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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.
Published
Feb 4, 2025
Effective
Mar 11, 2025
Citation
90 FR 8889
Agencies
2
Full text not available in our database.
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Docket No. FAA-2024-2325
Project Identifier AD-2024-00412-E
Amendment 39-22927
AD 2025-01-03
2120-AA64
14 CFR 39