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US-2012-19-03 : Fuselage - Strap Repositioning - Installation / Replacement

Number US-2012-19-03
Issued by United States of America  United States of America
Issue date 2012-10-02
Effective date 2012-11-05
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • BOEING
    • DC-10
      • DC-10-10
      • DC-10-10F
      • DC-10-15
      • DC-10-30
      • DC-10-30F
      • DC-10-40
      • DC-10-40F
    • MD-10
      • MD-10-10F
      • MD-10-30F
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2009-26-17 dated December 31, 2009.
Publication(s) and related information Boeing SB DC10-53-109, Revision 8, dated March 10, 2011; SB DC10-53-111, Revision 7, dated March 16, 2011; SB DC10-53-109, Revision 7, dated March 3, 2009; SB DC10-53-111, Revision 6, dated March 3, 2009; McDonnell Douglas DC-10 SB 53-109, Revision 4, dated October 7, 1992; and DC-10 SB 53-111, Revision 3, dated August 24, 1992. For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, 3855 Lakewood Boulevard, MC D800-0019, Long Beach, California 90846-0001; telephone 206-544-5000, extension 2; fax 206-766-5683; Internet https://www.myboeingfleet.
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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