NASA-STD-5009C:2023
Current
Current
The latest, up-to-date edition.
Nondestructive Evaluation Requirements for Fracture Critical Metallic Components
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
03-08-2023
This NASA Technical Standard establishes the nondestructive evaluation (NDE) requirements for any NASA system or component, flight or ground, where fracture control and a quantitative demonstration of probability of detection (POD) are required.
DocumentType |
Standard
|
Pages |
54
|
PublisherName |
National Aeronautics and Space Administration
|
Status |
Current
|
Supersedes |
SAE AS4787A | Eddy Current Inspection of Circular Holes in Nonferrous Metallic Aircraft Engine Hardware |
ASTM E 1742/E1742M : 2018 | Standard Practice for Radiographic Examination |
SAE AMS2647G | Fluorescent Penetrant Inspection Aircraft Structures and Engine Component Maintenance |
ASTM E 1417/E1417M : 2021 | Standard Practice for Liquid Penetrant Testing |
SAE ARP 4402 A : 2020 | Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure |
ASTM E 2375 : 2022 | Standard Practice for Ultrasonic Testing of Wrought Products |
ASTM E 1444/E1444M : 2021 | Standard Practice for Magnetic Particle Testing for Aerospace |
NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
ASTM E 164 : 2019 | Standard Practice for Contact Ultrasonic Testing of Weldments |
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