Airworthiness Directives; Pratt & Whitney JT8D-200 Series Turbofan Engines
type: Action
additional type: https://schema.org/LegalForceStatus
description: This amendment adopts a new airworthiness directive (AD) that applies to Pratt & Whitney (PW) JT8D-209, -217, -217A, -217C, and -219 series turbofan engines. This amendment requires removal and replacement of protective coating of the 7th and 9th through 12th stage high pressure compressor (HPC) disks and the 8th stage HPC hub, initial and repetitive inspections for corrosion pits and cracks, and removal from service as required. This amendment is prompted by reports from operators of cracks observed in JT8D engine steel HPC disks. We are issuing this AD to prevent fracture of the 7th and 9th through 12th stage HPC disks and 8th stage HPC hub, resulting in uncontained engine failure and damage to the airplane.
date published: 2003-08-08
start time: 2003-09-12
agent: Federal Aviation Administration
  type: GovernmentOrganization
  parent organization: US Department of Transportation
object: Pratt & Whitney JT8D-200 Series Turbofan
citation: DigitalDocument
license: https://creativecommons.org/publicdomain/zero/1.0/
source: https://www.federalregister.gov/documents/2003/08/08/03-19828/airworthiness-directives-pratt-and-whitney-jt8d-200-series-turbofan-engines
source organization: US Federal Register
publisher: AI Analytics

PropertyValue
property ID: Federal Register Document Number
value: 03-19828

PropertyValue
property ID: Federal Register Citation
value: 68 FR 47207

PropertyValue
property ID: FAA Docket
value: Docket No. 2002-NE-41-AD

AI Analytics
type: Organization