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-76/38 Main Rotor Gear Box No. 1 and No. 2 Input Bevel
Pinion Housing Assemblies - Inspection
Applicability: As per the Requirement Document. Requirement: Sikorsky S.B. No. 76-66-19.
Compliance: 1. Prior to the issue of an initial Certificate of Airworthiness; or
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2. Prior to the installation of a MRGB called up in the Requirement Document.
Background: During the overhaul of a gearbox, the manufacturer found a torque loss on the input bevel pinion housing assembly retaining nuts.
Overview
The Civil Aviation Regulations 1998 (Cth), amended through the legislative instrument F2006B06719, were enacted to address specific safety concerns regarding the Sikorsky S-76 Series Helicopters. This legislative instrument is part of a broader regulatory framework overseen by the Civil Aviation Safety Authority (CASA) and was introduced to mitigate risks associated with identified mechanical issues in the helicopter's main rotor gear box. Specifically, the instrument targets the inspection of the No. 1 and No. 2 Input Bevel Pinion Housing Assemblies to ensure airworthiness and compliance with safety standards. The policy objective behind this directive is to enhance flight safety by preventing potential mechanical failures that could arise from undetected torque loss in the retaining nuts of the gearboxes, as stipulated in Sikorsky S.B. No. 76-66-19. This directive underscores CASA's commitment to maintaining high safety standards in civil aviation by mandating specific inspections before the issuance of a Certificate of Airworthiness or the installation of a newly overhauled gearbox.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, outlines the Civil Aviation Safety Authority’s schedule of airworthiness directives, which includes the requirements for Sikorsky S-76 Series Helicopters. This legislation applies to all aircraft within its scope, ensuring compliance with airworthiness directives (AD) such as AD/S-76/38, which mandates inspections of the main rotor gear box No. 1 and No. 2 input bevel pinion housing assemblies. These directives are applicable to all operators of the affected Sikorsky S-76 helicopters, regardless of their location within the Commonwealth of Australia, thereby establishing a national scope for compliance. The regulations require inspections either prior to the issue of an initial Certificate of Airworthiness or prior to the installation of a main rotor gearbox called up in the Requirement Document, as per Sikorsky S.B. No. 76-66-19. The legislation ensures that all relevant aircraft meet the safety standards set by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39 and specifically within the Schedule of Airworthiness Directives, include a directive (AD/S-76/38) that pertains to Sikorsky S-76 series helicopters (section 39-105). This directive mandates an inspection of the main rotor gearbox No. 1 and No. 2 input bevel pinion housing assemblies. The applicability of this directive is determined by the Requirement Document, specifically Sikorsky S.B. No. 76-66-19. The compliance requirements include an inspection either before the issuance of an initial Certificate of Airworthiness or before the installation of a main rotor gearbox that is called up in the Requirement Document.
The obligations imposed by this directive are clear and specific. Owners and operators of Sikorsky S-76 series helicopters must ensure that the main rotor gearbox No. 1 and No. 2 input bevel pinion housing assemblies are inspected in accordance with the directive's requirements. This inspection must be completed by qualified personnel, as stipulated by the manufacturer, and any findings must be documented appropriately. The directive ensures that the identified issue with the torque loss on the input bevel pinion housing assembly retaining nuts is addressed, thereby maintaining the airworthiness and safety of the aircraft.
Failure to comply with the provisions of this airworthiness directive can result in significant consequences. The Civil Aviation Safety Authority (CASA) may take enforcement action against non-compliance, which could include the suspension or revocation of the aircraft's Certificate of Airworthiness. Additionally, operators may face penalties as prescribed by the Civil Aviation Act 1988. The maximum penalties for breaches of these regulations can include substantial fines and, in some cases, imprisonment for individuals found guilty of serious non-compliance. It is crucial for all parties involved to adhere to these requirements to avoid such severe repercussions.