandatory Service Bulletin No. 273 Issue 5. This compliance is to be carried out by following the instructions and timing specified in the AD. Non-compliance with these directives could result in the aircraft being deemed unsafe to operate, potentially leading to grounding and further legal repercussions. Violating the provisions of this AD may result in significant consequences. While the Civil Aviation Safety Regulations 1998 do not specify maximum penalties in this particular AD, non-compliance with ADs generally can lead to enforcement actions by CASA. Such actions may include fines, enforcement notices, and, in severe cases, prosecution. Additionally, operators may face civil liabilities if an incident occurs due to non-compliance, including potential compensation claims from passengers or third parties affected by the unsafe condition. Therefore, it is imperative that operators adhere strictly to the mandated inspection procedures to avoid these severe repercussions.

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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.