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US-2008-02-19 : High Pressure Turbine Rotor assemblies - Identification / Removal from Service

Number US-2008-02-19
Issued by United States of America  United States of America
Issue date 2008-02-05
Effective date 2008-03-06
EASA approval number
Contributor Federal Aviation Administration (FAA)
ATA Chapter 72
Approval Holder
/ Type Designation
  • HONEYWELL INTERNATIONAL INC.
    • TFE731
      • TFE731-2C
      • TFE731-3B
      • TFE731-3BR
      • TFE731-3C
      • TFE731-3CR
      • TFE731-3D
      • TFE731-3DR
      • TFE731-3R
      • TFE731-4R
      • TFE731-5AR
      • TFE731-5B
      • TFE731-5BR
      • TFE731-5R
    • TFE731-20/-40/-50/-60
      • TFE731-20AR
      • TFE731-20BR
      • TFE731-20R
      • TFE731-40
      • TFE731-40AR
      • TFE731-40R
      • TFE731-60
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Honeywell Service Bulletin (SB) No. TFE731-72-3720, dated July 5, 2006, or Alert SB No. TFE731-A72-5185, dated July 5, 2006, as applicable. Contact Honeywell Technical Publications and Distribution, M/S 2101-201, P.O. Box 52170, Phoenix, AZ 85072-2170; telephone: (602) 365-2493 (General Aviation), (602) 365-5535 (Commercial Aviation), fax: (602) 365-5577 (General Aviation and Commercial Aviation) for a copy of this service information. For technical support regarding the curvic root dimensional inspection criteria, contact the Technical Operations Center: telephone: (800) 601-3099 (U.S.) or (602) 365-3099 (International) and press option 9; e-mail: AeroTechSupport[at]Honeywell.com; or fax: (602) 365-3343.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu

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