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-76/12 Upper Deck Flight Controls Installation - Modification
7/80
Applicability: All models S76 with S/Nos. 76003 and 76005, 760001 to 760006, 760009 and
760011 to 760015.
Document: Sikorsky CSB 76-67-1.
Compliance: Within 100 hours time in service after 31 July 1980.
Background: Rework of a bracket and angle is necessary to increase the clearances for rigging pin installation and roll gradient spring cylinder operation.
Overview
The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, address various safety concerns in civil aviation, including specific directives for maintaining the airworthiness of aircraft. The legislation is overseen by the Civil Aviation Safety Authority (CASA), which issues airworthiness directives (ADs) to ensure the safe operation of aircraft within Australia. One such directive, AD/S-76/12, focuses on Sikorsky S-76 Series Helicopters, specifically addressing modifications to the upper deck flight controls. This directive was introduced to mitigate risks associated with insufficient clearances for rigging pin installation and roll gradient spring cylinder operation. The policy objective is to enhance flight safety by ensuring that specified helicopter models meet critical maintenance standards. Compliance with these directives is mandatory, and failure to adhere to the required timeframes can result in the grounding of affected aircraft.
Scope and Application
The Civil Aviation Regulations 1998, as detailed in Part 39 - 105 and the Civil Aviation Safety Authority Schedule of Airworthiness Directives, apply specifically to the Sikorsky S-76 series helicopters. The directive AD/S-76/12, which pertains to the upper deck flight controls installation, applies to all models S76 with specific serial numbers, including S/Nos. 76003 and 76005, as well as a range from 760001 to 760006, 760009, and 760011 to 760015. This regulation is essential for ensuring the airworthiness of these aircraft and mandates a modification to a bracket and angle to increase clearances for the rigging pin installation and roll gradient spring cylinder operation. Compliance with this directive is required within 100 hours of time in service after 31 July 1980, as specified in the document Sikorsky CSB 76-67-1. The scope of this legislation is limited to the mentioned helicopter models and specific serial numbers, and it is enforced under the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority. There are no stated exclusions or exemptions within the directive itself, although further interpretation and application may be subject to subordinate instruments or additional regulatory guidance.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39, Section 105, mandate specific airworthiness directives for certain aircraft, including the Sikorsky S-76 series helicopters. Specifically, AD/S-76/12 pertains to the installation modification of the upper deck flight controls (Section 7/80). This directive applies to all S76 models with specific serial numbers: 76003 and 76005, 760001 to 760006, 760009, and 760011 to 760015. The directive is documented in Sikorsky CSB 76-67-1 and requires compliance within 100 hours of time in service after 31 July 1980. The modification involves reworking a bracket and an angle to enhance clearances for the rigging pin installation and the roll gradient spring cylinder operation, addressing potential safety concerns.
The obligations imposed by this directive are clear and specific. Operators of the affected Sikorsky S-76 series helicopters must ensure that the required modifications to the upper deck flight controls are completed within the specified timeframe. This involves inspecting the relevant components and performing the necessary rework of the bracket and angle to meet the clearance requirements outlined in the directive. The compliance must be verified and documented to ensure that the modifications have been properly executed and that the aircraft meets the airworthiness standards set by the Civil Aviation Safety Authority.
Failure to comply with the requirements set out in AD/S-76/12 can lead to serious consequences. Under the Civil Aviation Act 1988, non-compliance with an airworthiness directive is an offence. The potential penalties for breaching these regulations include fines and, in severe cases, imprisonment. The exact penalties can vary depending on the specific circumstances of the breach, but the potential for significant financial and criminal repercussions underscores the importance of adhering to the directive. Operators must take the necessary steps to ensure that their aircraft meet the specified standards to avoid these serious consequences.