AD/FU24/59 - Rudder Torque Tube to Rudder Attachment - Inspection

Overview

The Civil Aviation Regulations 1998, as amended, represent a crucial framework governing aviation safety in Australia, ensuring that air operations meet high standards of safety and reliability. Part 39 - 105, concerning the Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically targets the safety of airparts such as those produced by Airparts (NZ) Ltd., including the FU 24 Series Aeroplanes. This legislation was enacted to address safety concerns identified within the aviation industry, particularly the looseness of the rudder torque tube attachment to the rudder ribs in the specified models. The objective of these regulations is to mandate regular inspections to ensure the continued airworthiness and safety of these aircraft, thereby protecting the integrity of civil aviation operations. The Civil Aviation Safety Authority, under the oversight of the Australian Government, enforces these directives to maintain public safety and ensure compliance with national and international aviation standards. The Civil Aviation Regulations 1998 were established by the Australian Parliament to regulate civil aviation and ensure the safety of air travel. Specifically, AD/FU24/59, issued by the Civil Aviation Safety Authority, targets the FU 24 Series Aeroplanes produced by Airparts (NZ) Ltd., mandating inspections of the rudder torque tube attachment within 100 hours of time in service after 30 November 1980. This directive aims to mitigate risks associated with looseness in the rudder torque tube attachment, which could compromise the structural integrity and operational safety of the aircraft. The policy objective of this regulation is to enhance aviation safety by enforcing stringent inspection protocols, thus preventing potential accidents and ensuring the continued reliability of the affected aircraft models.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105 and the Civil Aviation Safety Authority Schedule of Airworthiness Directives, apply to all models of FU 24 Series aeroplanes including the FU24, FU24A, FU24-950, FU24A-950, FU24A-950M, FU24-954, and FU24A-954, manufactured by Airparts (NZ) Ltd. This regulation mandates an inspection of the rudder torque tube to rudder attachment to ensure airworthiness following reports of looseness in this critical component. The inspection must be conducted within 100 hours of time in service after 30 November 1980, as outlined in Aerospace SB No. ASB/FU/071. This requirement extends to all operators of these specific aircraft models within the Commonwealth of Australia, ensuring safety standards are upheld. The Act does not explicitly mention any exclusions, exemptions, or thresholds, implying that all applicable aircraft must comply with the directive without exception. The scope of this directive is enforced nationally, applying uniformly across all states and territories in Australia.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39, mandate safety directives for certain aircraft models, with Section 39-105 detailing the airworthiness directives for Airparts (NZ) Ltd. FU 24 Series Aeroplanes. Under this directive (AD/FU24/59), the Rudder Torque Tube to Rudder Attachment requires inspection to ensure structural integrity and safety. This directive applies to all models FU24, FU24A, FU24-950, FU24A-950, FU24A-950M, FU24-954, and FU24A-954 (Section 11/80). The compliance requirement stipulates that this inspection must be carried out within 100 hours of time in service after 30 November 1980, referencing the Aerospace SB No. ASB/FU/071. The Civil Aviation Regulations 1998 impose clear obligations on aircraft operators and maintenance personnel to adhere to these airworthiness directives. Operators must ensure that the specified inspection of the rudder torque tube attachment is conducted as required, and maintenance personnel must perform these inspections meticulously, following the guidelines provided in Aerospace SB No. ASB/FU/071. Failure to comply with these directives could result in the aircraft being deemed unairworthy, potentially leading to grounding until the necessary inspections and repairs are completed. The Act does not explicitly outline criminal or civil penalties for non-compliance with these directives in the provided text. However, the broader framework of the Civil Aviation Act 1988 and Civil Aviation Regulations 1998 encompasses severe consequences for non-compliance with airworthiness directives. This can include fines, imprisonment for individuals, and significant penalties for corporations. The exact penalties may vary depending on the severity and circumstances of the breach, but the overarching aim is to enforce stringent safety standards to protect public safety in aviation.