AD Amdt-39-9361
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric | Company CF6 Series | Airworthiness Directives; General Electric Company CF6 Series Turbofan Engines |
Unsafe Condition
Uncontained failure of the high pressure compressor rotor (HPCR) stage 3-9 spool due to a material defect in the hub to web transition area of the stage 6 disk.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a more detailed fluorescent penetrant inspection process for the HPCR stage 3-9 spools. Address any defects found in accordance with the specified inspection procedures.
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Compliance Time
Before further flight
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Affected Aircraft
General Electric Company CF6 series turbofan engines
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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