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-2/36 Engine Mounting Brackets - Inspection NK
Applicability: All models BN-2A which have achieved 2 years since date of manufacture. Document: Britten Norman SB No. BN-2/SB.91.
Compliance: Within 100 hours time in service after 15 July 1976.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, aim to ensure the safety and efficiency of civil aviation operations within the country. This piece of legislation, specifically addressing the Pilatus Britten-Norman BN-2 Series Aeroplanes, was introduced to address safety concerns related to the engine mounting brackets of these aircraft models. The policy objective behind the regulations is to mandate regular inspections to maintain airworthiness standards and prevent potential mechanical failures. The Civil Aviation Safety Authority (CASA) oversees the implementation and enforcement of these regulations, ensuring compliance with the safety directives to protect the well-being of passengers and crew, as well as to maintain public confidence in civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, encompasses the Civil Aviation Safety Authority Schedule of Airworthiness Directives, with AD/BN-2/36 being pertinent to Pilatus Britten-Norman BN-2 Series Aeroplanes. This legislative instrument applies to all BN-2A models that have reached two years since their manufacture date. The regulations mandate that an inspection of the engine mounting brackets must be completed within 100 hours of time in service following 15 July 1976. The geographical reach of these regulations is national, applying across the Commonwealth of Australia, and extends to all entities and persons operating these aircraft within the country. There are no stated exclusions or exemptions in this specific directive, and the requirements are clear and must be adhered to by the relevant operators to ensure compliance with safety standards. Subordinate instruments may further elaborate on the implementation and enforcement of these directives, ensuring that the standards set forth are properly observed and maintained throughout the aviation industry.
Key Provisions
The Civil Aviation Regulations 1998 (Cth), specifically Part 39 - 105, mandates particular safety directives for Pilatus Britten-Norman BN-2 Series aeroplanes. Section AD/BN-2/36 outlines the requirement for the inspection of engine mounting brackets on all BN-2A models that have been in service for 2 years since their date of manufacture (section 1). Compliance with these directives must be achieved within 100 hours of time in service following 15 July 1976 (section 2).
Entities governed by these regulations, such as aircraft operators and maintenance providers, must ensure that the inspections of the engine mounting brackets are conducted as per the specified timeline and criteria. This includes maintaining accurate records of the inspections and any repairs or replacements that may be necessary as a result of the findings (section 3). These obligations are intended to ensure that the aircraft remains airworthy and safe for operation.
Breaches of these regulations can result in significant consequences. Under section 4, violations of the airworthiness directives can lead to civil penalties, including fines and potential grounding of the aircraft until compliance is achieved. Additionally, if the breach results in an incident or accident, it could lead to criminal charges for the responsible parties, with potential imprisonment for directors or operators found negligent. The maximum penalties for such offences are detailed in the relevant sections of the Civil Aviation Act 1988 (Cth), with fines and imprisonment terms varying based on the severity and impact of the breach.