COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
AlliedSignal (Lycoming) Turbine Engines - T53 Series
AD/T53/4 Engine Oil Pump Drive Gear Spline - Inspection 1/86
Applicability: All model T5311A engines S/N LE08149 to LE08293 not incorporating Overhaul Modification Bulletin No. 0028: Field Service Bulletin No. 0010, or Lycoming SB No. 41.
Document: 1. Lycoming SB No. 40; or
2. Lycoming Field Service Bulletin No. 0013; or
3. Lycoming Overhaul Modification bulletin No. 0027; or
4. AD/LYC-T/2.
Compliance: In accordance with the requirement documents.
Overview
The Civil Aviation Regulations 1998, which were enacted by the Australian Parliament, are fundamental to the regulation of civil aviation within Australia. These regulations provide a comprehensive framework for ensuring the safety and efficiency of civil aviation operations. A specific legislative instrument, F2006B07252, addresses the problem of ensuring the airworthiness of aircraft engines, particularly focusing on the AlliedSignal (Lycoming) Turbine Engines - T53 Series. This directive was introduced to address potential safety issues related to the engine oil pump drive gear spline, requiring specific inspections to prevent mechanical failures. The policy objective of this legislation is to maintain the highest safety standards in civil aviation by ensuring that all aircraft components meet the required airworthiness criteria.
The enactment of F2006B07252 under the Civil Aviation Regulations 1998 underscores the commitment to safety and compliance in the aviation sector. By specifying the applicability and compliance requirements for certain T53 Series engines, the regulation aims to mitigate risks associated with engine malfunctions. This legislative instrument mandates that inspections be carried out in accordance with specified documents, such as Lycoming Service Bulletins and Overhaul Modification Bulletins, to ensure the engines' operational integrity. The overarching goal is to protect public safety and uphold the stringent safety standards that are integral to Australia's civil aviation regulatory framework.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39 - 106, specifically mandate the Airworthiness Directives concerning AlliedSignal (Lycoming) Turbine Engines - T53 Series, focusing on the engine oil pump drive gear spline inspection. This legislation applies to all model T5311A engines with serial numbers ranging from LE08149 to LE08293 that do not incorporate the Overhaul Modification Bulletin No. 0028: Field Service Bulletin No. 0010, or Lycoming Service Bulletin No. 41. The directive ensures that these engines meet specific safety standards, which are referenced in the Lycoming SB No. 40, Lycoming Field Service Bulletin No. 0013, Lycoming Overhaul Modification bulletin No. 0027, or AD/LYC-T/2. Compliance with these requirements is mandatory and must be achieved in accordance with the stipulations outlined in the referenced documents. This regulation applies nationwide within the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority, ensuring uniform safety standards across the country.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 106, detail the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives. Under this section, AD/T53/4 mandates the inspection of the engine oil pump drive gear spline for AlliedSignal (Lycoming) Turbine Engines of the T53 Series (1). This directive applies to all model T5311A engines with serial numbers ranging from LE08149 to LE08293 that do not incorporate Overhaul Modification Bulletin No. 0028, Field Service Bulletin No. 0010, or Lycoming Service Bulletin No. 41. The compliance requirement necessitates that inspections be conducted in accordance with specific Lycoming documents, including Lycoming Service Bulletin No. 40, Lycoming Field Service Bulletin No. 0013, Lycoming Overhaul Modification Bulletin No. 0027, or AD/LYC-T/2.
The obligations imposed by AD/T53/4 on the parties governed by this directive are primarily centred around ensuring the airworthiness of the specified engines. Operators and maintenance providers must ensure that the engines in question are inspected according to the detailed guidelines provided in the referenced Lycoming documents. This involves a thorough examination of the engine oil pump drive gear spline to identify any potential defects or issues that could compromise the engine's safety and performance. It is essential that these inspections are performed by qualified personnel who are familiar with the specific requirements and procedures outlined in the Lycoming bulletins and directives.
Failure to comply with AD/T53/4 can lead to serious consequences. Non-compliance with airworthiness directives is not only a breach of the Civil Aviation Regulations 1998 but also poses significant risks to aviation safety. Civil penalties for non-compliance may include substantial fines, and in severe cases, criminal charges may be brought against individuals or companies responsible for the oversight. Additionally, the operation of non-compliant aircraft could result in grounding, leading to operational disruptions and financial losses. The exact penalties are not detailed in the directive but typically align with the severity of the non-compliance and its potential impact on safety.