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Final rule 2025-00207

Airworthiness Directives; CFM International, S.A. Engines

The FAA is adopting a new airworthiness directive (AD) for certain CFM International, S.A. (CFM) Model LEAP-1B engines. This AD was prompted by a report of a quality escape involving certain high- pressure compressor (HPC) stage 2 seals manufactured without detailed finish machining, which could result in deeper rubs and mechanical damage to the seal teeth of the stage 3-4 compressor rotor blisk (stage 3-4 blisk) of the mating compressor rotor during initial operation. This AD requires a visual inspection of the HPC stage 2 seal, a visual inspection of the forward arm seal teeth of the stage 3-4 blisk, an eddy current inspection (ECI) of the forward arm seal teeth of the stage 3-4 blisk, and replacement of the HPC stage 2 seal and the stage 3-4 blisk, if necessary. 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
2025-00207
Published
Jan 8, 2025
Effective
Feb 12, 2025
Comments close
Not supplied
Federal Register citation
90 FR 1365

Docket identifiers

  • Docket No. FAA-2024-1898
  • Project Identifier AD-2023-01013-E
  • Amendment 39-22904
  • AD 2024-25-02

CFR references

  • Title 14, part 39