Airworthiness Directives; Airbus Model A310 Series Airplanes
type: Action
additional type: https://schema.org/LegalForceStatus
description: This amendment adopts a new airworthiness directive (AD), applicable to all Airbus Model A310 series airplanes, that requires electrical conductivity testing to verify the correct heat treatment of the two half fittings holding the ejection jack for the ram air turbine (RAT). This action is necessary to prevent decreased structural integrity of the two half fittings and loss of the RAT during extension, which could lead to reduced controllability of the airplane in the event of a dual engine failure, or in the event of loss of two or all hydraulic systems. This action is intended to address the identified unsafe condition.
date published: 2003-09-11
start time: 2003-10-16
agent: Federal Aviation Administration
  type: GovernmentOrganization
  parent organization: US Department of Transportation
object: Airbus Model A310 Series
citation: DigitalDocument
license: https://creativecommons.org/publicdomain/zero/1.0/
source: https://www.federalregister.gov/documents/2003/09/11/03-22708/airworthiness-directives-airbus-model-a310-series-airplanes
source organization: US Federal Register
publisher: AI Analytics

PropertyValue
property ID: Federal Register Document Number
value: 03-22708

PropertyValue
property ID: Federal Register Citation
value: 68 FR 53498

PropertyValue
property ID: FAA Docket
value: Docket No. 2002-NM-179-AD

AI Analytics
type: Organization