AD/PW4000/4 - Low Pressure Turbine Stage 4 Disk

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Legislation au F2006B06395 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Pratt and Whitney Turbine Engines - PW4000 Series

 

AD/PW4000/4 Low Pressure Turbine Stage 4 Disk 10/99

Applicability: PW4000 series engines with a Low Pressure Turbine (LPT) Stage 4 disk as specified in FAA AD 99-15-01.

 

Requirement: Replace affected LPT Stage 4 Disks in accordance with the technical requirements of FAA AD 99-15-01.

 

Note: Pratt and Whitney Service Bulletins PW4ENG 72-657 and PW4G 100-72-105 also refer.

 

Compliance: At periods detailed in the Requirement document.

 

This Airworthiness Directive becomes effective on 7 October 1999.

 

Background: This Directive is prompted by advice that a change in cooling hole geometry on affected LPT disks results in a reduction in cooling air flow to the disk and higher stresses. Higher than normal stress could result in an uncontained disk failure.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.