Airworthiness Directives 2004 - Revocation and Remaking - Pratt and Whitney Canada Turbine Engines - PT6A Series

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Legislation au F2006B07970 In force Legislative Instrument

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 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

 Pratt and Whitney Canada Turbine Engines - PT6A Series

 AD Name AD Number

 Rotor Components - Service Life - CANCELLED AD/PT6A/1 Amdt 3

 Rotor Components - Service Life - CANCELLED AD/PT6A/2 Amdt 3

 Rotor Components - Service Life - CANCELLED AD/PT6A/3 Amdt 1

 Rotor Components - Service Life - CANCELLED AD/PT6A/4 Amdt 3

 Life Limits - Engine Rotating Parts - CANCELLED AD/PT6A/5 Amdt 2

 Rotor Components - Service Life - CANCELLED AD/PT6A/6 Amdt 4

 Re-Routing Of Governor Air Pressure Line AD/PT6A/7

 Compressor Rear Hub Hardness AD/PT6A/8

 Exhaust Duct Reinforcing Ring - CANCELLED AD/PT6A/9

 Propeller Reversing Teleflex Control Cable Terminals - CANCELLED AD/PT6A/10

 Woodward Primary Propeller Governors and Overspeed Governors - Solenoid  AD/PT6A/11

 Improved Wire Rope Reversing Cable AD/PT6A/12

 Fuel Pump Drive Coupling - Improved Lubrication AD/PT6A/13

 Sungear Coupling Shaft Retaining Rings AD/PT6A/14

 Reversing Linkage Front End Clevis - Incorporation of Inspection Hole AD/PT6A/15

 Improved Strength P.T. Shaft Housing and Reduction Gearbox Condition  AD/PT6A/16

 Improved Power Turbine Blade Containment - CANCELLED AD/PT6A/17

 No. 2 Bearing Oil Pressure Tube AD/PT6A/18

 Fuel Control Bypass Valve Diaphragm AD/PT6A/19

 No. 2 Bearing Cover AD/PT6A/20

 Replacement of Compressor Delivery Heated Air Tube AD/PT6A/21

 Fuel Pump Coupling - CANCELLED AD/PT6A/22

 Replacement of Compressor Delivery Heated Air Tube by a Non-Metallic Hose AD/PT6A/23

 Rotor Components - Service Life - CANCELLED AD/PT6A/24 Amdt 1

 Sundstrand Fuel Pump Drive Wear - CANCELLED AD/PT6A/25

 Power Turbine Containment Ring AD/PT6A/26

 Compressor Bleed Off Valve AD/PT6A/27

 Water Washing AD/PT6A/28

 Compressor Bleed Valve - CANCELLED AD/PT6A/29

 Propeller Governor Assembly AD/PT6A/30

 Fuel Control Unit AD/PT6A/31

 Exhaust Duct Cracking AD/PT6A/32

 Compressor Rear Hub - Life Limit Review AD/PT6A/33

 

Overview

The Airworthiness Directives 2004, enacted by David Alan Villiers as a delegate of the Civil Aviation Safety Authority, was introduced to address the need for updating and revoking certain airworthiness directives concerning Pratt and Whitney Canada Turbine Engines of the PT6A Series. This legislative instrument revokes and re-makes several airworthiness directives to ensure that aviation safety standards are maintained and that any safety concerns are adequately addressed. The directives, which cover a range of issues such as rotor components service life, life limits of engine rotating parts, and various structural improvements, are re-made in their latest published form to ensure compliance with current safety regulations. The policy objective is to enhance the safety of civil aviation by ensuring that all airworthiness directives are current and accurately reflect the necessary safety requirements.

Scope and Application

The Airworthiness Directives 2004, issued by David Alan Villiers, the delegate of the Civil Aviation Safety Authority under the Civil Aviation Safety Regulations 1998, revokes and remakes various airworthiness directives concerning Pratt and Whitney Canada's PT6A series turbine engines. This legislation applies to entities and individuals involved in the maintenance, operation, and oversight of aircraft equipped with these engines, ensuring compliance with updated safety standards and regulatory requirements. The directives cover a range of technical specifications and maintenance procedures, including rotor components, service life, life limits for engine rotating parts, and structural modifications. The geographic reach of this legislation is national, as it pertains to all civil aviation activities within Australia. Subordinate instruments may be used to extend or clarify the application of these directives, ensuring that they are effectively implemented and enforced across the aviation industry.

Key Provisions

The primary operative sections of this legislative instrument, F2006B07970, involve the revocation and remaking of various Airworthiness Directives concerning Pratt and Whitney Canada Turbine Engines, specifically the PT6A Series, as detailed in Schedule 1 (subsection 1(a) and (b)). These directives are meticulously re-made to align with the most current published versions, ensuring that all safety and operational standards are up-to-date and accurately reflected. Each directive is identified by its AD name and number, with specific amendments or cancellations noted. These Airworthiness Directives impose several obligations on the parties and entities governed by them, including aircraft operators and maintenance providers. They must comply with the detailed requirements outlined in each directive, such as maintaining specific service life limits for rotor components, ensuring proper routing and reinforcement of engine parts, and implementing improved safety measures like enhanced lubrication and strengthened components. The directives are designed to maintain the airworthiness of the aircraft by ensuring all components meet stringent safety standards. Failure to comply with these Airworthiness Directives can lead to severe consequences. Under the Civil Aviation Safety Regulations 1998, non-compliance can result in both civil and criminal penalties. Civil penalties may include fines and the potential grounding of aircraft, while criminal penalties can lead to imprisonment for individuals or hefty fines for corporations, depending on the severity of the breach. The specific penalties are outlined in the Civil Aviation Safety Regulations 1998, with maximum penalties varying according to the nature and extent of the non-compliance. The re-making of these directives also ensures that any previous inconsistencies or ambiguities are addressed, thereby reducing the risk of misinterpretation and ensuring uniform application across the industry. This legislative action is a critical step in maintaining the safety and reliability of aircraft operations in Australia, underscoring the importance of adhering to the updated standards set forth in the Airworthiness Directives.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.