AD 2003-01-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric | Co | Airworthiness Directives; General Electric Co. CF6-80A Series Turbofan Engines |
Unsafe Condition
Cracks in certain part number (P/N) stage 1 high pressure turbine (HPT) rotor disks.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the specified stage 1 HPT rotor disks using etch preparations and fluorescent penetrant inspections, visual inspections, and eddy current inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
General Electric Co. CF6-80A series turbofan engines with certain part number (P/N) stage 1 high pressure turbine (HPT) rotor disks.
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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