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US-2007-25-20 : Thrust Reverser Wiring and Locking System - Modification / Installation

Number US-2007-25-20
Issued by United States of America  United States of America
Issue date 2008-01-04
Effective date 2008-01-22
EASA approval number
ATA Chapter 78
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-11
      • MD-11
      • MD-11F
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information McDonnell Douglas Alert Service Bulletin (SB) DC10-78A057, Revision 01, dated February 18, 1999, McDonnell Douglas SB DC10-78-060, dated December 17, 1999; or McDonnell Douglas SB DC10-78-060, Revision 01, dated June 30, 2003, McDonnell Douglas SB DC10-78-064, dated June 24, 2003, McDonnell Douglas SB MD11-31-091, dated November 5, 1998, Boeing SB DC10-78-066, Revision 01, dated November 30, 2001, Boeing SB DC10-78-067, dated October 30, 2002, and Boeing Alert SB MD11-78A007, Revision 4, dated February 22, 2007. Rohr SB MD-11 54-200, Revision 1, dated May 14, 2001 and Rohr SB MD-11 54-201, Revision 2, dated December 12, 2005. 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 Boeing and McDonnell Douglas 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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