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.