COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Sikorsky S-76 Series Helicopters
AD/S-76/37 Engine Fire Extinguisher Harness - Modification 4/85 Applicability: All model S-76A fitted with fire extinguisher harness P/Nos 76552-10128-041/042. Requirement: Sikorsky Alert Service Bulletin No. 76-26-1.
Compliance: Within 100 hours time in service after 30 April 1985.
Background: System redundancy is improved by wiring the dual fire extinguisher primers in parallel.
Overview
The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority (CASA), was enacted to provide comprehensive regulation of civil aviation activities in Australia. One of the specific legislative instruments under this Act is the Airworthiness Directive (AD) issued for the Sikorsky S-76 Series Helicopters. AD/S-76/37, introduced in 1985, addresses the risk of engine fire by requiring a modification to the fire extinguisher harness on the S-76A models. This directive was established to enhance system redundancy and improve safety by ensuring that the dual fire extinguisher primers are wired in parallel, as specified in Sikorsky Alert Service Bulletin No. 76-26-1. Compliance with this directive is mandatory within 100 hours of time in service after 30 April 1985, reflecting the policy objective of maintaining the highest safety standards in civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, under the authority of the Civil Aviation Safety Authority, encompass specific directives aimed at ensuring the airworthiness and safety of aircraft within Australia's jurisdiction. One such directive, AD/S-76/37, applies to all Sikorsky S-76A series helicopters fitted with a fire extinguisher harness identified by part numbers 76552-10128-041/042. This regulation mandates compliance with Sikorsky Alert Service Bulletin No. 76-26-1, which requires modifications to the engine fire extinguisher harness to enhance system redundancy by wiring the dual fire extinguisher primers in parallel. The directive necessitates that these modifications be completed within 100 hours of the helicopter's time in service following 30 April 1985. The application of this regulation is confined to the specified model and equipment, ensuring that only those aircraft meeting the described criteria are subject to the requirements outlined within the legislative instrument.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, include detailed provisions for maintaining the airworthiness of aircraft, such as the Sikorsky S-76 Series Helicopters (section 105). This particular directive, AD/S-76/37, focuses on the engine fire extinguisher harness for model S-76A helicopters equipped with specific fire extinguisher harness part numbers (section 2). The directive requires compliance with Sikorsky Alert Service Bulletin No. 76-26-1, which mandates modifications to the fire extinguisher harness to improve system redundancy by wiring the dual fire extinguisher primers in parallel (section 3).
The key requirement of this directive is that all affected Sikorsky S-76A helicopters must implement the modifications outlined in Sikorsky Alert Service Bulletin No. 76-26-1. This modification is necessary to ensure that the fire extinguisher harness is more reliable in the event of an engine fire (section 4). Compliance must be achieved within 100 hours of time in service after 30 April 1985, which means operators must ensure that these modifications are completed well within this timeframe (section 5). Failure to adhere to this directive could result in the aircraft being deemed unairworthy, leading to potential grounding and other regulatory consequences.
Operators and entities governed by these regulations must ensure that they have the appropriate technical personnel and resources to perform the required modifications as per the Sikorsky Alert Service Bulletin. This includes keeping up-to-date records and documentation to demonstrate compliance with the directive. The onus is on the operator to ensure that their maintenance and modification processes align with CASA's requirements (section 6). Non-compliance with the specified deadlines and procedures can result in significant penalties, including fines and potential legal action against the operator or the manufacturer for any subsequent safety incidents arising from non-compliance (section 7).
In the event of a breach of this directive, the penalties can be severe. CASA may impose fines and other administrative penalties against the operator or the manufacturer. In some cases, the breach could lead to the suspension or revocation of the aircraft's airworthiness certificate, which would prevent the aircraft from operating until the required modifications are completed and CASA is satisfied with the compliance (section 8). Additionally, there may be civil or criminal liability for any accidents or incidents that occur due to non-compliance, further underscoring the importance of adhering to these safety directives (section 9).