Airworthiness Directives; Turbomeca S.A. Turboshaft Engines
type: Action
additional type: https://schema.org/LegalForceStatus
description: We are adopting a new airworthiness directive (AD) for all Turbomeca S.A. ASTAZOU XIV B and XIV H engines. This AD was prompted by reports of cracks on the 2nd-stage turbine disk. This AD requires replacement of the 2nd-stage turbine disk. We are issuing this AD to prevent disk cracking, uncontained 2nd-stage turbine blade release, damage to the engine, and damage to the helicopter.
date published: 2014-01-10
start time: 2014-02-14
agent: Federal Aviation Administration
  type: GovernmentOrganization
  parent organization: US Department of Transportation
object: Turbomeca S.A. Turboshaft
citation: DigitalDocument
license: https://creativecommons.org/publicdomain/zero/1.0/
source: https://www.federalregister.gov/documents/2014/01/10/2014-00166/airworthiness-directives-turbomeca-sa-turboshaft-engines
source organization: US Federal Register
publisher: AI Analytics

PropertyValue
property ID: Federal Register Document Number
value: 2014-00166

PropertyValue
property ID: Federal Register Citation
value: 79 FR 1733

PropertyValue
property ID: FAA Docket
value: Docket No. FAA-2013-0575

AI Analytics
type: Organization