Safety Publications Tool

US-2005-18-07 : Fuselage - Lower Cargo Doorjamb Corners - Inspection / Modification

Number US-2005-18-07
Issued by United States of America  United States of America
Issue date 2005-09-02
Effective date 2005-10-07
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • BOEING
    • DC-8
      • DC-8-11
      • DC-8-12
      • DC-8-21
      • DC-8-31
      • DC-8-32
      • DC-8-33
      • DC-8-41
      • DC-8-42
      • DC-8-43
      • DC-8-51
      • DC-8-52
      • DC-8-53
      • DC-8-55
      • DC-8-61
      • DC-8-61F
      • DC-8-62
      • DC-8-62F
      • DC-8-63
      • DC-8-63F
      • DC-8-71
      • DC-8-71F
      • DC-8-72
      • DC-8-72F
      • DC-8-73
      • DC-8-73F
      • DC-8F-54
      • DC-8F-55
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2004-06-06, dated March 25, 2004.
Publication(s) and related information McDonnell Douglas SB DC8-53-078, Revision 01, dated January 25, 2001. Contact Boeing Commercial Airplanes, Long Beach Division, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Data and Service Management, Dept. C1-L5A (D800-0024), for a copy of this service information.
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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