COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Robinson R22 Series Helicopters
AD/R22/5
Amdt 2
Main Gearbox Flexible Coupling Yokes - Inspection 10/81
Applicability: All R22 series helicopters fitted with P.N. A192 and P.N. A194 yokes. Document: Robinson Service Bulletin SB-11.
Compliance: At periods not exceeding 10 hours time in service.
Background: The manufacturer advises of the failure of the main gearbox coupling yoke on three helicopters. AD/R22/5A is raised in issue to include all P.N. A192 and A194 yokes.
Overview
The Civil Aviation Regulations 1998, under Part 39, specifically address airworthiness directives for various aircraft, including the Robinson R22 Series Helicopters. One such directive, AD/R22/5 Amendment 2, pertains to the inspection of main gearbox flexible coupling yokes for all R22 series helicopters equipped with parts numbered A192 and A194. This directive was introduced to address the problem of yoke failures in the main gearbox coupling, as reported by the manufacturer following incidents on three helicopters. The objective of this directive is to ensure compliance with the manufacturer's recommended inspection periods, which should not exceed 10 hours of time in service, as outlined in Robinson Service Bulletin SB-11. The enactment of these regulations by the Australian Government aims to maintain the highest standards of aviation safety and reliability.
The Civil Aviation Regulations 1998 were enacted by the Parliament of the Commonwealth of Australia to regulate civil aviation within Australia, ensuring safety, efficiency, and environmental protection. The policy objective behind the introduction of airworthiness directives such as AD/R22/5 Amendment 2 is to enhance the safety of civil aviation by mandating specific maintenance and inspection requirements for aircraft components. This directive is part of the ongoing efforts by the Civil Aviation Safety Authority to mitigate risks associated with known mechanical failures and to ensure that aircraft remain airworthy throughout their operational life. The regulations are designed to provide clear and enforceable standards that all operators must adhere to, thereby safeguarding both the public and aviation personnel.
Scope and Application
The Civil Aviation Regulations 1998, as amended, apply to all R22 series helicopters that are fitted with the specified yokes, P.N. A192 and P.N. A194. This legislation falls under the purview of the Civil Aviation Safety Authority and is designed to ensure the safety and airworthiness of these helicopters by mandating specific inspection procedures. The regulation applies nationally, with the Civil Aviation Safety Authority exercising oversight across the Commonwealth of Australia. The requirement is clear: inspections must be conducted at intervals not exceeding 10 hours of time in service following the guidance provided in Robinson Service Bulletin SB-11. This directive is imperative for maintaining the operational integrity of the helicopters and preventing potential failures that could lead to safety issues. The application of this regulation is not limited by state or territory boundaries, ensuring a consistent approach to safety across Australia. There are no exclusions or exemptions specified within the directive, indicating that all affected helicopters must comply without exception.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, address the airworthiness directives for the Robinson R22 series helicopters. In this context, AD/R22/5 Amendment 2 is of particular relevance, focusing on the inspection of the main gearbox flexible coupling yokes. This directive applies to all R22 series helicopters fitted with P.N. A192 and P.N. A194 yokes (section 10/81). Compliance with this directive is mandatory, and it is supported by the Robinson Service Bulletin SB-11. The requirement is that inspections must be conducted at periods not exceeding 10 hours of time in service to ensure the continued airworthiness of the affected helicopters.
Under these regulations, operators and owners of the specified Robinson R22 series helicopters are obligated to adhere strictly to the inspection intervals and procedures outlined in AD/R22/5 Amendment 2. This includes ensuring that the main gearbox flexible coupling yokes are inspected within the specified 10-hour intervals. These inspections are critical for identifying and mitigating potential failure risks, as highlighted by the manufacturer’s reports of failures on three helicopters. The compliance with this directive is not only a legal requirement but also a vital safety measure to prevent in-flight incidents.
Failure to comply with the airworthiness directive AD/R22/5 Amendment 2 can result in severe consequences. Non-compliance with these safety regulations can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions may include fines, operational restrictions, or even the grounding of non-compliant aircraft. The severity of the penalties is determined based on the nature and extent of the non-compliance, with potential maximum penalties that can be imposed under Australian law. Ensuring adherence to these directives is therefore not only a legal necessity but also a fundamental aspect of maintaining the safety standards expected in civil aviation.