AD 2000-03-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric | Company CF6-80C2 Series | Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan Engines |
Unsafe Condition
Fan mid shaft failure due to exceeding the new lower cyclic life limit, which could result in uncontained engine failure and damage to the aircraft.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove affected fan mid shafts from service prior to reaching the new lower cyclic life limit and replace with serviceable parts.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight if the fan mid shaft has reached or will reach the new cyclic life limit.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
General Electric Company CF6-80C2 series 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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