Overview

The Civil Aviation Regulations 1998 were enacted to ensure the safety and efficiency of civil aviation in Australia, providing a comprehensive regulatory framework to govern all aspects of civil aviation. Part 39 - 105, which pertains to airworthiness directives, was introduced to address specific safety issues identified in certain aircraft models. This part of the regulations is overseen by the Civil Aviation Safety Authority (CASA) and aims to maintain and enhance the safety standards within the aviation industry. The Embraer EMB-110 (Bandeirante) Series Aeroplanes Airworthiness Directive AD/EMB-110/17, for instance, was issued to address potential fire hazards associated with the fire detector bracket assembly, ensuring that these aircraft meet stringent safety requirements. The directive specifies the applicability and compliance requirements, mandating modifications to the fire detector bracket assembly within a specified timeframe to mitigate risks identified in Embraer Service Bulletin No. 110-26-003 and CTA Airworthiness Directive No. 82-02-02. The Embraer EMB-110 (Bandeirante) Series Aeroplanes Airworthiness Directive AD/EMB-110/17, part of the Civil Aviation Regulations 1998, was introduced to tackle a specific safety concern related to the fire detector bracket assembly on Embraer EMB-110 aircraft. This directive applies to all EMB-110 models with serial numbers referenced in Embraer Service Bulletin No. 110-26-003 and mandates compliance within 250 hours of time in service after 30 September 1982. The primary objective of this directive is to prevent potential fire hazards that may arise from damage to the fire detector installation during the removal and installation of the engine upper cowling. The regulation underscores the commitment of the Civil Aviation Safety Authority (CASA) to ensuring the highest safety standards in civil aviation, focusing on the proactive identification and mitigation of risks.

Scope and Application

The Embraer EMB-110 (Bandeirante) Series Aeroplanes Airworthiness Directive, specifically AD/EMB-110/17, pertains to all models of the EMB-110 aeroplanes with serial numbers as referenced in Embraer Service Bulletin No. 110-26-003. This legislative instrument, under the Civil Aviation Regulations 1998, is aimed at ensuring the safety and compliance of these aircraft by mandating the modification of the fire detector bracket assembly, identified by part number 4A-513-21-02. The directive requires compliance within 250 hours of time in service following 30 September 1982, and it is enforceable through either Embraer Service Bulletin No. 110-26-003 or Civil Aviation Order No. 82-02-02. This regulation applies to the Commonwealth of Australia and is overseen by the Civil Aviation Safety Authority, reflecting a commitment to maintaining stringent safety standards across the nation's airspace.

Key Provisions

The Civil Aviation Regulations 1998, specifically in Part 39 - 105, address the airworthiness directives for various aircraft, including the Embraer EMB-110 (Bandeirante) Series Aeroplanes. Section AD/EMB-110/17 pertains to the modification of the fire detector bracket assembly P/N 4A-513-21-02. This directive applies to all models of the EMB-110 series with specific serial numbers referenced in Embraer Service Bulletin No. 110-26-003. Compliance with this directive must be achieved within 250 hours of time in service following 30 September 1982. Entities governed by these regulations must ensure that the specified modifications to the fire detector bracket assembly are implemented correctly. This includes verifying that the aircraft in question falls within the serial number range outlined in Embraer SB No. 110-26-003 or CTA AD No. 82-02-02. The primary focus of this directive is to mitigate potential damage to the fire detector installation that may occur during the removal and installation of the engine upper cowling. The obligations imposed by these regulations are quite clear. Operators and owners of the affected EMB-110 series aircraft must undertake the required modifications to the fire detector bracket assembly within the specified timeframe. This involves either referring to Embraer SB No. 110-26-003 or CTA AD No. 82-02-02 to confirm applicability and then ensuring that the modifications are carried out by appropriately qualified personnel. Failure to adhere to these directives can have serious implications for the airworthiness and safety of the aircraft. In the event of non-compliance with the airworthiness directives outlined in the Civil Aviation Regulations, there can be significant consequences. The Civil Aviation Safety Authority (CASA) has the authority to impose penalties for breaches of these regulations. Depending on the severity and nature of the breach, penalties can include fines, suspension or revocation of aircraft certificates of airworthiness, and other regulatory actions. The exact penalties are determined based on the specific circumstances of the breach and can be substantial, reflecting the critical importance of adhering to these safety directives.