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-76/22 Main Rotor Control Servo Actuators - Inspection
for Balance Tube Passage
6/82
Applicability: All models.
Document: Sikorsky Alert SB 76-67-14A. NOTE: Helicopters previously inspected to SB 76-67- 14 are to be re-inspected.
Compliance: Within 30 hours time in service after 28 April 1982.
Background: Restricted flight control motion was found to be due to the omission of a passage in the servo oil return system.
Overview
The Civil Aviation Regulations 1998, specifically within Part 39, was enacted to ensure the safety and airworthiness of aircraft in Australian airspace. This regulation addresses the need to manage and mitigate risks associated with aircraft operation by setting standards and directives for maintaining the safety and operational readiness of aircraft. The Civil Aviation Safety Authority, as the enforcing body, aims to ensure that all aircraft meet stringent safety standards and comply with relevant directives to prevent incidents and accidents. The policy objective behind these regulations is to provide a robust framework for the oversight and management of civil aviation, thereby protecting public safety and fostering confidence in air travel.
One such directive, AD/S-76/22, pertains to the Sikorsky S-76 Series Helicopters and mandates the inspection of main rotor control servo actuators for the presence of a balance tube passage. This directive was introduced to address a specific issue where restricted flight control motion was identified due to the omission of this passage in the servo oil return system. The regulation requires that all models of the Sikorsky S-76 Series Helicopters be inspected within 30 hours of time in service after 28 April 1982, with a particular note that helicopters previously inspected under SB 76-67-14 must be re-inspected. This directive ensures that the identified safety concern is rectified, maintaining the airworthiness of the affected aircraft and preventing potential flight control issues.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, establish the Civil Aviation Safety Authority's Schedule of Airworthiness Directives which include provisions for the Sikorsky S-76 Series Helicopters. This legislation applies to all models of the Sikorsky S-76 Series Helicopters, mandating that inspections of the main rotor control servo actuators for the balance tube passage be conducted. The directive applies to any operator or entity that holds or operates these aircraft within the Commonwealth of Australia, ensuring adherence to safety standards set forth by the Civil Aviation Safety Authority. Compliance with the directive is required within 30 hours of time in service after 28 April 1982, with particular emphasis on re-inspecting helicopters that had previously been inspected according to Sikorsky Alert SB 76-67-14. The regulations do not specify exclusions, exemptions, or thresholds beyond what is outlined in the directive itself, and further detail or implementation may be provided through subordinate instruments.
Key Provisions
The main operative sections of the Civil Aviation Regulations 1998, specifically AD/S-76/22, address the inspection requirements for the balance tube passage in the main rotor control servo actuators of the Sikorsky S-76 series helicopters (Part 39 - 105). These sections mandate that all models of the Sikorsky S-76 helicopters must undergo an inspection to ensure the passage is correctly installed, as this was found to be omitted in previous inspections, leading to restricted flight control motion (Section 39 - 105). The inspection must be completed within 30 hours of the helicopter's time in service following the directive's effective date of 28 April 1982. This directive is based on Sikorsky Alert SB 76-67-14A, and helicopters that have already been inspected under SB 76-67-14 are required to be re-inspected.
The obligations and requirements imposed by these regulations are clear and specific. Helicopter operators must ensure that the main rotor control servo actuators are inspected by qualified personnel within the stipulated timeframe. This inspection should verify the existence and proper functionality of the balance tube passage in the servo oil return system. Compliance with this directive is not optional; it is mandatory for all Sikorsky S-76 series helicopters. The inspection must be logged in the aircraft's maintenance records, and any deficiencies identified must be rectified before the helicopter is returned to service.
Failure to comply with these directives can result in severe consequences. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement action against operators who do not adhere to the specified inspection requirements. The potential penalties for non-compliance can include fines, enforcement notices, and in severe cases, the grounding of the aircraft until the required inspections are completed and any deficiencies are rectified. Additionally, operators may face legal action, which could result in significant financial penalties and damage to their reputation. The specific penalties for non-compliance are not detailed in the directive but are typically enforced under the broader civil aviation regulations, which can include fines of up to $330,000 for corporations and $66,000 for individuals, as well as potential criminal charges for serious safety breaches.