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AD FAA-2008-0821

Airworthiness Directives; General Electric Company (GE) CF34-8E Series Turbofan Engines

Summary

The FAA is superseding an existing airworthiness directive (AD) for GE CF34-8E series turbofan engines with certain part number (P/N) full authority digital electronic controls (FADECs) installed. That AD currently requires removing certain P/N FADECs. This superseding AD requires removal of 12 more P/Ns of FADECs. This AD results from 20 additional reports received of loss of thrust control events since AD 2008-16-01 was issued. We are issuing this AD to prevent loss of thrust control of the airplane.

Directive Details

AD Number

FAA-2008-0821

Document Number

E9-27985

Type

Rule

Publication Date

November 23, 2009

Effective Date

December 28, 2009

Affected Manufacturer

General Electric Company (GE) CF34-8E Series Turbofan

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2008-0821

Topics

Air transportationAircraftAviation safetySafety

Official Documents

View all ADs for General Electric Company (GE) CF34-8E Series Turbofan →

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