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  Safety Publications Tool

G-003-01-99 : Engine - IP compressor stage 6-7 rotor shaft assembly - Bolt hole cracking.

Number G-003-01-99
Issued by United Kingdom  United Kingdom
Issue date 1999-01-01
Effective date 1999-01-01
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 SB 72-C538
Remarks Applicable to Lockheed L-1011, Boeing 747 and 767 aircraft fitted with RB 211-22B and -524 engines as detailed in Service Bulletin. Compliance required as detailed in Service Bulletin.