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Final rule 2025-02204

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-1A and LEAP-1C engines. This AD was prompted by an investigation of an in-flight shut down event that revealed the aft arm of the high-pressure turbine (HPT) rotor interstage seal had failed. This AD requires removal from service and replacement of the HPT rotor interstage seal for LEAP-1A engines. Since the HPT rotor interstage seal part number is interchangeable between LEAP-1A and LEAP-1C engines, this AD also prohibits installation of these affected parts onto any LEAP-1A or LEAP-1C engine. 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
2025-02204
Published
Feb 4, 2025
Effective
Mar 11, 2025
Comments close
Not supplied
Federal Register citation
90 FR 8889

Docket identifiers

  • Docket No. FAA-2024-2325
  • Project Identifier AD-2024-00412-E
  • Amendment 39-22927
  • AD 2025-01-03

CFR references

  • Title 14, part 39