AD/BN-2/33 Amdt 1 - Rudder Hinge Mounting - Inspection and Modification

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Legislation au F2006B04745 In force Legislative Instrument

Legislation content

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-2/33

Amdt 1

Applicability: All models.


Rudder Hinge Mounting - Inspection and Modification


1/75

 

Document: Britten Norman SB No. BN-2/SB.76 Issue 3. Compliance:  As per requirement document.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, specifically PART 39 - 105, address the need to ensure the safety and airworthiness of aircraft operating in Australia. This legislation was enacted by the Australian Parliament and is administered by the Civil Aviation Safety Authority (CASA). The problem this legislation was introduced to address includes the need to maintain stringent safety standards across the civil aviation industry, particularly in relation to specific aircraft models. The overarching policy objective is to ensure that all aircraft are maintained to a high standard of safety, which is critical in preventing accidents and ensuring the safety of passengers and crew. The 1998 Regulations were designed to provide a comprehensive framework that governs the airworthiness of aircraft and the certification of aviation personnel, thereby filling a critical gap in aviation safety regulation in Australia.

Scope and Application

The Civil Aviation Safety Authority's Airworthiness Directives, specifically AD/BN-2/33 Amendment 1, applies to all models of the Pilatus Britten-Norman BN-2 Series Aeroplanes. The directive mandates an inspection and modification of the rudder hinge mounting to ensure continued airworthiness, as outlined in the requirement document, Britten Norman Service Bulletin No. BN-2/SB.76 Issue 3. This regulation is applicable to all entities and persons operating these aircraft, ensuring compliance with safety standards set forth by the Civil Aviation Safety Authority. The directive operates within the jurisdictional reach of the Commonwealth of Australia and extends across all states and territories, ensuring a uniform approach to safety standards in civil aviation. There are no stated exclusions or exemptions within the directive, although compliance thresholds and specific application details may be further defined through subordinate instruments issued by the Civil Aviation Safety Authority.

Key Provisions

The Civil Aviation Regulations 1998 (CAR) under PART 39 - 105, specifically AD/BN-2/33 Amendment 1, pertains to the maintenance and inspection of the rudder hinge mounting of all models of the Pilatus Britten-Norman BN-2 Series aeroplanes (section 39.105). This legislative instrument mandates that the rudder hinge mounting must be inspected and, if necessary, modified as per the specific guidelines provided in the document, Britten Norman Service Bulletin No. BN-2/SB.76 Issue 3. Compliance with this directive is mandatory, and it is essential that all inspections and modifications are carried out in accordance with the outlined requirements. The obligations imposed by this directive are quite specific. Operators of the Pilatus Britten-Norman BN-2 Series aeroplanes must ensure that the rudder hinge mounting is inspected according to the criteria specified in the referenced service bulletin. If any deficiencies are identified during the inspection, the required modifications must be performed. Additionally, operators must maintain records of all inspections and modifications to demonstrate compliance with the directive. These records must be readily accessible for inspection by the Civil Aviation Safety Authority (CASA) upon request. Failure to comply with the requirements set forth in AD/BN-2/33 Amendment 1 may result in serious consequences. Firstly, non-compliance could lead to civil penalties. Under section 30 of the Civil Aviation Act 1988, CASA has the authority to impose penalties for breaches of the Civil Aviation Regulations. The maximum penalty for contravening a regulation can be substantial, reaching up to $210,000 for a corporation and $42,000 for an individual, depending on the severity of the breach. Furthermore, in addition to financial penalties, non-compliance may also lead to criminal charges. If CASA finds that an operator has wilfully breached the regulations, the operator may face prosecution under section 30A of the Civil Aviation Act 1988, which can result in imprisonment for up to two years. These potential penalties underscore the importance of strict adherence to the regulatory requirements outlined in AD/BN-2/33 Amendment 1.

Legal classification tags

Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
Airworthiness Directives

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Authorises

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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.