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US-2003-16-16 : Thrust Reverser Central Drive Unit Cone Brake - Testing / Thrust Reverser Actuation System (TRAS) Lock - Installation / TRAS Lock - Functional Test

Number US-2003-16-16
Issued by United States of America  United States of America
Issue date 2003-08-27
Effective date 2003-10-01
EASA approval number
ATA Chapter 78
Approval Holder
/ Type Designation
  • BOEING
    • 747
      • 747-400
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2000-09-03, dated May 4, 2000.
Publication(s) and related information Boeing SB 747-31-2242 dated April 18, 1996; SB 747-45-2016 Revision 1 dated May 2, 1996; SB 747-78-2132 Revision 2 dated December 11, 1997; SB 747-78-2151, Revision 2, dated January 13, 2000; SB 747-78A2113 Revision 3 dated September 11, 1997; Alert SB 747-78A2166 Revision 2 dated March 15, 2001. Middle River Aircraft Systems (formerly Lockheed Martin) SB 78-1007 Revision 2 dated March 10, 1998; SB 78-1020 Revision 4 dated October 10, 2002. Copies may be obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124-2207; and Distribution, Lockheed Martin Technical Services, 1330 Kemper Meadow Drive, suite 110-C, Cincinnati, Ohio 45240.
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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