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US-2020-20-11 : Engine - High-Pressure Turbine Rotor Stage 2 Disks and Stage 6-10 Compressor Rotor Spools - Removal

Number US-2020-20-11
Issued by United States of America  United States of America
Issue date 2020-10-01
Effective date 2020-11-03
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • GENERAL ELECTRIC
    • GEnx
      • GEnx-1B64/P2
      • GEnx-1B67/P2
      • GEnx-1B70/75/P2
      • GEnx-1B70/P2
      • GEnx-1B70C/P2
      • GEnx-1B74/75/P2
      • GEnx-1B76/P2
      • GEnx-1B76A/P2
      • GEnx-2B67/P
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information GEnx-1B Service Bulletin (SB) 72-0473 R00; GE GEnx-1B SB 72-0474 R00; and GE GEnx-2B SB 72-0416 R00, all dated April 14, 2020. For service information identified in this final rule, contact General Electric Company, 1 Neumann Way, Cincinnati, OH 45215; phone: (513) 552-3272; email: aviation.fleetsupport[at]ae.ge.com; website: www.ge.com.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu

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