COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
AlliedSignal (Garrett/AiResearch) Turbine Engines - TFE731 Series
AD/TFE731/25 Low Pressure Turbine Nozzle A5 Airseal 11/94 DM
Applicability: TFE731-3 series engines not incorporating Allied Signal Service Bulletin TFE731- 72-3502 or TFE731-72-3509 as applicable.
Requirement: Replace the low pressure turbine nozzle A5 airseal in accordance with Allied Signal Service Bulletin TFE731-72-3502 or TFE731-72-3509 as applicable.
Note: This Directive provides the terminating action for CAO105 Airworthiness Directives, AD/HS125/130 Amdt 1, AD/IAI-W/16 Amdt 1 and AD/CESSNA 650/5.
Compliance: Effective 14 September 1994:
Airseals with less than 500 hours total time in service since new; prior to accumulating 650 hours total time in service.
Airseals with more than 500 hours total time in service since new; within 150 hours time in service.
Background: This Directive has been issued to require replacement of certain low pressure turbine nozzle A5 airseals. The requirement follows reports of uncontained 1st stage low pressure turbine disc failures in AlliedSignal TFE731-3 engines.
The turbine disc failures were attributed to failure of the A5 airseal.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 106, addresses safety directives for various aircraft components and systems, ensuring that civil aviation in Australia adheres to stringent safety standards. Enacted by the Commonwealth of Australia, these regulations aim to mitigate risks associated with airworthiness and operational safety. This legislative instrument, F2006B07405, pertains to AlliedSignal (Garrett/AiResearch) Turbine Engines of the TFE731 Series, targeting issues with the low pressure turbine nozzle A5 airseal. The policy objective is to mandate the replacement of these airseals to prevent uncontained failures of the 1st stage low pressure turbine disc, which can have serious safety implications. The directive specifies that the replacement must be carried out in accordance with Allied Signal Service Bulletin TFE731-72-3502 or TFE731-72-3509, depending on the engine's service history.
Scope and Application
The Civil Aviation Regulations 1998, as part of the legislative framework administered by the Civil Aviation Safety Authority (CASA), extend their regulatory reach to all civil aviation activities within Australia, ensuring adherence to safety standards for aircraft operations. Specifically, Part 39 of these regulations encompasses Airworthiness Directives (ADs) that mandate compliance with safety standards for various aircraft components and systems. AD/TFE731/25 pertains to the AlliedSignal (Garrett/AiResearch) Turbine Engines of the TFE731 series, focusing on the replacement of the low pressure turbine nozzle A5 airseal. This directive applies to TFE731-3 series engines that do not incorporate specific Allied Signal Service Bulletins (TFE731-72-3502 or TFE731-72-3509), which are identified as essential for airworthiness. The regulation mandates that airseals with less than 500 hours of total time in service since new be replaced prior to accumulating 650 hours, while those with more than 500 hours must be replaced within 150 hours of service. This directive effectively terminates previous airworthiness directives related to the TFE731 series engines, ensuring streamlined compliance with updated safety standards.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39, contains several sections that are particularly relevant to the AlliedSignal (Garrett/AiResearch) Turbine Engines - TFE731 Series, as detailed in AD/TFE731/25 (1). This Airworthiness Directive mandates the replacement of the low pressure turbine nozzle A5 airseal for TFE731-3 series engines that do not incorporate the modifications specified in Allied Signal Service Bulletin TFE731-72-3502 or TFE731-72-3509 (2). The directive applies to engines that have not yet incorporated these specific service bulletins, necessitating compliance through replacement of the airseal.
Under these regulations, the primary requirement is the replacement of the low pressure turbine nozzle A5 airseal, as per the specified service bulletins (3). This applies to airseals with less than 500 hours of total time in service since new, before they accumulate 650 hours of total time in service, and for those with more than 500 hours of total time in service, within 150 hours of that time (4). The directive also serves to terminate other previous directives, including AD/HS125/130 Amdt 1, AD/IAI-W/16 Amdt 1, and AD/CESSNA 650/5, indicating a comprehensive update to the safety standards governing these engines (5).
The obligations imposed by this Act on the parties involved, particularly aircraft operators and maintenance organisations, are stringent. They must ensure that the specified airseals are replaced according to the timelines and procedures outlined in the service bulletins (6). This includes conducting thorough inspections to identify the airseals that fall under the applicability criteria and scheduling the necessary replacements accordingly (7). Failure to comply with these obligations could result in significant safety risks, including potential uncontained engine failures, which could endanger both the aircraft and its occupants.
Failure to comply with these directives can result in severe consequences. The legislation does not explicitly outline the specific civil or criminal penalties for non-compliance; however, non-compliance with Civil Aviation Regulations can lead to enforcement actions by the Civil Aviation Safety Authority (CASA) (8). This may include fines, suspension or revocation of operating certificates, and other regulatory actions that can impact the operational status of the aircraft (9). Additionally, in cases where non-compliance results in accidents or incidents, the penalties can be more severe, potentially including criminal charges if gross negligence or intentional disregard for safety regulations is established (10).