AD 2002-05-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric | Company CF34-3A1 and -3B1 Series | Airworthiness Directives; General Electric Company CF34-3A1 and -3B1 Series Turbofan Engines; Correction |
Unsafe Condition
Cracks in the high-pressure turbine (HPT) blade platforms can occur due to high-cycle fatigue.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct inspections for cracks in the HPT blade platforms using the specified methods and replace affected blades if cracks are found.
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 CF34-3A1 and -3B1 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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.