AD 2002-10-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric | Company CF6-80E1A2 | Airworthiness Directives; General Electric Company CF6-80E1A2 Turbofan Engines |
Unsafe Condition
Exceeding the life limit of the low pressure turbine rotor (LPTR) shaft may result in low cycle fatigue (LCF) cracking and failure, potentially leading to an uncontained engine failure and damage to the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the low pressure turbine rotor (LPTR) shaft at or before reaching the new reduced life cycle limit.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before reaching the new reduced life cycle limit.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
General Electric Company CF6-80E1A2 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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