AD/FU24/50 - Control Column Grip - Inspection

Overview

The Civil Aviation Regulations 1998 were enacted to establish comprehensive safety standards for civil aviation in Australia. This legislation was introduced to address the need for stringent safety protocols in the rapidly evolving aviation industry, aiming to ensure the highest standards of airworthiness and safety for aircraft operations within Australian airspace. The regulations are overseen by the Civil Aviation Safety Authority (CASA), which is tasked with enforcing compliance and maintaining the safety standards set forth in the regulations. The policy objective of the Civil Aviation Regulations 1998 is to protect the public by ensuring that all civil aviation activities are conducted with the utmost regard for safety, thereby minimising the risk of accidents and incidents. The specific legislative instrument F2006B09998 pertains to an Airworthiness Directive issued under the Civil Aviation Regulations 1998, focusing on the inspection of control column grips for FU 24 Series Aeroplanes manufactured by Airparts (NZ) Ltd. This directive mandates inspections to be conducted at specified intervals to maintain the airworthiness of these aircraft, reflecting the ongoing commitment to safety and operational reliability within the civil aviation sector.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, applies to all models of FU 24 Series Aeroplanes manufactured by Airparts (NZ) Ltd. The directive, AD/FU24/50, pertains to the inspection of the control column grip and is designed to ensure the continuing airworthiness of these aircraft. This regulation applies to any person or entity operating such aircraft within Australia, thereby extending its jurisdictional reach across the Commonwealth. The directive mandates that compliance be achieved in two phases: Part A requires the inspection to occur at the next daily or overnight inspection following 12 May 1976, while Part B necessitates that the inspection be completed within 100 hours of time in service after the same date. The directive is supported by Aerospace SB ASB/FU/022, which provides further detail on the required inspection procedures. No specific exclusions, exemptions, or thresholds are mentioned in this directive, indicating that it applies universally to all FU 24 Series Aeroplanes within the specified timeframes.

Key Provisions

The Civil Aviation Regulations 1998, specifically within Part 39, outlines the requirements for Airworthiness Directives (ADs) applicable to various aircraft models, including the FU 24 Series Aeroplanes manufactured by Airparts (NZ) Ltd. The directive AD/FU24/50 pertains to the inspection of the control column grip, and it is crucial for maintaining the safety and airworthiness of these aircraft. The directive, referenced in Section 105, mandates inspections at specific intervals post the directive’s issuance date of 12 May 1976. The main operative sections of AD/FU24/50 require a daily or overnight inspection of the control column grip as stated in Part A of the directive. This inspection must occur at the next available opportunity after the directive is issued. Additionally, Part B of the directive mandates a more stringent inspection within 100 hours of the aircraft being in service after the directive’s issuance date. The directive references the Aerospace Service Bulletin ASB/FU/022 for detailed instructions on how to perform the required inspections and ensure compliance. The obligations imposed by AD/FU24/50 are primarily on aircraft operators and maintenance personnel. Operators must ensure that the control column grip inspections are carried out as per the stipulated timelines. Maintenance personnel are responsible for conducting these inspections meticulously and documenting the findings to verify compliance with the directive. Failure to comply with these obligations can lead to serious safety implications and potential regulatory penalties. Breach of AD/FU24/50 can result in significant legal and safety repercussions. The Civil Aviation Safety Authority (CASA) enforces compliance with these airworthiness directives, and non-compliance can lead to enforcement actions, including fines, suspension of airworthiness certificates, or even grounding of the aircraft. The potential penalties for such breaches are not explicitly stated in the directive, but they can be severe, reflecting the critical nature of ensuring aircraft safety and airworthiness. It is essential for all parties involved to adhere strictly to the requirements to avoid these consequences.