COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
AMD Falcon 50 and 900 Series Aeroplanes
AD/AMD 50/12 Right Hand Electrical Cabinet Wiring Harness 8/96
Applicability: This Directive is applicable to Mystere-Falcon 50 aeroplanes with equipment racks fitted between frames 9 and 11, aft of the right hand electrical cabinet.
Requirement: Action in accordance with Dassault Aviation Falcon 50 Mandatory Service Bulletin F50-256 dated 24 April 1996.
Note: DGAC AD 96-094-017(B) dated 24 April 1996 refers.
Compliance: Within 300 hours time in service after 18 July 1996 or prior to 31 December 1996, whichever occurs first.
Background: This Directive is issued following a report from Dassault Aviation advising of an incident resulting from a chafed wiring harness aft of the right hand electrical cabinet. The actions specified by this Directive are designed to decrease the likelihood of wire harness chafing occurring in this area.
Overview
The Civil Aviation Regulations 1998, as amended, are a comprehensive set of rules governing all aspects of civil aviation in Australia, ensuring the safety and efficiency of the nation's airspace. One such amendment, F2006B02379, specifically addresses the safety of the Falcon 50 and 900 series aeroplanes by introducing Airworthiness Directives that target identified issues. This particular directive was introduced to address a problem identified by Dassault Aviation concerning the right-hand electrical cabinet wiring harness in Mystere-Falcon 50 aeroplanes, which had been associated with an incident due to chafing. The directive aims to mitigate such risks by requiring compliance with Dassault Aviation's Mandatory Service Bulletin F50-256. The policy objective behind this regulation is to enhance aircraft safety by ensuring that identified faults are rectified in a timely manner, thereby preventing potential incidents that could compromise the safety of the flight. Enacted by the Australian Government, this directive is part of the broader framework designed to maintain the highest standards of aviation safety.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, addresses the application of AD/AMD 50/12 concerning the right-hand electrical cabinet wiring harness of Mystere-Falcon 50 aeroplanes. This directive applies to specific models of Falcon 50 aeroplanes equipped with equipment racks installed between frames 9 and 11, aft of the right-hand electrical cabinet. The requirement mandates compliance with Dassault Aviation Falcon 50 Mandatory Service Bulletin F50-256 dated 24 April 1996, which aims to mitigate the risk of wire harness chafing in the specified area. The directive necessitates action within 300 hours of time in service following 18 July 1996, or before 31 December 1996, whichever comes first. This regulation is issued in response to a reported incident caused by chafed wiring, thereby underscoring the importance of timely corrective measures to ensure aviation safety.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39 - 105, outlines the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives for specific aircraft types. In this instance, AD/AMD 50/12 pertains to the Falcon 50 and 900 series aeroplanes, focusing on the wiring harness in the right hand electrical cabinet. According to section 105 of the Regulations, this directive applies to Mystere-Falcon 50 aeroplanes equipped with racks between frames 9 and 11, located aft of the right hand electrical cabinet. The directive requires compliance with Dassault Aviation Falcon 50 Mandatory Service Bulletin F50-256 dated 24 April 1996, as referenced in DGAC AD 96-094-017(B) from the same date.
The obligations imposed by this directive necessitate adherence to the actions detailed in the aforementioned service bulletin. Specifically, operators of Mystere-Falcon 50 aeroplanes must ensure that the specified wiring harness modifications are implemented within 300 hours of time in service after 18 July 1996 or before 31 December 1996, whichever comes first. This timeframe is critical to ensure the safety of the aircraft and its occupants by mitigating the risk of wiring harness chafing. The directive underscores the importance of timely compliance to address a reported incident where chafing of the wiring harness led to safety concerns.
Failure to comply with the requirements set out in AD/AMD 50/12 could result in serious safety implications. While the specific penalties are not detailed in the provided text, non-compliance with CASA directives generally could lead to enforcement actions. These may include fines, sanctions, or even the grounding of the aircraft until the necessary modifications are completed. The overarching objective is to ensure that all operators maintain their aircraft to the highest safety standards, preventing potential hazards that could compromise flight safety.
In summary, AD/AMD 50/12 under the Civil Aviation Regulations 1998 mandates specific actions to address wiring harness issues in Mystere-Falcon 50 aeroplanes. Operators must implement these actions within a prescribed timeframe to ensure compliance with safety directives. The consequences of non-compliance could range from administrative penalties to more severe measures, reflecting the critical importance of adhering to safety regulations in aviation.