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G-003-07-86 : Engine – LP turbine – Stage 2 nozzle vane – Inner seal with extended lock ring and seal Housing with thickened section – Mod. 72-8301.

Number G-003-07-86
Issued by United Kingdom  United Kingdom
Issue date 1986-07-03
Effective date 1996-07-05
EASA approval number
ATA Chapter
Approval Holder
/ Type Designation
  • ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
    • RB211-22B
      • RB211-22B-02
    • RB211-524
      • B-02
      • B2-19
      • B3-02
      • C2-19
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Rolls-Royce SB RB.211-72-8301 dated 05 July 1996. Applicable to RB211-22B engines installed on Lockheed L-1011 aircraft, and RB211-524 engine sinstalled on Boeing 747 aircraft. Compliance required as detailed in Service Bulletin.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu