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-76/14 Fuselage Bulkhead - Engine Support
Fitting Area - Inspection and Modification Applicability: All models S-76 with S/Nos. 76003, 76005, and 76006; 760001 to 760024. Document: Sikorsky CSB No. 76-53-5A.
Compliance: As per requirement document.
10/80
Background: The manufacturer has received reports of cracks being found in the engine support bulkhead at STA.255.
Overview
The Civil Aviation Safety Authority (CASA) introduced the Civil Aviation Regulations 1998, particularly Part 39 - 105, as a legislative instrument to ensure the safety and efficiency of civil aviation in Australia. This legislation was enacted to address the need for stringent regulatory oversight and to provide clear directives for maintaining airworthiness standards. Specifically, the regulation targets Sikorsky S-76 Series Helicopters, identifying and addressing a safety concern related to the fuselage bulkhead in the engine support fitting area. The regulation was issued to mandate inspections and modifications to mitigate risks associated with cracks in the engine support bulkhead at Station 255. The policy objective is to enhance the safety of air operations by ensuring that aircraft meet specific maintenance and structural integrity standards.
The Australian Parliament enacted these regulations to provide a robust framework for civil aviation safety, reflecting the importance of preventing accidents and ensuring the reliability of aircraft operations. CASA’s authority to issue Airworthiness Directives under these regulations aims to proactively address safety issues, thereby protecting both the public and aviation personnel. Compliance with these directives is mandatory for the specified Sikorsky S-76 models, as outlined in the regulation to ensure that any identified structural vulnerabilities are rectified.
Scope and Application
The Civil Aviation Safety Authority (CASA) has issued Airworthiness Directive (AD) S-76/14 as part of the Civil Aviation Regulations 1998 to address safety concerns related to specific Sikorsky S-76 Series helicopters. This directive applies to all models S-76 with serial numbers ranging from 76003 to 76006, and from 760001 to 760024. The directive mandates that the engine support bulkhead fitting area, particularly at Station 255, be inspected and modified as per the requirement document Sikorsky CSB No. 76-53-5A to prevent and rectify potential cracks that could compromise the structural integrity of the aircraft. Compliance with this directive is mandatory for all affected aircraft operators and must be completed in accordance with the specified timeframes. This regulation is applicable nationally, enforcing stringent safety standards across all states and territories within the Commonwealth of Australia.
Key Provisions
The key sections of the Civil Aviation Regulations 1998, specifically Part 39 - 105, mandate that certain Sikorsky S-76 Series helicopters undergo an inspection and, if necessary, modification of the fuselage bulkhead in the engine support fitting area. This requirement is outlined in AD/S-76/14, which applies to all models of the S-76 series with specific serial numbers, namely 76003, 76005, and 76006, as well as 760001 to 760024. Compliance with these directives is expected to be in accordance with the manufacturer’s requirement document, Sikorsky CSB No. 76-53-5A.
Under this legislation, the primary obligation on the parties involved, particularly the operators of the specified Sikorsky S-76 helicopters, is to ensure that the mandated inspection and modifications are carried out. Operators must meticulously adhere to the guidelines set forth in Sikorsky CSB No. 76-53-5A, which includes a detailed inspection process and specific procedures for any required modifications to the engine support bulkhead at STA.255. These measures are critical to maintaining the airworthiness and safety standards of the aircraft, as mandated by the Civil Aviation Safety Authority.
Failure to comply with the requirements of AD/S-76/14 can result in significant legal consequences. The Act stipulates that non-compliance with airworthiness directives can lead to enforcement actions, including potential civil penalties. Under the Civil Aviation Act 1988, non-compliance with such directives may also result in criminal charges, with maximum penalties for individuals including fines of up to $21,000 and imprisonment for up to one year. For corporations, the fines can be substantially higher, reflecting the serious nature of ensuring aircraft safety and compliance with regulatory standards.