COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
British Aerospace BAe 3100 (Jetstream) Series Aeroplanes
AD/JETSTREAM/55 Engine Fire Protection System Hose Assemblies
13/92 DM
Applicability: British Aerospace Jetstream Series 3100 and Series 3200 aircraft constructor’s numbers 601 to 964 inclusive with the exception of numbers 703, 705 and 707.
Requirement: Action in accordance with the technical requirements of the CAA (UK) Airworthiness Directive 006-10-92.
Note: British Aerospace Alert Services Bulletin26-A-JA920401 refers.
Compliance: As detailed in the Requirement Document with a compliance date of 8 December 1992.
Background: All hoses identified in the Directive must be replaced because the manufacturer has determined that the hose material may be subject to premature ageing.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 105, was enacted to ensure the safety and airworthiness of aircraft operating in Australia. This legislation, established by the Commonwealth of Australia, aims to address safety concerns and compliance with international standards set forth by the Civil Aviation Safety Authority (CASA). One particular focus of these regulations is the British Aerospace BAe 3100 (Jetstream) Series Aeroplanes, where Airworthiness Directive AD/JETSTREAM/55 has been issued to ensure the integrity of engine fire protection system hose assemblies. The directive applies to aircraft with constructor’s numbers 601 to 964, excluding certain numbers identified as exempt, and mandates action in accordance with the UK CAA Airworthiness Directive 006-10-92. The directive requires the replacement of all affected hoses due to concerns over premature ageing of the hose material, with compliance mandated by a specified date to maintain safety standards.
The policy objective behind these regulations is to enhance the safety of air travel by ensuring that aircraft meet stringent airworthiness criteria. By aligning with international directives and addressing specific issues identified by manufacturers, the Civil Aviation Regulations 1998 provide a robust framework for maintaining the highest safety standards in the aviation industry. This ensures that aircraft operating within Australia adhere to critical safety requirements, thereby protecting passengers, crew, and the general public from potential hazards.
Scope and Application
The Civil Aviation Regulations 1998, specifically PART 39 - 105, applies to the British Aerospace BAe 3100 (Jetstream) Series Aeroplanes, covering aircraft constructor’s numbers 601 to 964 inclusive, with the exception of numbers 703, 705, and 707. This legislation mandates adherence to the technical requirements set forth by the Civil Aviation Authority (UK) Airworthiness Directive 006-10-92, which pertains to the replacement of engine fire protection system hose assemblies due to potential premature ageing of the hose material. The requirement for compliance is detailed in the accompanying Requirement Document, with a compliance deadline of 8 December 1992. This directive ensures that the specified aircraft maintain safety standards in line with international airworthiness directives, and British Aerospace Alert Services Bulletin 26-A-JA920401 provides additional relevant information. The scope of this regulation is limited to the aforementioned aircraft models and excludes those with specific constructor numbers, thereby targeting a precise subset within the broader category of British Aerospace Jetstream Series aeroplanes.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, include a schedule of airworthiness directives pertaining to various aircraft types, including the British Aerospace BAe 3100 (Jetstream) Series aeroplanes. One such directive, AD/JETSTREAM/55 13/92 DM, concerns the engine fire protection system hose assemblies for Jetstream Series 3100 and Series 3200 aircraft with constructor’s numbers 601 to 964, excluding numbers 703, 705, and 707. This directive mandates that these aircraft must adhere to the technical requirements outlined in the CAA (UK) Airworthiness Directive 006-10-92. The directive also references British Aerospace Alert Services Bulletin 26-A-JA920401 for additional details.
The primary obligation imposed by this directive is the replacement of all hoses identified within it, as determined by the manufacturer due to the potential for premature ageing of the hose material. Compliance with this directive is required by a specified date, 8 December 1992, as detailed in the Requirement Document. The compliance ensures that the engine fire protection system remains effective and safe for operation, thus maintaining the airworthiness of the aircraft.
Failure to comply with the provisions of this directive can result in significant legal and operational consequences. The Civil Aviation Regulations 1998 outline various offences and penalties for non-compliance with airworthiness directives. Although the specific penalties are not detailed in the directive itself, general penalties under the Civil Aviation Act 1988 can include substantial fines and potential criminal charges for individuals and corporations. Additionally, non-compliance can lead to the grounding of the aircraft, which can have severe financial and operational repercussions for the aircraft operator.
Moreover, the operation of an aircraft that does not meet airworthiness standards can pose a serious risk to safety, leading to potential criminal charges for endangerment. The seriousness of these consequences underscores the importance of adhering to the directives and ensuring all required actions are taken in a timely and effective manner.