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Final rule 2026-21590

Airworthiness Directives; General Electric Company Engines

The FAA is adopting a new airworthiness directive (AD) for certain General Electric Company (GE) Model CF34-8C1, CF34-8C5, CF34- 8C5A1, CF34-8C5A2, CF34-8C5B1, CF34-8E2, CF34-8E2A1, CF34-8E5, CF34- 8E5A1, CF34-8E5A2, CF34-8E5A2HA, CF34-8E6, and CF34-8E6A1 engines. This AD was prompted by reports of in-flight "Engine Degraded" messages from the engine indicating and crew alerting system (EICAS) due to corrosion of the variable geometry (VG) system actuator. This AD requires removing certain electronic engine control (EEC) full authority digital electronic control (FADEC) software versions from service and installing an updated EEC FADEC software that is eligible for installation. The FAA is issuing this AD to address the unsafe condition on these products.

Source: FederalRegister.gov API v1Recently refreshed. Last successful refresh: 2026-10-22 08:49:02 UTC.

Source-supplied record

Document details

Document number
2026-21590
Published
Oct 22, 2026
Effective
Nov 27, 2026
Comments close
Not supplied
Federal Register citation
91 FR 66631

Docket identifiers

  • Docket No. FAA-2025-3998
  • Project Identifier AD-2025-00432-E
  • Amendment 39-23500
  • AD 2026-21-11

CFR references

  • Title 14, part 39