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Final rule 2025-09205

Airworthiness Directives; General Electric Company Engines

The FAA is adopting a new airworthiness directive (AD) for all General Electric Company (GE) Model CF34-10E2A1, CF34-10E5, CF34- 10E5A1, CF34-10E6, CF34-10E6A1, CF34-10E7, and CF34-10E7-B engines with certain part-numbered high-pressure turbine (HPT) shroud/low pressure turbine (LPT) nozzle assemblies installed. This AD was prompted by a report of failed retention features of the inner and outer support air ducts (commonly referred to as spoolies) discovered during engine disassembly. This AD requires a visual inspection of the combustion case for wear and gouges, repair if necessary, and rework of the affected HPT shroud/LPT nozzle assemblies to add a positive retention of the support air duct. The FAA is issuing this AD to address the unsafe condition on these products.

Source: FederalRegister.gov API v1Recently refreshed. Last successful refresh: 2026-07-31 22:49:02 UTC.

Source-supplied record

Document details

Document number
2025-09205
Published
May 22, 2025
Effective
Jun 26, 2025
Comments close
Not supplied
Federal Register citation
90 FR 21855

Docket identifiers

  • Docket No. FAA-2024-1883
  • Project Identifier AD-2023-01120-E
  • Amendment 39-23038
  • AD 2025-10-04

CFR references

  • Title 14, part 39