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-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