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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.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 2016-03-05 |
| ICS | 49.040 : Coatings and related processes used in aerospace industry |
| Number of pages | 6 |
| Replace | SAE ARP 1925A:2000-10-01 |
| Set | AEROPAKS10U-10 |
| Year | 2016 |
| Document history | SAE ARP 1925A:2000-10-01 |
| Country | USA |
| Keyword | SAE 1925;SAE ARP1925B;SAE ARP1925B;SAE ARP 1925 |