COMMONWEALTH OF AUSTRALIA (Civil Aviation 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 CAR 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/12 Oil System Venting 1/2003
Applicability: Rotax 912 A/F/S series and Rotax 914 F series engines.
Requirement: 1. Carry out the instructions as detailed in paragraphs 3.1.1 through 3.1.4 of Rotax Service Bulletin (SB) 912-036R1 or Rotax SB 914-022R1, whichever is applicable.
2. Carry out the instructions as detailed in paragraphs 3.1.5 through 3.1.7 of Rotax Service Bulletin (SB) 912-036R1 or Rotax SB 914-022R1, whichever is applicable.
3. Carry out engine test run as detailed in paragraph 3.2 of Rotax Service Bulletin (SB) 912-036R1 or Rotax SB 914-022R1, whichever is applicable.
Note: Austrian AD 113 R1 refers.
Compliance: 1. For engines addressed in paragraph 1.5) a) of the applicable SB - unless previously accomplished, prior to further flight.
2. a. For engines addressed in paragraph 1.5) b) of the applicable SB - unless previously accomplished, for engines with up to 50 hours flight time, within 5 flight hours from the effective date of this Directive.
b. For engines exceeding 50- flight hours operation no action is required.
3. Following completion of requirement 1 or 2, prior to further flight.
This Airworthiness Directive becomes effective on 23 January 2003.
Background: Incorrect venting of the lubrication system can lead to damage to the valve train with subsequent engine failure.
James Coyne
Delegate of the Civil Aviation Safety Authority 27 November 2002
The above AD is notified in the Commonwealth of Australia Gazette on 18 December 2002.
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Overview
The Civil Aviation Regulations 1998 (CAR 1998) are a comprehensive set of rules and regulations designed to ensure the safety of civil aviation in Australia. Enacted by the Australian Parliament, these regulations are administered by the Civil Aviation Safety Authority (CASA), which is responsible for enforcing compliance and ensuring that aviation operations meet the required safety standards. The regulations address various aspects of aviation, including the airworthiness of aircraft, the licensing of pilots and other aviation personnel, and the operation of aircraft in Australian airspace. One specific aspect covered by the CAR 1998 is the issuance of Airworthiness Directives (ADs), which are mandatory orders issued by CASA to address identified safety issues. These directives compel aircraft operators to take corrective actions to ensure the continued airworthiness of their aircraft. The AD in question, AD/ROTAX/12 Oil System Venting 1/2003, was introduced to address the problem of incorrect venting of the lubrication system in certain Rotax engines, which can lead to damage to the valve train and subsequent engine failure. This directive mandates specific corrective actions to mitigate this safety risk, ensuring the continued safe operation of the affected aircraft.
Scope and Application
The Airworthiness Directive (AD) issued under Part 39 - 106 of the Civil Aviation Regulations 1998 applies specifically to Rotax 912 A/F/S series and Rotax 914 F series engines. The AD mandates corrective actions to address issues arising from incorrect venting of the lubrication system, which can lead to potential damage to the valve train and subsequent engine failure. The directive requires adherence to specific instructions detailed in designated Rotax Service Bulletins, with particular attention to compliance timelines based on the flight hours of the affected engines. The AD is applicable on a Commonwealth level, as it is issued by the Civil Aviation Safety Authority (CASA) and is binding within the jurisdiction of the Commonwealth of Australia. There are no exclusions or exemptions specified within the directive itself, although compliance thresholds are provided based on the flight hours of the engines. The AD may be subject to further interpretation or modification through subordinate instruments or subsequent bulletins issued by CASA or the engine manufacturer.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 106, includes an Airworthiness Directive (AD) concerning the oil system venting for certain Rotax engines. According to section 39.1 (1) of the Civil Aviation Regulations 1998, the Civil Aviation Safety Authority (CASA) delegate issues this AD, mandating specific actions to rectify an unsafe condition. The AD applies to Rotax 912 A/F/S series and Rotax 914 F series engines, as stated in the applicability section. The directive requires compliance with the instructions detailed in the requirement section, and it must be carried out under the circumstances and within the timeframe outlined in the compliance section.
The obligations imposed by this AD include carrying out detailed instructions specified in paragraphs 3.1.1 through 3.1.7 of the relevant Rotax Service Bulletins (SB) 912-036R1 or 914-022R1, and conducting an engine test run as detailed in paragraph 3.2 of the respective bulletins. For engines mentioned in paragraph 1.5(a) of the applicable bulletin, these actions must be completed before further flight unless previously accomplished. For engines with up to 50 hours of flight time, the actions must be undertaken within 5 flight hours from the effective date of the AD. Engines with more than 50 flight hours are exempt from this requirement. The AD requires completion of the specified requirements before any further flight.
Failure to comply with this AD may result in serious consequences, including potential damage to the valve train and subsequent engine failure, which could lead to accidents or incidents. Although the AD itself does not specify penalties, non-compliance with regulations governing airworthiness can result in enforcement actions by CASA. These actions can include fines, suspension or revocation of aircraft or engine certificates, and other civil or criminal penalties as provided under relevant aviation legislation. The severity of penalties may depend on the extent of non-compliance and its impact on aviation safety.