Safety Publications Tool

G-001-10-2000 : Engine - HP compressor stage 4-6 rotor shaft subjected to grit blast overspray.

Number G-001-10-2000
Issued by United Kingdom  United Kingdom
Issue date 2000-10-01
Effective date 2000-10-01
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
    • RB211-535
      • RB211-535E4-37
      • RB211-535E4-B-37
      • RB211-535E4-C-37
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Applicable to Boeing 757 aircraft fitted with RB211-535E4 series engines. Compliance required as detailed in Rolls-Royce SB RB.211-72-D085.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu