COMMONWEALTH OF AUSTRALIA (Civil Aviation Safety Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
Rotax Piston Engines
AD/ROTAX/15 Inspection of Exhaust Bends 12/2003
Applicability: Rotax 914 F series engines with Serial Number (S/N) 4,420.001 up to 4,420.363, if equipped with genuine Rotax exhaust bends Part Number (PN) 979420/421/422, 979430/431/432, 979440/441/442, and 979450/451/452.
Requirement: 1. Carry out a detailed visual inspection of the exhaust bends (exhaust tubes between cylinder head and exhaust) in accordance with instructions contained in Rotax Service Bulletin (SB) 914-017R1.
2. If cracks are detected when carrying out Requirement 1, replace the exhaust bend in accordance with the relevant Maintenance Manual.
Note: Austrian CAA AD 106R1 refers.
Compliance: For Requirement 1: Every 50 hours time-in-service (TIS) from the effective date of this Directive.
For Requirement 2: Before further flight.
This Airworthiness Directive becomes effective on 27 November 2003.
Background: Cracks have been detected on Rotax engine exhaust bends which could have been caused by a number of reasons outlined in the SB relevant to this Directive. The Austrian CAA requires inspection of the exhaust bends at regular intervals.
Jim Coyne
Delegate of the Civil Aviation Safety Authority 14 October 2003
The above AD is notified in the Commonwealth of Australia Gazette on 5 November 2003.
Overview
The Civil Aviation Safety Regulations 1998, enacted by the Commonwealth of Australia, address the need for ensuring the safety of civil aviation within the country. This legislation, administered by the Civil Aviation Safety Authority (CASA), is aimed at maintaining the airworthiness of aircraft and aeronautical products to mitigate safety risks. The policy objective is to establish a robust regulatory framework that mandates regular inspections and maintenance to prevent potential safety hazards. A specific instance of this legislative intent is evident in Airworthiness Directive AD/ROTAX/15, issued in 2003, which targets the inspection and replacement of exhaust bends in certain Rotax 914 F series engines to address detected cracks that could compromise flight safety. This directive underscores the regulatory authority's commitment to proactive safety measures by requiring detailed inspections at specified intervals and immediate corrective action upon identifying defects.
Scope and Application
The Civil Aviation Safety Regulations 1998, specifically Part 39 - 106, encompasses the Airworthiness Directives issued under the authority of the Civil Aviation Safety Authority (CASA). These regulations apply to particular aircraft or aeronautical products, in this case, Rotax 914 F series engines with specified serial numbers, which are used within the aviation industry. The directive mandates that inspections and repairs must be carried out as per the outlined requirements, which include a detailed visual inspection of the exhaust bends and the replacement of any bends found to be cracked, in accordance with the relevant service bulletin and maintenance manual instructions. The directive applies nationwide and its implementation is overseen by CASA, which has the authority to delegate its responsibilities to designated officials. The directive becomes effective from the date of its notification in the Commonwealth of Australia Gazette, and compliance is mandatory for the specified aircraft within the prescribed timeframes.
Key Provisions
The Civil Aviation Safety Regulations 1998, Part 39 - 106, includes an Airworthiness Directive (AD) pertaining to specific Rotax 914 F series engines. This AD, specifically AD/ROTAX/15, requires certain inspections and actions to be taken to ensure the safety of the aircraft using these engines. According to section (a), the directive applies to Rotax 914 F series engines with serial numbers ranging from 4,420.001 to 4,420.363 that are equipped with specific genuine Rotax exhaust bends. The requirements, outlined in section (b), include a detailed visual inspection of the exhaust bends every 50 hours of time-in-service, as per the instructions in Rotax Service Bulletin (SB) 914-017R1, and the replacement of any cracked exhaust bends before further flight. Section (c) indicates that the compliance timeframes for these requirements are effective from the date the directive was issued, 27 November 2003.
The obligations imposed by this AD on the parties governed include the requirement to conduct the specified inspections and replacements as mandated. Aircraft operators and maintenance personnel must ensure that these actions are carried out in accordance with the detailed instructions provided in the Rotax Service Bulletin, which outlines the precise methodology for conducting the inspections and making necessary replacements. The directive is clear that any detected cracks in the exhaust bends must be addressed immediately by replacing the affected parts before the aircraft is flown again, thereby preventing potential unsafe conditions from arising.
Failure to comply with the requirements set forth in this Airworthiness Directive may result in significant consequences. The regulations governing these directives are stringent, and non-compliance could lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Specifically, CASA may take legal action against the aircraft operator or maintenance personnel responsible for the oversight. Penalties for non-compliance can include fines and potential grounding of the affected aircraft, which can lead to substantial operational disruptions and financial losses. The exact penalties are not explicitly stated in the directive but are subject to the broader regulatory framework under which CASA operates.