Airworthiness Directives; General Electric Company CF6-45 and CF6-50 Series Turbofan Engines
airworthiness · Rule · Final rule; request for comments. · Published 2010-03-17 · Effective 2010-04-01 · 75 FR 12661
Document
Document number
2010-5777
Federal Register citation
75 FR 12661
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
General Electric Company CF6-45 and CF6-50 Series Turbofan
Publication date
2010-03-17
Effective date
2010-04-01
FAA docket
Docket No. FAA-2010-0068
Abstract
The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF6-45 and CF6-50 series turbofan engines with certain low-pressure turbine (LPT) stage 3 disks installed. This AD requires fluorescent penetrant inspection (FPI) of the LPT stage 3 disk under certain conditions and removal of the disk from service before further flight if found cracked. This AD also requires initial and repetitive borescope inspections of the high-pressure turbine (HPT) rotor stage 1 and stage 2 blades for wear and damage, including excessive airfoil material loss. This AD results from three reports of uncontained failures of LPT stage 3 disks and eight reports of cracked LPT stage 3 disks found during shop visit inspections. We are issuing this AD to prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.