AD/TFE731/24 Amdt 1 - First and Second Stage Low Pressure Turbine Discs

AD/TFE731/24Amdt 1	First and Second Stage LowPressure Turbine Discs	1/2010

Applicability:	TFE731-2 and -3 series engines fitted with first and/or second stage low pressure turbine discs as listed by serial number in Table 1 of Allied Signal Aerospace Service Bulletin (ASB) TFE731-A72-3544.
Requirement:	Remove first and second stage low pressure turbine discs in accordance with Allied Signal Aerospace ASB TFE731-A72-3544.Note: FAA AD 95-07-02 refers.
Compliance:	Unless already accomplished in accordance with the previous issue of this Directive, within 100 hours time-in-service (TIS) after the effective date of this Directive.
	This Amendment becomes effective on 22 January 2010.
Background:	This Directive requires the removal from service of certain first and second stage low pressure turbine discs. The requirement follows advice that certain first and second stage discs may have been subjected to incorrect heat treatment during the manufacturing process.This amendment references the applicable State of design Directive which is also applicable to AD/TFE731/26 Amdt 1. For information, AD/TFE731/34 is also applicable to first and second stage low pressure turbine discs, but unrelated to this Directive.

Mike Higgins
Delegate of the Civil Aviation Safety Authority

4 January 2010

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

AD/TFE731/24Amdt 1	First and Second Stage LowPressure Turbine Discs	1/2010

Applicability:	TFE731-2 and -3 series engines fitted with first and/or second stage low pressure turbine discs as listed by serial number in Table 1 of Allied Signal Aerospace Service Bulletin (ASB) TFE731-A72-3544.
Requirement:	Remove first and second stage low pressure turbine discs in accordance with Allied Signal Aerospace ASB TFE731-A72-3544.Note: FAA AD 95-07-02 refers.
Compliance:	Unless already accomplished in accordance with the previous issue of this Directive, within 100 hours time-in-service (TIS) after the effective date of this Directive.
	This Amendment becomes effective on 22 January 2010.
Background:	This Directive requires the removal from service of certain first and second stage low pressure turbine discs. The requirement follows advice that certain first and second stage discs may have been subjected to incorrect heat treatment during the manufacturing process.This amendment references the applicable State of design Directive which is also applicable to AD/TFE731/26 Amdt 1. For information, AD/TFE731/34 is also applicable to first and second stage low pressure turbine discs, but unrelated to this Directive.

Mike Higgins
Delegate of the Civil Aviation Safety Authority

4 January 2010

Pressure Turbine Discs

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