AD 2002-01-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric | Company CF6-80E1 Model | Airworthiness Directives; General Electric Company CF6-80E1 Model Turbofan Engines |
Unsafe Condition
HPT stage two (S2) nozzle guide vane (NGV) distress leading to blade failure and potential uncontained engine failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect HPT stage two (S2) nozzle guide vanes (NGV) using a flex borescope to detect distress.
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
General Electric Company CF6-80E1 model turbofan 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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