COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
British Aerospace BAe 125 Series Aeroplanes
AD/HS 125/140 Galley Electrical Feeder Cables 5/94
Applicability: BAe 125 Series 1000 aircraft, furnished with a `Traditional Galley’ at Chester and identified in Hawker Raytheon Corporate Jets Service Bulletin SB.25-75-25A699A dated 10 February 1994.
Requirement: Incorporate Modification Number 25A699A in accordance with the Accomplishment Instructions of Hawker Raytheon Corporate Jets Service Bulletin SB.25-75-25A699A dated 10 February 1994.
Note: This Service Bulletin has been classified as Mandatory by the CAA(UK).
Compliance: Prior to 30 June 1994.
Background: Galley electrical feeder cables and fuse ratings are not compatible. An electrical fault in the galley could result in the cables overheating, together with possible smoke generation. This Directive requires an increase in the gauge of the galley electrical feeder cables and the addition of a fuse in the galley.
The CAA(UK) compliance time is extended by two months.
Overview
The Civil Aviation Safety Authority, under the authority of the Civil Aviation Act 1988, enacted the Civil Aviation Regulations 1998 to provide a comprehensive legal framework governing civil aviation safety in Australia. The regulations, including Part 39, aim to address safety issues and ensure compliance with international aviation standards. A specific focus of these regulations is the issuance of Airworthiness Directives to mitigate identified safety risks. The directive AD/HS 125/140 addresses a significant safety concern involving the British Aerospace BAe 125 Series 1000 aircraft, specifically those equipped with a "Traditional Galley" at Chester. The directive mandates the incorporation of Modification Number 25A699A, as outlined in Hawker Raytheon Corporate Jets Service Bulletin SB.25-75-25A699A dated 10 February 1994, to resolve compatibility issues between galley electrical feeder cables and fuse ratings. Failure to adhere to these requirements could result in overheating of the cables, potentially leading to smoke generation and increased fire risk. The directive's objective is to enhance the safety of the aircraft by ensuring the galley electrical system's integrity, thereby preventing potential hazards that could compromise flight safety.
Scope and Application
The Civil Aviation Regulations 1998, specifically PART 39 - 105, pertain to the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, focusing on the British Aerospace BAe 125 Series Aeroplanes. This legislation applies to BAe 125 Series 1000 aircraft that are equipped with a 'Traditional Galley' at Chester, as identified in Hawker Raytheon Corporate Jets Service Bulletin SB.25-75-25A699A dated 10 February 1994. The directive mandates that these aircraft must incorporate Modification Number 25A699A in line with the Accomplishment Instructions detailed in the aforementioned service bulletin. Notably, the Civil Aviation Authority (UK) has classified this service bulletin as mandatory, underscoring the importance of compliance to ensure the airworthiness of these aircraft. The directive requires compliance by 30 June 1994, with an additional two-month extension granted by the UK CAA. This requirement is prompted by the incompatibility of galley electrical feeder cables and fuse ratings, which could lead to overheating and potential smoke generation due to an electrical fault in the galley. The directive thus necessitates an increase in the gauge of the galley electrical feeder cables and the addition of a fuse in the galley to mitigate these risks.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39 - 105, specifically address the airworthiness directives for British Aerospace BAe 125 Series aeroplanes. The regulation in question, AD/HS 125/140, pertains to the galley electrical feeder cables (s. 5/94). This directive is applicable to BAe 125 Series 1000 aircraft equipped with a 'Traditional Galley' at Chester, identified in Hawker Raytheon Corporate Jets Service Bulletin SB.25-75-25A699A dated 10 February 1994. The primary requirement of this directive is to incorporate Modification Number 25A699A in accordance with the Accomplishment Instructions provided in the same Service Bulletin. Notably, the Service Bulletin has been classified as Mandatory by the Civil Aviation Authority (UK).
The regulation imposes several obligations on the operators and owners of the BAe 125 Series 1000 aircraft. Operators must ensure that the galley electrical feeder cables and fuse ratings are compatible to prevent potential overheating and possible smoke generation due to electrical faults. Compliance with this directive requires the incorporation of the specified modification (Modification Number 25A699A) before the deadline of 30 June 1994. This deadline can be extended by two months under the CAA(UK) compliance provisions. The directive mandates an increase in the gauge of the galley electrical feeder cables and the addition of a fuse in the galley to enhance safety.
Failure to comply with this airworthiness directive can result in significant consequences. Operators and owners of the affected aircraft who do not adhere to the requirements specified in the directive may face enforcement actions. The potential penalties for non-compliance can include both civil and criminal liabilities, although the specific penalties are not detailed in the provided text. However, it is understood that non-compliance with airworthiness directives can lead to severe repercussions, including fines and potential grounding of the aircraft, which can disrupt operations and compromise safety.
The directive aims to mitigate risks associated with electrical faults in the galley, which could otherwise lead to overheating and smoke generation. By mandating the modification of the galley electrical feeder cables and the addition of a fuse, the regulation seeks to enhance the safety and reliability of the aircraft. Ensuring compliance with these provisions is crucial for maintaining the airworthiness of the BAe 125 Series 1000 aircraft and preventing potential hazards during flight operations.