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Airworthiness Directives; General Electric Company CF6-45A, CF6-50A, CF6-50C, and CF6-50E Series Turbofan Engines

airworthiness · Rule · Final rule. · Published 2005-12-22 · Effective 2006-01-26 · 70 FR 75933

Document

Document number
05-24341
Federal Register citation
70 FR 75933
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-12-22
Effective date
2006-01-26
FAA docket
Docket No. FAA-2005-22124

Abstract

The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF6-45A, CF6-50A, CF6-50C, and CF6-50E series turbofan engines. This AD requires removing from service pre-GE Service Bulletin (SB) No. CF6-50S/B 72-1268 configuration low pressure turbine (LPT) stage 2 interstage seal assemblies and stage 3 interstage seal assemblies. This AD also requires installing new or reworked configuration stage 2 interstage seal assemblies and stage 3 interstage seal assemblies. This AD results from reports of fan mid shaft separation, leading to separation of the LPT stage 1 disk, disk overspeed, and uncontained engine failure. We are issuing this AD to prevent uncontained engine failure and damage to the airplane.

Source

Authoritative
Federal Register document
Machine
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