Safety Publications Tool

US-2011-18-03 : Automatic Shutoff System for the Center Tank Fuel Boost Pumps - Installation

Number US-2011-18-03
Issued by United States of America  United States of America
Issue date 2011-09-16
Effective date 2011-09-30
EASA approval number
ATA Chapter 28
Approval Holder
/ Type Designation
  • BOEING
    • 737
      • 737-600
      • 737-700
      • 737-700C
      • 737-800
      • 737-900
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Boeing ASB 737-28A1206 Revision 2, dated 21 May 2009 and ASB 737-28A1248 Revision 2, dated 28 August 2009. Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), of the Boeing 737-600/700/800/900 Maintenance Planning Data Document, D626A001-CMR, Revision March 2011, issue date March 2011 - AWL No. 28-AWL-23 of Subsection E, AWLs – Fuel Systems of Section 9. For Boeing service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206-544-5000, extension 1; fax 206-766-5680; e-mail me.boecom@boeing.com; Internet https://www.myboeingfleet.com.
Remarks Optional Terminating Action - Paragraph (s) of the FAA AD 2011-18-03 allows the installation of TDG Aerospace Inc Universal Fault Interrupter (UFI) in accordance with FAA STC ST02076LA as a terminating action. For European registered aircraft the reference STC is EASA.IM.A.S.02796 and is accepted as the same optional terminating action. General Note: EASA through the acceptance of the FAA AD grants no approval for the referenced FAA STC: European installations must comply with the EASA validation requirements as specified in the EASA STC: EASA.IM.A.S.02796.

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