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G-0037-PRE80 : Engine - HP compressor rotor - Inspection of HP compressor stage 4 to 6 rotor shaft for electron beam weld impingement on the front face of the stage 5 disc.

Number G-0037-PRE80
Issued by United Kingdom  United Kingdom
Issue date 1980-01-01
Effective date 1980-01-01
EASA approval number
ATA Chapter
Approval Holder
/ Type Designation
  • ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
    • RB211-524
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information 72-5201
Remarks Applicable to: Lockheed L1011 RB211-524-02 and -524B-02 engines fitted with HP compressor stage 4 to 6 rotor shafts with Serial Nos. prior to 13923. Boeing 747 RB211-524B-19, -524B2-19, -524C-19 and -524B2-39 engines fitted with HP compressor stage 4 to 6 rotor shafts with Serial Nos. prior to 13923. Compliance as detailed in Service Bullettin.