Safety Publications Tool

G-006-02-2002 : Engine - Front bearing support - Introduction of LP compressor shaft extreme axial movement detector system.

Number G-006-02-2002
Issued by United Kingdom  United Kingdom
Issue date 2002-02-15
Effective date 2002-02-15
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
    • RB211-22B
      • RB211-22B-02
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Applicable to Lockheed L-1011 aircraft fitted with RB211-22B Series engines. Compliance required as detailed in SB RB211-72-C863 dated 15 February 2002. 2001. Concurrent requirements: SB RB.211-72-6149 Revision 9, dated November 24, 1999; SB RB.211-77-C144, Revision 1, dated February 13, 2002; and Lockheed Martin SB 093-77-060.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu