Airworthiness Directives; General Electric Company CF34-3A1 and -3B1 Series Turbofan Engines
airworthiness · Rule · Final rule; request for comments. · Published 2004-07-30 · Effective 2004-08-16 · 69 FR 45562
Document
Document number
04-17040
Federal Register citation
69 FR 45562
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
General Electric Company CF34-3A1 and -3B1 Series Turbofan
Publication date
2004-07-30
Effective date
2004-08-16
FAA docket
Docket No. FAA-2004-18648
Abstract
The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF34-3A1 and -3B1 series turbofan engines with certain serial numbers (SNs) of stage 5 low pressure turbine (LPT) disks, part number (P/N) 6078T92P01, and or certain SNs of stage 6 LPT disks, P/N 6089T89P01. This AD requires initial and repetitive visual and eddy current inspections of those disks. This AD also allows as optional terminating action to the repetitive inspections, replacement of those SN disks. This AD also requires replacement of certain stage 5 and stage 6 LPT disks. This AD results from a report of a stage 5 LPT disk that failed due to cracking from low-cycle-fatigue (LCF) during factory testing. We are issuing this AD to prevent LCF failure of stage 5 LPT disks and stage 6 LPT disks, which could lead to uncontained engine failure.