AD 2024-07-06

Recurring final rule
Data completeness: 70%

Airworthiness Directives; CFM International, S.A. Engines

AD Number
2024-07-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2023-1991
FR Citation
89 FR 33211

Applicability

TypeManufacturerModelDetails
engine CFM International Airworthiness Directives; CFM International, S.A. Engines

Unsafe Condition

Wear on the No. 3 bearing spring finger housing can lead to high levels of non-synchronous vibration (NSV), which could induce high-pressure compressor (HPC) stall.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Initial and repetitive calculations of the levels of NSV, inspection of the stage 2 high-pressure turbine (HPT) nozzle assembly honeycomb and HPT stator stationary seal honeycomb, and, depending on the results of the calculations and inspections, replacement of certain parts. Replacement of certain No. 3 bearing spring finger housings at a certain time.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

CFM Model LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A engines.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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