Airworthiness Directive 2023-04-19

one-time
Official AD 2023-04-19 · FR doc 2023-04869 · 2023-03-10 · turbine engine

Airworthiness Directives; General Electric Company Turbofan Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain General Electric Company (GE) GE90-110B1 and GE90-115B model turbofan engines. This AD was prompted by a manufacturer investigation which discovered that florescent penetrant inspections (FPI) were not performed on the dovetail pressure face of certain high-pressure compressor (HPC) rotor spools at overhaul. This AD requires FPI of the affected HPC rotor stage 7-9 spool and, depending on the results of the inspection, replacement with a part eligible for installation. The FAA is issuing this AD to address the unsafe condition on these products.

Which aircraft AD 2023-04-19 applies to

MakesGeneral Electric Company
ModelsGE90-110B1, GE90-115B, GE90
Part-conditional2032M23G01, 2032M23G02, 2676M00G01, 2676M00G02.

Applies only to engines with an installed HPC rotor stage 7-9 spool bearing P/N 2032M23G01, 2032M23G02, 2676M00G01, or 2676M00G02, and a serial number listed in paragraph 4, Appendix A, Table 1 of GE Service Bulletin 72-0905 R00, dated July 25, 2022.

Whether AD 2023-04-19 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2023-04-19 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.