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US-2012-26-02 : Fuselage - Skin Crown Area Fatigue Cracking - Inspection / Repair

Number US-2012-26-02
Issued by United States of America  United States of America
Issue date 2013-01-31
Effective date 2013-02-06
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • BOEING
    • 737
      • 737-300
      • 737-400
      • 737-500
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2005-13-27, dated June 27, 2005.
Publication(s) and related information Boeing Special Attention SB 737-53-1234, Revision 1, dated March 31, 2005, or Alert SB 737-53A1234, Revision 2, dated November 24, 2010. For 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; Internet https://www.myboeingfleet.com.
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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