Airworthiness Directives 2004
I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety
Authority, acting under subregulation 39.001 (1) of the Civil
Aviation Safety Regulations 1998:
(a) revoke the Airworthiness Directives mentioned in
Schedule 1; and
(b) make, as separate instruments, each Airworthiness
Directive mentioned in Schedule 1 and attached.
David Villiers
Delegate of the Civil Aviation Safety Authority
20 December 2004
Note: Each attached Airworthiness Directive is being re-made in exactly the
same form as appears in the latest published edition of the Directive.
Schedule 1 Revocation and Remaking of
Airworthiness Directives
AlliedSignal (Lycoming) Turbine Engines - LTS 101 Series
AD Name AD Number
Life Limited Components - CANCELLED AD/LTS/1 Amdt 8
Inspection of Torque Applied to Number Ten Bearing Outer Race Nut 4-082- AD/LTS/2
Power Turbine Governor - Functional Check/Replacement AD/LTS/3
Gas Producer Turbine AD/LTS/4 Amdt 1
Oil System Flow Distribution and Contamination - CANCELLED AD/LTS/5 Amdt 1
Oil System Flow Distribution and Contamination - CANCELLED AD/LTS/6 Amdt 1
Power Turbine Rotor AD/LTS/7 Amdt 2
Number 4 Bearing Distress AD/LTS/8
Number 3 and 4 Bearing Monitoring AD/LTS/9 Amdt 2
Number Two Bearing AD/LTS/10
Engine Electronic Overspeed Protection System AD/LTS/11
Cast Material Axial Compressor AD/LTS/12
Improved Power Turbine Retention AD/LTS/13
Power Turbine Rotor AD/LTS/14
Gas Generator Rotor AD/LTS/15
Rigid Tube Fuel Manifold AD/LTS/16
Compressor Impeller AD/LTS/17
Overview
The Airworthiness Directives 2004 is a legislative instrument enacted to address specific issues related to the airworthiness of aircraft and their components. This instrument was issued by David Alan Villiers, acting as the delegate of the Civil Aviation Safety Authority, under the authority granted by subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The primary purpose of this instrument is to revoke certain existing Airworthiness Directives and remake them in a separate instrument. This legislative action ensures that the directives remain current and aligned with the latest safety standards, thereby maintaining the high safety levels expected in the aviation industry. The policy objective underpinning this instrument is to ensure the ongoing safety and reliability of aircraft by regularly updating and reissuing critical airworthiness directives.
Scope and Application
The Airworthiness Directives 2004 applies to individuals, entities, and industries within the aviation sector, specifically targeting the airworthiness of certain AlliedSignal (Lycoming) Turbine Engines—LTS 101 Series. This legislative instrument is issued by the Civil Aviation Safety Authority (CASA), thereby falling under the Commonwealth jurisdiction of Australia. The directives govern the conduct and maintenance requirements for the specified engines, ensuring they meet the necessary safety standards. This legislation revokes and re-makes several directives related to the inspection, maintenance, and replacement of components in the LTS 101 Series engines. The geographic reach of this legislation is national, as it applies uniformly across Australia. The document notes that each directive is being re-made in the same form as the latest published edition, ensuring consistency and clarity in the regulations. Exclusions or exemptions are not explicitly stated in the provided text, and any further application details or restrictions are left to the subordinate instruments issued under this legislation.
Key Provisions
The legislative instrument F2006B07720, issued under the authority of David Alan Villiers as a delegate of the Civil Aviation Safety Authority, primarily addresses the revocation and re-making of various Airworthiness Directives (ADs) related to the AlliedSignal (Lycoming) Turbine Engines - LTS 101 Series. The instrument revokes certain ADs listed in Schedule 1 and re-makes them as separate instruments, ensuring that they align with the latest published editions (Section 1). Each directive is re-made in exactly the same form as found in the most recent publication, maintaining consistency and accuracy in aviation safety standards.
The obligations imposed by this legislative instrument on the parties governed by the ADs are primarily centred around ensuring that all relevant aircraft components meet the specified airworthiness standards. This includes adherence to inspection schedules, functional checks, and replacements as detailed in the individual ADs. For instance, AD/LTS/2 mandates a functional check or replacement of the power turbine governor, while AD/LTS/10 addresses the engine electronic overspeed protection system. These directives require that operators of the affected engines conduct the specified actions within the timelines provided, ensuring ongoing compliance with airworthiness standards.
Failure to comply with the requirements set out in these ADs can lead to serious consequences. The Civil Aviation Safety Regulations 1998, under which this legislative instrument is enacted, outline potential civil and criminal penalties for non-compliance. Operators and owners of the affected aircraft may face fines, and in more severe cases, criminal charges may be brought against individuals responsible for the non-compliance. The maximum penalties for these offences can be significant, reflecting the critical importance of adhering to airworthiness directives to ensure the safety of air travel. The precise penalties are detailed within the Civil Aviation Safety Regulations 1998 and can vary based on the severity and nature of the breach.