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Airworthiness Directives (ADs)

CAA-2024-01-009

The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.

Issue Date
2024/01/26
Applicability
This AD applies to General Electric Company (GE) Model GE90–90B and GE90–94B engines with interstage HPT seals listed in Table 1 to Paragraph (c) of this AD and GE90–110B1 and GE90–115B engines with an installed high-pressure turbine (HPT) stage 1 disk, HPT stage 2 disk, forward HPT rotor seal, or stages 7–9 compressor rotor spool part number (P/N) and serial number (S/N) identified in Table 1 to Paragraph (c) of this AD, or identified in Paragraph 4. APPENDIX—A, Tables 1, 2, or 3, of GE GE90–100 Service Bulletin 72–0914, dated January 25, 2023 (GE90–100 SB 72–0914).
Model Number
GE90–90B, GE90–94B, GE90–110B1, and GE90–115B engines.
CAA AD Number
CAA-2024-01-009
Aeronautics Authority of Original AD
FAA
Original AD Number
2023-26-07
Effective Date
2024/02/27
Subject
This AD requires replacement of affected HPT stage 1 disks, HPT stage 2 disks, forward HPT rotor seals, interstage HPT seals, and stages 7–9 compressor rotor spools.
Reference Publications (Revision/ATA/SB)
General Electric GE90–100 Service Bulletin 72–0914, dated January 25, 2023.
Remarks
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CAA-2024-01-009.pdf
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