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US-2003-14-21 : NOT ADOPTED BY EASA - DECISION ATTACHED

Number US-2003-14-21
Issued by United States of America  United States of America
Issue date 2003-07-21
Effective date 2003-08-25
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • LOCKHEED MARTIN CORPORATION
    • L-1011 (Tristar)
  • ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
    • RB211-22B
    • RB211-524
      • B-02
      • B-B-02
      • B3-02
      • B4-02
      • B4-D-02
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2000-17-10 R1, dated August 22, 2001.
Publication(s) and related information RR Mandatory SB RB.211-72-C963, dated December 4, 2001, or RR Mandatory SB RB.211-72-C863, dated February 15, 2002; and RR Mandatory SB RB.211-71-E047, dated August 2, 2002. Concurrent requirements: RR SB RB.211-72-6149, Revision 9, dated November 24, 1999, RR SB RB.211-72-C178, Revision 1, dated March 9, 2001, RR SB RB.211-77-C144, Revision 1, dated February 13, 2002, Lockheed Martin SB 093-77-059, Revision 2, dated April 11, 2002, and Lockheed Martin SB 093-77-060, dated April 11, 2002.
Remarks For engines installed on affected aeroplanes registered in an EASA Member State, the applicable State of design ADs are CAA UK AD 006-12-2001, 006-02-2002 and 003-08-2002. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu