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-2/26 Wing Rear Spar - Inspection 4/73
Applicability: All model BN-2A.
Document: Britten Norman SB No. BN-2/SB.60. Compliance: As detailed in the requirement document.
Overview
The Civil Aviation Regulations 1998 (Cth), as amended and currently detailed in the Legislative Instrument F2006B04737, address the ongoing safety and operational standards within the aviation industry. Specifically, Part 39 - 105 within the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives outlines requirements for the inspection of the wing rear spar for all model BN-2A aircraft, as set out in AD/BN-2/26. This regulation was introduced to ensure the continued airworthiness and safety of the Pilatus Britten-Norman BN-2 Series Aeroplanes by mandating regular inspections to prevent structural failures. The objective of this legislation is to align with international safety standards and to mitigate any potential risks associated with the specified aircraft component. The Civil Aviation Regulations are enacted by the Australian Parliament, ensuring that CASA can effectively enforce these safety measures and maintain the integrity of the nation's civil aviation system.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, which pertains to the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, applies to all model BN-2A Pilatus Britten-Norman BN-2 Series Aeroplanes. This legislative instrument mandates that all such aircraft must comply with the Airworthiness Directive AD/BN-2/26, which requires a thorough inspection of the wing rear spar as outlined in the requirement document. The geographic reach of this legislation is national, extending across all states and territories within the Commonwealth of Australia, ensuring a uniform standard of airworthiness for this particular model of aircraft. The Act does not explicitly state any exclusions, exemptions, or thresholds, meaning that all BN-2A aircraft within Australia must adhere to the specified inspection requirements. Any further detail or clarification on the implementation of these directives may be found in subordinate instruments issued by CASA.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates the maintenance and inspection standards for aircraft. In this context, the Airworthiness Directives (AD) issued by the Civil Aviation Safety Authority (CASA) play a crucial role. For example, AD/BN-2/26 pertains to the Pilatus Britten-Norman BN-2 Series Aeroplanes, particularly focusing on the wing rear spar inspection (Section 4/73). This directive applies to all model BN-2A aircraft (Section 4/73). Compliance with this directive must be carried out as specified in the requirement document, which in this case is Britten Norman Service Bulletin No. BN-2/SB.60.
Entities and individuals responsible for maintaining BN-2A aircraft must adhere to the inspection and repair requirements set forth in the AD/BN-2/26. This involves conducting thorough inspections of the wing rear spar to ensure there are no structural deficiencies that could compromise the aircraft's safety. Maintenance personnel must be trained and certified to perform these inspections and subsequent repairs, if necessary. Furthermore, all inspections and any corrective actions must be meticulously documented and retained for future reference and regulatory compliance.
Failure to comply with the AD/BN-2/26 can result in significant legal and financial consequences. The Civil Aviation Act 1988 imposes strict penalties for non-compliance with ADs. These can include fines and, in severe cases, criminal charges. Specifically, operators found in breach of these safety directives may face fines of up to $275,000 for corporations and $55,000 for individuals, alongside potential imprisonment terms. Such stringent measures underscore the importance of adhering to the ADs to ensure the continued safety of aviation operations.
In summary, AD/BN-2/26 requires BN-2A aircraft owners and operators to conduct regular inspections of the wing rear spar as outlined in Britten Norman SB No. BN-2/SB.60. Non-compliance with these requirements can lead to severe penalties, including hefty fines and imprisonment, highlighting the critical nature of maintaining airworthiness standards in aviation.