You are not logged in
  Safety Publications Tool

US-2010-10-05 : Fuselage Skin Lap Joints - Inspection / Repair / Modification

Number US-2010-10-05
Issued by United States of America  United States of America
Issue date 2010-05-20
Effective date 2010-06-21
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • BOEING
    • 747
      • 747-100
      • 747-100B
      • 747-100B SUD
      • 747-200B
      • 747-300
      • 747SP
      • 747SR
Revision Not applicable
Correction Not applicable
Supersedure This FAA AD supersedes FAA AD 94-12-04.
Publication(s) and related information See FAA AD Tables: Table 1 – All material incorporated by reference; Table 2 – New material incorporated by reference and Table 3 – Material previously incorporated by reference. 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; e-mail me.boecom@boeing.com; 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

Download attachments: