You are not logged in
  Safety Publications Tool

US-2011-14-02 : Fuselage - Bulkhead Structure and the Vertical Inner Chord at STA 1809.5 - Inspection / Repair

Number US-2011-14-02
Issued by United States of America  United States of America
Issue date 2011-10-21
Effective date 2011-11-16
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • BOEING
    • 767
      • 767-200
      • 767-300
      • 767-300F
      • 767-400ER
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2006-24-04 dated November 27, 2006.
Publication(s) and related information (1) Boeing Alert Service Bulletin 767-53A0131, Revision 1, dated March 12, 2009. (2) Subject 53-00-03, Fuselage Stringers, of Chapter 53, Fuselage; or Subject 53-80-08, Fuselage Bulkheads–Section 48, Repair 9–Station 1809.5 Bulkhead–Forward Outer Chord Repair Between S-4 to S-8, Repair 10–Station 1809.5 Bulkhead–Horizontal Inner Chord Repair at Approximately WL 257 and BL 28, or Repair 11–Station 1809.5 Bulkhead–Vertical Inner Chord Repair at Approximately WL 256 and BL 30, as applicable, of Chapter 53, Fuselage; as applicable; of the applicable Structural Repair Manual (SRM) specified in paragraphs (o)(2)(i) through (o)(2)(v) of this AD.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu

Download attachments: