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US-2009-20-11 : [Correction] Fuel System Limitations and Inspections associated with Goodrich Corporation STC ST00127BO

Number US-2009-20-11
Issued by United States of America  United States of America
Issue date 2010-01-06
Effective date 2009-11-05
EASA approval number
ATA Chapter 28
Approval Holder
/ Type Designation
  • BOEING
    • 737
      • 737-300
      • 737-400
      • 737-500
  • GOODRICH CORPORATION
    • STC ST00127BO
Revision Not applicable
Correction The FAA is correcting information in an existing airworthiness directive (AD) that was published in the Federal Register on October 1, 2009. The error resulted in use of an outdated division name and e-mail address in the vendor contact information.
Supersedure None
Publication(s) and related information Goodrich AMM Supplement with Wiring Diagrams, 737-300/-400/-500 FQIS with Goodrich Digital Indicators and Transient Suppression Device, STC ST00127BO, Revision 5 dated December 20, 2006. Goodrich ICA Document T2007-0010-0101, Revision D dated January 16, 2007.For service information identified in this AD, contact Goodrich Corporation, Sensors and Integrated Systems (Formerly Fuel and Utility Systems), 100 Panton Road, Vergennes, Vermont 05491-1008; telephone 802-877-4476; e-mail SIS.TechPubs-VT@Goodrich.com; Internet http://www.goodrich.com/TechPubs.
Remarks STC ST00127BO was validated in Europe through CAA UK AAN 28225 dated 4 July 2002. 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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