Airworthiness Directives; General Electric Company CF34 Series Turbofan Engines
airworthiness · Rule · Final rule; request for comments. · Published 2001-05-16 · Effective 2001-05-31 · 66 FR 27017
Document
Document number
01-12006
Federal Register citation
66 FR 27017
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
General Electric Company CF34 Series Turbofan
Publication date
2001-05-16
Effective date
2001-05-31
FAA docket
Docket No. 2000-NE-42-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CF34-1A, -3A, -3A1, - 3A2, -3B, and -3B1 turbofan engines. This action requires a one-time inspection, and if necessary replacement of certain fan disks for electrical arc-out indications, and assigns a reduction in the life limit of certain fan disks. This amendment is prompted by a report of a crack that was found during a visual inspection as part of routine engine maintenance. The actions specified in this AD are intended to prevent rupture of the fan disk due to cracks that initiate at an electrical arc-out, which could result in an uncontained failure of the engine.