NASA STD 5009 : 2008
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE-CRITICAL METALLIC COMPONENTS - MEASUREMENT SYSTEM IDENTIFICATION: METRIC (INCH-POUND)
02-11-2018
01-01-2008
DOCUMENT HISTORY LOG
FOREWORD
1 SCOPE
1.1 Purpose
1.2 Applicability
2 APPLICABLE DOCUMENTS
2.1 General
2.2 Government Documents
2.3 Non-Government Documents
2.4 Order of Precedence
3 ACRONYMS AND DEFINITIONS
3.1 Acronyms
3.2 Definitions
4 NDE REQUIREMENTS
4.1 NDE Procedures, Standards, and Methods
4.1.1 Cracks
4.1.2 Material Review Board (MRB)
4.1.3 Detailed NDE Requirements
4.1.4 NDE Drawing Callouts
4.1.5 NDE Process and Configuration Control
4.1.6 Capability Demonstration Specimens
4.1.7 Supporting Data and Record Retention
4.1.8 Organizational Guidelines and Documentation
Requirement
4.2 Standard NDE
4.2.1 Standard NDE Methods
4.2.2 Standard NDE Crack Sizes
4.2.3 Table 1 (or 2) - Minimum Detectable Flaw Sizes
Conditional Notes
4.2.4 Demonstration of Standard NDE Capability
4.2.5 Inability to Meet Standard NDE Inspection Process
Requirements
4.2.6 Standard NDE Classification Justification
4.2.7 Standard NDE Deviations
4.3 Special NDE
4.3.1 General
4.3.2 Special NDE Crack Sizes
4.3.3 Demonstration of Special NDE Capability
4.3.4 NDE Capability Demonstration Specimens
4.3.5 Point Estimate Method
4.3.6 POD Method
4.4 NDE Documentation
4.4.1 NDE Plan
4.4.2 NDE Summary Report
4.4.3 Supporting Data and Record Retention
4.5 Personnel Qualification and Certification
4.5.1 Standard NDE Qualification and Certification
4.5.2 Special NDE Qualification and Certification
5 GUIDANCE
5.1 Reference Documents
5.1.1 Government Documents
5.1.2 Non-Government Documents
Appendix A - Example of an NDE Organization
Establishes the nondestructive evaluation (NDE) requirements for any NASA system or component, flight or ground, where fracture control is a requirement. Also defines the primary requirements for NDE in support of NASA-STD-5019.
DevelopmentNote |
Supersedes NASA STD 5009(INT) & NASA MSFC STD 1249. (05/2008)
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DocumentType |
Standard
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PublisherName |
National Aeronautics and Space Administration
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Status |
Superseded
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SupersededBy | |
Supersedes |
NASA MSFC SPEC 3679 : 2012 | PROCESS SPECIFICATION - WELDING AEROSPACE HARDWARE |
NASA PRC 0001 : 2012 | PROCESS SPECIFICATION FOR THE MANUAL ARC WELDING OF ALUMINUM ALLOY HARDWARE |
NASA MSFC SPEC 3635 : 2012 | PYROTECHNIC SYSTEM SPECIFICATION |
NASA PRC 6510 : 2011 | PROCESS SPECIFICATION FOR ULTRASONIC INSPECTION OF WELDS |
NASA PRC 6509 : 2011 | PROCESS SPECIFICATION FOR EDDY CURRENT INSPECTION |
NASA STD 5005 : 2013 | STANDARD FOR THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
NASA PRC 6506 : 2011 | PROCESS SPECIFICATION FOR LIQUID PENETRANT INSPECTION |
NASA PRC 6505 : 2011 | PROCESS SPECIFICATION FOR MAGNETIC PARTICLE INSPECTION |
NASA PRC 0015 : 2016 | PROCESS SPECIFICATION FOR AUTOMATIC AND MACHINE ARC WELDING OF TITANIUM AND TITANIUM ALLOY HARDWARE |
NASA KSC DE 512-SM : 2012 | FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS |
NASA TM 218770 : 2015 | NASA DOEPOD NDE CAPABILITIES DATA BOOK |
NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
NASA STD 5006 : 2015 | GENERAL FUSION WELDING REQUIREMENTS FOR AEROSPACE MATERIALS |
NASA STD 8719.24 : 2011 | NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS |
NASA PRC 0010 : 2012 | PROCESS SPECIFICATION FOR AUTOMATIC AND MACHINE ARC WELDING OF STEEL AND NICKEL ALLOY HARDWARE |
NASA PRC 0005 : 2012 | PROCESS SPECIFICATION FOR THE MANUAL ARC WELDING OF CARBON STEEL AND NICKEL ALLOY HARDWARE |
NASA PRC 6503 : 2011 | PROCESS SPECIFICATION FOR RADIOGRAPHIC INSPECTION |
NASA PRC 0002 : 2012 | PROCESS SPECIFICATION FOR THE MANUAL ARC WELDING OF TITANIUM ALLOY HARDWARE |
NASA MSFC STD 3716 : 2017 | STANDARD FOR ADDITIVELY MANUFACTURED SPACEFLIGHT HARDWARE BY LASER POWDER BED FUSION IN METALS |
NASA PRC 0014 : 2012 | PROCESS SPECIFICATION FOR FRICTION STIR WELDING |
NASA HDBK 5010 : 0 | FRACTURE CONTROL IMPLEMENTATION HANDBOOK FOR PAYLOADS, EXPERIMENTS, AND SIMILAR HARDWARE |
NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
NASA GSFC STD 7000 : 2013 | GENERAL ENVIRONMENTAL VERIFICATION STANDARD (GEVS) FOR GSFC FLIGHT PROGRAMS AND PROJECTS |
NASA JSC 25863 : 2009 | FRACTURE CONTROL PLAN FOR JSC SPACE-FLIGHT HARDWARE |
ASTM E 2982 : 2014 | Standard Guide for Nondestructive Testing of Thin-Walled Metallic Liners in Filament-Wound Pressure Vessels Used in Aerospace Applications |
SAE AS 4787 : 2013 | EDDY CURRENT INSPECTION OF CIRCULAR HOLES IN NONFERROUS METALLIC AIRCRAFT ENGINE HARDWARE |
SAE AMS2647E | FLUORESCENT PENETRANT INSPECTION, AIRCRAFT AND ENGINE COMPONENT MAINTENANCE |
NAS410:2003 | NAS CERTIFICATION & QUALIFICATION OF NONDESTRUCTIVE TEST PERSONNEL |
NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
ASTM E 2375 : 2016 : REDLINE | Standard Practice for Ultrasonic Testing of Wrought Products |
ASTM E 1444 : 2005 | Standard Practice for Magnetic Particle Testing |
SAE ARP 4402 : 2013 | EDDY CURRENT INSPECTION OF OPEN FASTENER HOLES IN ALUMINUM AIRCRAFT STRUCTURE |
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