COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Rolls Royce Turbine Engines - Viper Series
AD/VIPER/3 Blow Off Valve Operation Limit 3/90
Applicability: Viper Mk. 521, 522 engines.
Requirement: 1. Action in accordance with Rolls Royce Service Bulletin No. 75-A32, or
2. CAO 106 AD/RRT-V/13. Compliance: Effective 22 March 1990.
Background: This Directive has been reissued to require a revised blow-off valve operating point to reduce the possibility of engine surge or stall.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 106, under the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, address the safety and operational standards for aviation components, including Rolls Royce Turbine Engines. One such directive, AD/VIPER/3, was enacted to address the operational limits of the blow-off valve in Viper Mk. 521 and 522 engines, aiming to mitigate risks such as engine surge or stall. This directive, reissued to incorporate a revised blow-off valve operating point, was introduced to enhance safety in line with industry standards and Rolls Royce's service bulletin No. 75-A32. The policy objective is to ensure compliance with these safety measures, thereby maintaining the airworthiness of affected aircraft engines and safeguarding aviation safety. The directive was enacted by the Civil Aviation Safety Authority, ensuring adherence to the stringent safety standards set forth by the Commonwealth of Australia.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 106, pertains to the Civil Aviation Safety Authority’s schedule of Airworthiness Directives (ADs) and is applicable to the Viper Series Rolls Royce turbine engines, namely the Viper Mk. 521 and 522 engines. This legislative instrument applies to any person or entity involved in the operation, maintenance, or modification of these specified engines. The directive ensures compliance with safety standards by mandating adherence to Rolls Royce Service Bulletin No. 75-A32 or CAO 106 AD/RRT-V/13, both of which outline the necessary actions to be taken to mitigate the risk of engine surge or stall. The compliance requirement is effective from 22 March 1990, making it imperative for all relevant parties to implement the prescribed measures to maintain airworthiness. The scope of this legislation is national, extending across all jurisdictions within the Commonwealth of Australia, ensuring a uniform approach to aviation safety standards. There are no stated exclusions, exemptions, or thresholds in this particular AD, and its application is not extended or restricted through subordinate instruments.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 106, establish the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives (AD). One such directive, AD/VIPER/3, pertains to the blow-off valve operation limit for Rolls Royce Turbine Engines of the Viper Series (section 3/90). This directive applies to Viper Mk. 521 and 522 engines. The directive mandates that operators must take action in accordance with either Rolls Royce Service Bulletin No. 75-A32 or CAO 106 AD/RRT-V/13 (section 1). The directive became effective on 22 March 1990, aiming to address concerns regarding engine surge or stall by adjusting the blow-off valve operating point.
Operators of Viper Mk. 521 and 522 engines must ensure compliance with the AD/VIPER/3 directive to maintain the airworthiness of their aircraft. This involves following the specific instructions outlined in the Rolls Royce Service Bulletin No. 75-A32 or the Civil Aviation Order 106 AD/RRT-V/13. Compliance is crucial to ensure that the engines meet the required safety standards and to prevent potential issues such as engine surge or stall, which could compromise flight safety.
Failure to comply with AD/VIPER/3 may result in serious safety risks, as it directly affects the operational reliability and safety of the affected engines. While the specific penalties for non-compliance are not detailed within the directive itself, CASA can impose various measures under the broader Civil Aviation Regulations. These may include fines, suspension of airworthiness certificates, and other regulatory actions to enforce compliance. The exact penalties would depend on the severity of the non-compliance and the specific circumstances surrounding the breach.
Additionally, non-compliance with airworthiness directives can have broader implications, potentially leading to civil or criminal liability for operators and manufacturers. Under Australian law, significant breaches of safety regulations can result in substantial penalties, including fines and imprisonment for individuals found guilty of negligence or misconduct. It is, therefore, imperative for operators and manufacturers to adhere strictly to the requirements set out in AD/VIPER/3 to avoid these serious consequences.