NASA STD 5009(INT) : 2006
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE CRITICAL METALLIC COMPONENTS
07-04-2008
01-01-2006
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
4.2 Standard NDE
4.3 Special NDE
4.4 NDE Documentation
4.5 Personnel Qualification and Certification
5. GUIDANCE
5.1 Reference Documents
Appendix A Example of an NDE Organization
Establishes the nondestructive evaluation (NDE) requirements for fracture control of all aerospace flight systems including manned and unmanned spaceflight systems, manned and unmanned aeronautical systems, payloads, flight experiments and associated ground based hardware.
| DevelopmentNote |
Expires 10 Sept 2007. (10/2006)
|
| DocumentType |
Standard
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Superseded
|
| SupersededBy |
| NASA STD 6016(INT) : 2006 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 5019(INT) : 2006 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| MIL-HDBK-1823 Revision A:2009 | NONDESTRUCTIVE EVALUATION SYSTEM, RELIABILITY ASSESSMENT |
| SAE AS4787 | 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 |
| ASTM E 2375 : 2016 : REDLINE | Standard Practice for Ultrasonic Testing of Wrought Products |
| ASTM E 1444 : 2005 | Standard Practice for Magnetic Particle Testing |
| NASA STD 5003 : 0 | FRACTURE CONTROL REQUIREMENTS FOR PAYLOADS USING THE SPACE SHUTTLE |
| SAE ARP4402 | Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure |
| NASA STD 5007 : 2001 | GENERAL FRACTURE CONTROL REQUIREMENTS FOR MANNED SPACEFLIGHT SYSTEMS |
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