Airworthiness Directives; General Electric Company CF6-50 and - 80C2 Series Turbofan Engines
airworthiness · Rule · Final rule; request for comments. · Published 1997-10-31 · Effective 1997-11-17 · 62 FR 58892
Document
Document number
97-28742
Federal Register citation
62 FR 58892
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
General Electric Company CF6-50 and - 80C2 Series Turbofan
Publication date
1997-10-31
Effective date
1997-11-17
FAA docket
Docket No. 97-ANE-52-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CF6-50 and -80C2 series turbofan engines. This action requires removal from service of defective high pressure compressor rotor (HPCR) stage 3-9 spools, and replacement with serviceable parts. This amendment is prompted by a report of an uncontained failure of an HPCR stage 3-9 spool installed on a GE model CF6-80C2 turbofan engine. The actions specified in this AD are intended to prevent failure of the HPCR stage 3-9 spool, which can result in an uncontained engine failure and damage to the aircraft.