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

airworthiness · Rule · Final rule; request for comments. · Published 2007-03-07 · Effective 2007-03-12 · 72 FR 10054

Document

Document number
E7-3833
Federal Register citation
72 FR 10054
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
General Electric
Publication date
2007-03-07
Effective date
2007-03-12
FAA docket
Docket No. FAA-2007-27308

Abstract

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.

Source

Authoritative
Federal Register document
Machine
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