Safety Publications Tool

US-2001-22-04 : Fuselage - Skin adjacent to the Drag Splice Fitting - Inspection

Number US-2001-22-04
Issued by United States of America  United States of America
Issue date 2001-10-29
Effective date 2001-12-03
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • BOEING
    • 747
      • 747-100
      • 747-100B
      • 747-100B SUD
      • 747-200B
      • 747-200C
      • 747-200F
      • 747-300
      • 747-400
      • 747-400D
      • 747-400F
      • 747SP
      • 747SR
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2000-14-04, dated July 13, 2000.
Publication(s) and related information Boeing Alert SB 747-53A2444, dated May 25, 2000, or Revision 1, dated June 15, 2000, or Revision 2, dated May 24, 2001. For a copy of this service information, contact Boeing Commercial Airplane Group, 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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