540 PG 8700.2.1A - FOIA and eLibrary website! - NASA

DIRECTIVE NO. 540-PG-8700.2.1A Page 2 of 9EFFECTIVE DATE: 09/28/2009EXPIRATION DATE: 09/28/2014P.7 TRAININGN/AP.8 RECORDS* NRRS – NASA Records Retention Schedule (NPR 1441.1)Record Title Record Custodian RetentionStress Analysis Hardware Owner 5 Yrs or until Project CompletionTipping Analysis Hardware Owner 5 Yrs or until Project CompletionProof Test Hardware Owner 5 Yrs or until Project CompletionNDT Report Hardware Owner 5 Yrs or until Project CompletionP.9 METRICSN/AP.10 DEFINITIONSCatastrophicHazardCritical FastenerCritical WeldNDT (Non-Destructive Test)PayloadA condition in which a failure can result in disabling or fatal personnel injury, the loss of aspacecraft or launch vehicle.A fastener where the single failure would result in a Catastrophic HazardA weld where the single failure of which could result in disabling or fatal personnel injury ordamage to property or flight hardware.The development and application of technical methods to examine materials or components inways that do not impair future usefulness and serviceability in order to detect, locate, measureand evaluate flaws; to assess integrity, properties and composition; and to measure geometricalcharacteristics.Any flight hardware supported by MGSEP.11 ACRONYMSDLL Design Limit LoadFS Factor of SafetyGSFC Goddard Space Flight CenterOEM Original Equipment ManufacturerMGSE Mechanical Ground Support EquipmentMS Margin of SafetyS/C SpacecraftCHECK THE GSFC DIRECTIVES MANAGEMENT SYSTEM AThttp://gdms.gsfc.nasa.gov/gdmsnew/home.jsp TO VERIFY THAT THIS IS THE CORRECT VERSION PRIOR TO USE.GSFC 3-18 (7/06)