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Emergency ADRule

AD FAA-2007-27308

Airworthiness Directives; General Electric Aircraft Engines (GE) CF34-3A1/-3B/-3B1 Turbofan Engines

Summary

This action supersedes emergency airworthiness directive (AD) 2007-04-51 that was sent previously to all known U.S. owners and operators of GE CF34-3A1/-3B/-3B1 turbofan engines. That action required a onetime visual and tactile inspection of certain areas of certain serial number (SN) fan disks for an arc-out defect, within 20 engine flight hours after the effective date of that AD. This AD supersedes AD 2007-04-51 and adds eight SNs to the list of suspect fan disks. This AD results from GE discovering eight additional SNs of fan disks suspected of having an arc-out defect, and from the original report that a GE CF34-3B1 turbofan engine experienced an uncontained fan disk failure during flight operation. We are issuing this AD to prevent an uncontained fan disk failure and airplane damage.

Directive Details

AD Number

FAA-2007-27308

Document Number

E7-3833

Type

Rule

Publication Date

March 7, 2007

Effective Date

March 12, 2007

Affected Manufacturer

General Electric Aircraft Engines (GE) CF34-3A1/-3B/-3B1 Turbofan

Criticality

critical

Emergency

Yes

Docket ID

Docket No. FAA-2007-27308

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for General Electric Aircraft Engines (GE) CF34-3A1/-3B/-3B1 Turbofan →

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