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G-2003-0009 : [Correction] Engine – Group A (Critical) Parts – Focused Inspections

Number G-2003-0009
Issued by United Kingdom  United Kingdom
Issue date 2003-11-25
Effective date 2003-09-26
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
    • RB211-524
      • B-02
      • B-19
      • B-B-02
      • B2-19
      • B2-39
      • B2-B-19
      • B3-02
      • B4-02
      • B4-D-02
      • C2-19
      • C2-B-19
      • D4-19
      • D4-39
      • D4-B-19
      • D4-B-39
      • D4X-19
      • D4X-B-19
      • G2-19
      • G2-T-19
      • G3-19
      • G3-T-19
      • H-36
      • H-T-36
      • H2-19
      • H2-T-19
Revision Not applicable
Correction This AD was republished to clarify that compliance action should only be carried out at an appropriate level of engine workshop visit, and to ensure common text with the Time Limits Manual reference.
Supersedure None
Publication(s) and related information Rolls-Royce RB211-524 series Time Limits Manual Reference 05-20-01, dated 1 July 2002 or later CAA approved revision. Copies may be obtained from Rolls-Royce plc, Technical Publications, PO Box 31, Derby, DE24 8BJ, United Kingdom. Phone: +44 (0) 1332 242424, Fax: +44 (0) 1332 249936.
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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