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Acceptance Criteria - Magnetic Particle, Fluorescent Penetrant, and Contrast Dye Penetrant Inspection
- Aerospace Standard
Published October 26, 2018 by SAE International in United States
Downloadable datasets availableAnnotation ability available
To establish the acceptance criteria for discontinuities as revealed by magnetic particle or liquid penetrant examination of aircraft utility parts as in 1.2.
All figures updated to show requirements in more clarity, Specs updated, Para 3.1.1 magnification changed from X10 to X100, Headings for table 2 corrected to show correct callout.
|Aerospace Material Specification||Magnetic Particle Acceptance Criteria for Parts|
|Aerospace Standard||NUT-HEX, CHECK, UNS G87400|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Table 1||Acceptance criteria for type of part|
|Table 2||Thread height|
|Table 3||Permissible surface discontinuities - internal threads (laps, seams, and inclusions)|
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
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