Safety Publications Tool

G-016-03-81 : Engine - HP compressor - Withdrawal of specific HP compressor rotor stage 1 and 2 disc assemblies from service.

Number G-016-03-81
Issued by United Kingdom  United Kingdom
Issue date 1981-03-01
Effective date 1981-03-01
EASA approval number
ATA Chapter
Approval Holder
/ Type Designation
  • ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
    • RB211-22B
    • RB211-524
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information 72-A5885
Remarks Applicable to Lockheed L1011 aircraft fitted with RB211-22B-02, -524-02, -524B-02, -524B3-02 and -524B4-02 engine variants and Boeing 747 aircraft fitted with RB211-524B2-19, -524C-19 and -524B2-39 engine variants. Compliance required as detailed in Service Bullettin.