Airworthiness Directives 2004 - Revocation and Remaking - AlliedSignal (Garrett/AiResearch) Turbine Engines - TFE731 Series

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Legislation au F2006B07717 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

 AlliedSignal (Garrett/AiResearch) Turbine Engines - TFE 731 Series

 AD Name AD Number

 Life Limited Components - CANCELLED AD/TFE 731/1 Amdt 5

 Fuel Pump Anti-Icing Valve - Inspection AD/TFE 731/2

 H.P. Turbine Blade P/N 3072111-1 - Replacement AD/TFE 731/3 Amdt 1

 Transfer Bearing Support - Inspection AD/TFE 731/4

 Compressor Tie Rod - Replacement AD/TFE 731/5

 High Pressure Rotor and Nozzle Assembly Bolt - Replacement AD/TFE 731/6

 Turbine Interstage Transition Duct AD/TFE 731/7 Amdt 2

 Second Stage Turbine Disc Inspection AD/TFE 731/8

 L.P. Turbine Blade - Review, Inspection and Replacement AD/TFE 731/9

 No. 1 Bearing - Replacement AD/TFE 731/10

 H.P. Turbine Blades P/N 3072455-10 Replacement AD/TFE 731/11

 Fan Rotor Assembly - CANCELLED AD/TFE 731/12 Amdt 5

 Turbine Interstage Transition Duct Re-Inspection AD/TFE 731/13

 First Stage L.P. Turbine Disc AD/TFE 731/14

 HP Turbine Rotor Disc AD/TFE 731/15

 HP Turbine Rotor Disc P/N 3072316-2/-3 and P/N 3073110-1/-2 AD/TFE 731/16

 L.P. Turbine Third Stage Rotor Disc AD/TFE 731/17

 Digital Electronic Engine Control AD/TFE 731/18

 Fan Rotor Disc Inspection - CANCELLED AD/TFE 731/19 Amdt 2

 First Stage Low Pressure Turbine Nozzle Airseal - CANCELLED AD/TFE 731/20

 Fan Disc Dovetail Slot - CANCELLED AD/TFE 731/21 Amdt 1

 Low Pressure Turbine Third Stage Disc Material Anomalies AD/TFE 731/22

 Fuel Line Clamp - CANCELLED AD/TFE 731/23

 First and Second Stage Low Pressure Turbine Discs AD/TFE 731/24

 Low Pressure Turbine Nozzle A5 Airseal AD/TFE 731/25

 Low Pressure Turbine First and Second Stage Disc Suspect Material Properties AD/TFE 731/26

 P/N 3072816 Fan Disc Life Reduction - CANCELLED AD/TFE 731/27

 P/N 3072816 Fan Disc Inspection - CANCELLED AD/TFE 731/28

 Fan Disc Life Reduction - CANCELLED AD/TFE 731/29

 Re-Inspect Fan Disc - CANCELLED AD/TFE 731/30

 HP Compressor Impeller AD/TFE 731/31

 Fan Rotor Disc AD/TFE 731/32

 

Overview

The Airworthiness Directives 2004, enacted under the Civil Aviation Safety Regulations 1998, represent a legislative instrument aimed at enhancing the airworthiness standards for aircraft engines, specifically the AlliedSignal (Garrett/AiResearch) Turbine Engines - TFE 731 Series. This instrument, issued by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, revokes and remakes a series of Airworthiness Directives to ensure that aircraft maintenance and operational practices meet the highest safety standards. The primary objective of this legislative action is to address identified safety concerns and maintain the integrity of the aircraft's operational capability through the implementation of specific maintenance, inspection, and replacement requirements.

Scope and Application

The Airworthiness Directives 2004, issued under the Civil Aviation Safety Regulations 1998, apply to the specified AlliedSignal (Garrett/AiResearch) Turbine Engines of the TFE 731 series. The legislation is concerned with ensuring the continued airworthiness of these engines by setting forth mandatory safety standards and procedures for inspection, maintenance, and repair. These directives are applicable to all aircraft operators, maintenance organisations, and other entities that fall under the jurisdiction of the Civil Aviation Safety Authority (CASA). The legislation has a national reach, applying across Australia in accordance with the Civil Aviation Act 1988. Certain components and systems of the TFE 731 engines, as listed in Schedule 1, have been either cancelled or amended, reflecting updated safety requirements or the resolution of previous safety issues. The specific details of these amendments and cancellations are provided in the attached Airworthiness Directives, which are re-made to match the latest published editions.

Key Provisions

The primary operative sections of the Airworthiness Directives 2004 (F2006B07717) involve the revocation and remaking of various Airworthiness Directives (ADs) as listed in Schedule 1. Specifically, section (a) revokes the ADs mentioned in Schedule 1, while section (b) re-makes each of these ADs as separate instruments. These ADs pertain to the AlliedSignal (Garrett/AiResearch) Turbine Engines - TFE 731 Series, covering a range of components including fuel pumps, turbine blades, bearing supports, and more. Each AD is re-made in the exact form as it appears in the latest published edition, ensuring consistency and accuracy in safety requirements. The obligations and requirements imposed by this legislative instrument are primarily focused on ensuring the airworthiness of turbine engines, specifically those in the AlliedSignal (Garrett/AiResearch) TFE 731 Series. Each AD mandates specific inspections, replacements, and reviews of various engine components to maintain their airworthiness. For instance, AD/TFE 731/2 requires the replacement of H.P. Turbine Blade P/N 3072111-1, while AD/TFE 731/7 mandates the inspection of the Second Stage Turbine Disc. These obligations ensure that aircraft using these engines meet stringent safety standards, thereby protecting the integrity of air travel. There are no explicit offences, penalties, or civil/criminal consequences outlined in the text of the Airworthiness Directives 2004. However, it is important to note that non-compliance with ADs can have significant ramifications. Failure to adhere to the requirements of these directives could lead to the grounding of affected aircraft, which can result in substantial financial losses for airlines and potential safety risks. Furthermore, regulatory bodies like the Civil Aviation Safety Authority (CASA) may take enforcement actions against entities that do not comply with airworthiness directives, which could include fines, legal action, or other penalties. The specific penalties would depend on the nature and severity of the non-compliance, as well as the regulatory framework governing aviation safety in Australia.

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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.