COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Rolls Royce Turbine Engines - RB211 Series
AD/RB211/5
Amdt 2
Low Pressure Compressor Rotor (Fan) Axial Retention
1/83
Applicability: RB211-22B-02, RB211-524B-02, RB211-524B2-19, RB211-524B2-39, RB211-
524C2-19 engines and modules as specified in SB No. RB211-72-6574, Rev. 6.
Document: Rolls Royce SB No. RB211-72-6574, Rev. 6.
Note: FAA AD No. 82-12-05, Amdt. 39-4398 refers.
Compliance: In accordance with the requirement document.
Background: This Directive is amended in order to reference the latest revision to the manufacturer’s requirement document.
Overview
The Civil Aviation Regulations 1998, specifically under Part 39 - 106, introduces the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which aims to ensure the safety and airworthiness of aircraft operating in Australian airspace. One such directive, AD/RB211/5 Amendment 2, pertains to Rolls Royce turbine engines of the RB211 series, addressing issues with the Low Pressure Compressor Rotor (Fan) Axial Retention. This legislation was enacted to fill a critical gap in maintaining the safety standards for these specific engine models, ensuring compliance with international safety protocols and the manufacturer's latest requirements. The policy objective is to mitigate any potential risks associated with the specified engines, thereby enhancing overall aviation safety.
The Civil Aviation Regulations 1998 are administered by the Commonwealth of Australia, with CASA being the primary regulatory body responsible for enforcing these directives. The legislative instrument F2006B06565, which pertains to the RB211 series engines, is part of a broader effort to maintain stringent safety standards in civil aviation. This amendment updates the directive to align with the most recent revisions from Rolls Royce, as documented in their Service Bulletin No. RB211-72-6574, Revision 6, ensuring that operators of these engines comply with the latest safety requirements.
Scope and Application
The Civil Aviation Regulations 1998, specifically PART 39 - 106, addresses the safety directives for Rolls Royce Turbine Engines, focusing on the RB211 Series. This legislation applies to particular models of RB211 engines, namely the RB211-22B-02, RB211-524B-02, RB211-524B2-19, RB211-524B2-39, and RB211-524C2-19 engines and modules as identified in Service Bulletin No. RB211-72-6574, Revision 6. The directive mandates compliance with the specified requirement document to ensure the airworthiness of these engines, and it references an amendment by the Federal Aviation Administration (FAA) under AD No. 82-12-05, Amendment 39-4398. The scope of this regulation is nationwide, applying across the Commonwealth of Australia, and it is enforced by the Civil Aviation Safety Authority (CASA). There are no explicit exclusions or exemptions mentioned in the provided text, suggesting that the directive applies broadly to all relevant engines within the specified models. The application may be further defined or extended through subordinate instruments issued by CASA.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39, contain the Airworthiness Directives (AD) which are legally binding for the maintenance and operation of aircraft and engines. Section 106 of the Civil Aviation Regulations focuses on the Rolls Royce Turbine Engines of the RB211 series, detailing specific maintenance requirements. This is further clarified in AD/RB211/5 Amendment 2, which pertains to the Low Pressure Compressor Rotor (Fan) Axial Retention (section 1/83). This amendment applies to certain Rolls Royce engines and modules, specifically those listed as RB211-22B-02, RB211-524B-02, RB211-524B2-19, RB211-524B2-39, and RB211-524C2-19 as detailed in Service Bulletin (SB) No. RB211-72-6574, Revision 6. The compliance with this directive must be in line with the requirement document specified in Rolls Royce SB No. RB211-72-6574, Revision 6, and it references FAA AD No. 82-12-05, Amendment 39-4398.
The obligations imposed by this directive require aircraft operators and maintenance personnel to ensure that the specified engines and modules adhere to the latest revisions of the manufacturer's requirement document. This includes conducting necessary inspections and maintenance tasks to comply with the provisions of the directive. It is imperative that the engines are maintained according to the updated Service Bulletin to ensure airworthiness and safety. Non-compliance with these directives can lead to significant safety risks, including potential engine failures, which could endanger the aircraft and its occupants.
In the event of non-compliance with the Airworthiness Directive, there are serious legal consequences. Under the Civil Aviation Act 1988, any breach of these regulations can lead to criminal charges. The penalties for such offences can be severe, including substantial fines and imprisonment for individuals and corporations found guilty of non-compliance. The specific penalties are determined by the court but can include fines up to several thousand dollars and imprisonment for terms extending up to several years, depending on the severity of the breach and its impact on aviation safety. Additionally, the Civil Aviation Safety Authority (CASA) can impose administrative penalties and take enforcement actions, which may include grounding the aircraft until compliance is achieved.