AD 2008-16-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric | Co | Airworthiness Directives; General Electric Co. (GE) CF34-8E Series Turbofan Engines |
Unsafe Condition
Loss of thrust control events from the same software fault scenario in FADEC software version 8Ev5.40.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Reprogram the FADEC software to an FAA-approved version or replace the FADEC with a non-listed part number.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 660 flight hours time-in-service after the effective date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
GE CF34-8E series turbofan engines with FADEC part numbers 4120T00P47, 4120T00P48, 111E9320G48, or 111E9320G49, installed on, but not limited to, EMBRAER ERJ 170 series airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.