Airworthiness Directives; General Electric Company CF6-80C2 and CF6-80E1 Series Turbofan Engines
type: Action
additional type: https://schema.org/LegalForceStatus
description: The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF6-80C2 and CF6-80E1 series turbofan engines with high-pressure compressor rotor (HPCR) spool shaft stage 14 disks, part number (P/N) 1703M49G02, 1703M49G03, or 1509M71G10 installed. This AD requires a one-time eddy current inspection (ECI) of the HPCR spool shaft stage 14 disk web for crack indications, and removing from service any parts with web cracks. This AD results from reports of 12 HPCR spool shaft stage 14 disks with web cracks discovered to date. We are issuing this AD to prevent cracks from propagating to an uncontained failure of the disk and damage to the airplane.
date published: 2009-03-26
start time: 2009-04-30
agent: Federal Aviation Administration
  type: GovernmentOrganization
  parent organization: US Department of Transportation
object: General Electric Company CF6-80C2 and CF6-80E1 Series Turbofan
citation: DigitalDocument
license: https://creativecommons.org/publicdomain/zero/1.0/
source: https://www.federalregister.gov/documents/2009/03/26/E9-6387/airworthiness-directives-general-electric-company-cf6-80c2-and-cf6-80e1-series-turbofan-engines
source organization: US Federal Register
publisher: AI Analytics

PropertyValue
property ID: Federal Register Document Number
value: E9-6387

PropertyValue
property ID: Federal Register Citation
value: 74 FR 13092

PropertyValue
property ID: FAA Docket
value: Docket No. FAA-2008-1025

AI Analytics
type: Organization