AD/ROBIN/4 - Aileron/Flap Support Brackets - Inspection and Reinforcement

Overview

The Civil Aviation Regulations 1998, specifically Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, introduces AD/ROBIN/4 concerning Robin Aviation Series Aeroplanes. This legislative instrument was enacted to address the safety concern of cracking adjacent to the attachment points of the left and right aileron/flap common support brackets and the corresponding wing skin areas in model R2000 aircraft. The Australian Government, through the relevant legislature, introduced this directive to ensure the ongoing airworthiness of these aeroplanes and to mitigate the risk of structural failure. The policy objective of this regulation is to mandate a timely inspection and, if necessary, reinforcement of the affected areas to maintain safety standards in accordance with the manufacturer's advisory. Compliance with this directive is mandatory for all model R2000 aircraft, requiring inspection and reinforcement within 100 hours of time in service after 31 October 1982, in line with Avions Pierre Robin Service Bulletin No. 90. This regulation ensures that all relevant stakeholders adhere to the safety measures prescribed by the Civil Aviation Safety Authority to prevent potential safety incidents.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies to all model R2000 aircraft within the Robin Aviation series. This legislation mandates specific inspections and reinforcement of aileron/flap support brackets to address reported cracking issues near the attachment points of the left and right aileron/flap common support brackets and corresponding wing skin areas. Compliance with this directive is required within 100 hours of time in service following 31 October 1982, as per the documented requirement outlined in Avions Pierre Robin Service Bulletin No. 90. The directive's jurisdictional reach is comprehensive, applying across all relevant aircraft within the specified model in Australia, as overseen by the Civil Aviation Safety Authority. The application of this legislation ensures safety and operational standards are maintained within the specified industry sector.

Key Provisions

The key operative sections of the Civil Aviation Regulations 1998 (Cth) in the context of AD/ROBIN/4 concern the inspection and reinforcement of aileron/flap support brackets for Robin Aviation Series Aeroplanes, specifically model R2000 (section 39-105). This directive mandates that all R2000 models must comply with Avions Pierre Robin Service Bulletin No. 90. The compliance timeline stipulates that inspections and necessary reinforcements must be carried out within 100 hours of time in service following 31 October 1982. This directive aims to address the reported cracking adjacent to the attachment points of the left and right aileron/flap common support brackets and corresponding wing skin areas, as reported by the manufacturer. The obligations imposed by this Act on the parties or entities it governs are clear and specific. Owners and operators of Robin Aviation Series Aeroplanes, model R2000, must ensure that their aircraft undergo a thorough inspection of the aileron/flap support brackets as per the specified timeline. If any cracking is detected, the relevant areas must be reinforced according to the guidelines provided in Avions Pierre Robin Service Bulletin No. 90. This includes conducting the inspection within the stipulated timeframe and documenting the findings and any actions taken. Additionally, the responsible authorities must maintain records of compliance to ensure that all aircraft meet the necessary safety standards. The Civil Aviation Regulations 1998 (Cth) include provisions for penalties and consequences for non-compliance with the outlined directives. Failure to adhere to the inspection and reinforcement requirements can result in civil penalties. Specifically, operators who do not comply with the safety directives may face fines and potential grounding of their aircraft. These penalties are intended to enforce compliance and ensure the safety of the aviation operations. The maximum penalties for non-compliance can vary but are designed to be significant enough to encourage adherence to the regulations. This underscores the importance of timely inspections and necessary repairs to prevent potential safety hazards.