COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Turbomeca Turbine Engines - Turmo Series
AD/TURMO/4 Fuel Control - Acceleration Unit 10/92
Applicability: All Turmo IV A, B, C, CA and CB engines.
Requirement: Unless previously carried out, action in accordance with Turbomeca Service Bulletin No 088.
Note: DGAC AD 92-115(B) refers.
Compliance: Prior to 30 September 1992.
Background: In certain operating conditions the vibratory torsion modes between the gearbox and engine could damage both engine flexible couplings.
Overview
The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority (CASA), were enacted to regulate civil aviation safety in Australia. Part 39 of these regulations, specifically in relation to airworthiness directives, addresses the safety and operational standards for various aircraft components, including engines. One such directive, AD/TURMO/4, focuses on ensuring the safety of Turbomeca Turmo Series engines through specific maintenance actions. This directive was introduced to address potential damage to engine flexible couplings caused by vibratory torsion modes in certain operating conditions, as referenced in Turbomeca Service Bulletin No 088 and DGAC AD 92-115(B). The policy objective is to mitigate risks and maintain the integrity of the engines, thereby ensuring the safety of all flights using these engines. Compliance with this directive is mandatory for all Turmo IV A, B, C, CA, and CB engines, with a requirement to take action prior to 30 September 1992.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 106, applies to all Turmo IV A, B, C, CA, and CB engines manufactured by Turbomeca, as detailed in the Civil Aviation Safety Authority Schedule of Airworthiness Directives AD/TURMO/4. This legislation mandates that unless the action specified in Turbomeca Service Bulletin No 088 has already been carried out, operators must comply with this directive. The directive is grounded in DGAC AD 92-115(B) and requires adherence prior to 30 September 1992. The legislation aims to prevent potential damage to engine flexible couplings caused by vibratory torsion modes between the gearbox and engine under specific operating conditions. The regulations have a broad jurisdictional reach, applying across the Commonwealth of Australia and are enforced by the Civil Aviation Safety Authority. There are no explicit exclusions, exemptions, or thresholds mentioned in the directive, and its application is not extended or restricted through subordinate instruments.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39, section 106, detail the Airworthiness Directives for certain turbine engines. The regulation AD/TURMO/4 addresses issues related to the Turbomeca Turmo Series engines, focusing on the fuel control acceleration unit (10/92). The directive applies to all Turmo IV A, B, C, CA, and CB engines (section 106). The requirement is that any action must be taken in accordance with Turbomeca Service Bulletin No 088 unless it has already been completed. The directive notes a reference to DGAC AD 92-115(B) for further context.
The obligations under this directive require all affected parties, such as aircraft operators and maintenance providers, to ensure that the specified actions are carried out on the designated engines. This involves following the instructions and procedures outlined in Turbomeca Service Bulletin No 088. Ensuring compliance with this directive is essential to maintaining the airworthiness of the aircraft using these engines. The directive necessitates that any required actions be completed before 30 September 1992 to prevent potential damage to the engine flexible couplings due to vibratory torsion modes under certain operating conditions.
The consequences of not adhering to this directive can be severe. Failure to comply with the AD/TURMO/4 regulation can result in non-compliance with airworthiness standards, potentially leading to safety issues and operational disruptions. Such non-compliance could result in enforcement actions by the Civil Aviation Safety Authority (CASA). Civil penalties for non-compliance may include fines or other monetary penalties, while criminal penalties could involve imprisonment, depending on the severity of the breach and the impact on aviation safety. The exact penalties would be determined based on the specific circumstances of the non-compliance and in accordance with the Civil Aviation Act 1988. It is crucial for all parties involved to understand and adhere to these requirements to avoid these serious repercussions.