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US-2004-16-12 : Wing Front Spar / Engine Strut Outboard Pitch Load Fitting - Rework / Replacement / Modification

Number US-2004-16-12
Issued by United States of America  United States of America
Issue date 2004-08-17
Effective date 2004-09-21
EASA approval number
ATA Chapter 54
Approval Holder
/ Type Designation
  • BOEING
    • 767
      • 767-200
      • 767-300
      • 767-300F
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2001-02-07, dated January 29, 2001; FAA AD 2001-06-12, dated April 2, 2001; and FAA AD 2001-08-23, dated April 27, 2001.
Publication(s) and related information Boeing SB 767-29-0057, dated December 16, 1993, or Revision 1, dated August 14, 2003; SB 767-54-0069 Revision 1, dated January 29, 1998, or Revision 2, dated August 31, 2000; SB 767-54-0080, dated October 7, 1999, or Revision 1, dated May 9, 2002; SB 767-54-0081 dated July 29, 1999, or Revision 1 dated February 7, 2002; SB 767-54-0083, dated September 17, 1998; SB 767-54-0088 Revision 1, dated July 29, 1999; SB 767-54A0094 Revision 1, dated September 16, 1999, or Revision 2, dated February 7, 2002; SB 767-57-0053, Revision 2, dated September 23, 1999; and SB 767-57A0070 Revision 1 November 16, 2000, or Revision 2 dated August 2, 2001, or Revision 3 dated November 8, 2001, as applicable. Copies may be obtained from Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207.
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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