COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Sikorsky S-76 Series Helicopters
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
AD/S-76/63 Main Rotor Blade Root and Pocket Separation 7/2000
TX
Applicability: All models S76 with main rotor blades not repaired in accordance with Overhaul and Repair Instruction (ORI) No. 76150-023 Revision A dated 26 May 2000.
Requirement: Action in accordance with Sikorsky Aircraft Corp. ASB No. 76-65-50 dated 25 May 2000.
Note: FAA Emergency AD 2000-11-52 refers.
Compliance: Before further flight after the effective date of this directive.
This Airworthiness Directive becomes effective on 1 June 2000.
Background: This directive is issued due to a report of a 20 inch crack in the root end pocket of a main rotor blade and three reports of root end pocket separation of 4 to 6 foot sections of main rotor blade during flight. These unsafe conditions are attributed to improper manufacture of certain main rotor blade skins.
Bernard Malcolm Hole
Delegate of the Civil Aviation Safety Authority 30 May 2000
The above AD is notified in the Commonwealth of Australia Gazette on 1 June 2000.
Overview
The Civil Aviation Regulations 1998 (CAR 1998) were enacted to provide comprehensive regulations governing civil aviation in Australia, addressing various aspects of aircraft safety, operation, and maintenance. One particular legislative instrument, F2006B06739, was introduced to specifically address safety concerns related to the Sikorsky S-76 series helicopters. This Airworthiness Directive (AD) was issued by the Civil Aviation Safety Authority (CASA) to correct unsafe conditions identified with the main rotor blade root and pocket separation in certain S76 models. The directive aims to rectify these issues by requiring specific actions to be taken by operators to ensure the airworthiness of their aircraft, thereby enhancing flight safety. The AD became effective on 1 June 2000, following reports of significant structural failures in main rotor blades attributed to improper manufacturing processes.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39 - 105 and the Airworthiness Directives, mandate the maintenance and safety standards for aircraft operating in Australia. This directive pertains to the Sikorsky S-76 Series Helicopters, addressing specific concerns related to the separation of main rotor blade roots and pockets. The directive applies to all models of S76 helicopters with main rotor blades that have not been repaired according to the Overhaul and Repair Instruction (ORI) No. 76150-023 Revision A dated 26 May 2000. The requirement is that these helicopters must adhere to the actions specified in Sikorsky Aircraft Corp. ASB No. 76-65-50 dated 25 May 2000, with a reference to FAA Emergency AD 2000-11-52. Compliance with these directives is mandatory before any further flight after the effective date of this directive, which is 1 June 2000. This directive underscores the importance of maintaining stringent safety standards to mitigate risks associated with identified unsafe conditions, thereby ensuring the continued airworthiness of the aircraft within Australia's jurisdiction.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, outlines the Airworthiness Directive for Sikorsky S-76 Series Helicopters, which is encapsulated in AD/S-76/63 (section 7/2000TX). This directive applies to all S76 models with main rotor blades that have not been repaired according to Overhaul and Repair Instruction (ORI) No. 76150-023 Revision A dated 26 May 2000 (applicability section). The directive mandates that the action specified in Sikorsky Aircraft Corp. ASB No. 76-65-50 dated 25 May 2000 must be taken under the conditions and instructions outlined in the requirement section, and before further flight after the effective date of this directive, which is 1 June 2000 (compliance section).
Operators and owners of the affected Sikorsky S-76 helicopters must ensure compliance with the specified action to rectify the unsafe conditions identified in the directive. This involves following the instructions from Sikorsky Aircraft Corp. ASB No. 76-65-50, which likely includes detailed procedures for the inspection and repair of the main rotor blade root and pocket separation. The directive emphasises that any corrective action must be undertaken before the aircraft is flown again after the directive's effective date. Failure to comply with these instructions could potentially compromise the airworthiness of the helicopter, thereby posing significant safety risks.
Failure to adhere to the requirements set out in this Airworthiness Directive can lead to severe consequences. As per the regulatory framework of the Civil Aviation Regulations 1998, non-compliance with an Airworthiness Directive is a breach of the statutory requirements. Such breaches can result in the imposition of civil or criminal penalties. In terms of civil consequences, operators may face fines or other penalties imposed by the Civil Aviation Safety Authority (CASA). For criminal consequences, the severity of the penalty can vary, but it may include imprisonment, particularly if the non-compliance is deemed to have contributed to an aviation accident or incident. The exact penalties are determined by the relevant courts and can depend on the specific circumstances of the non-compliance.