Summary
This recommended practice establishes a procedure for the application of long string abrasive monofilaments to machined aircraft structures for the purpose of removing burrs produced during the machining operations. This procedure is typically applicable to aluminum, titanium, and steel, but usage is not limited to such applications.
Notes
Approuvée 2010-05-19, 2010-05-00, 2006-04-00.
Technical characteristics
| Publisher | SAE International |
| Publication Date | 08/09/2021 |
| Confirmation Date | 08/09/2021 |
| Page Count | 6 |
| Themes | Aerospace |
| EAN | --- |
| ISBN | --- |
| Weight (in grams) | --- |
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