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ASTM F2108-17
Standard Practice for Inspection of Transparent Parts by PrismMore info
1.1 Aerospace transparencies undergo high stresses induced by flight, environmental, or other factors. The transparency attachment points are especially subject to fatigue. These areas of fatigue are often obstructed or hidden from normal inspection. An inspector, following the techniques described in this practice, shall use a prism to view damage located near transparency bolt holes, voids, and delamination that are hidden by edge strips or frames.
| Author | ASTM |
|---|---|
| Editor | ASTM |
| Document type | Standard |
| Format | File |
| ICS | 19.100 : Non-destructive testing |
| Number of pages | 7 |
| Replace | ASTM F2108-06(2011) |
| Set | ASTMVOL1503 |
| Year | 2017 |
| Document history | ASTM F2108-06(2011) |
| Country | USA |
| Keyword | ASTM 2108;ASTM F2108;ASTM F2108;10.1520/F2108-17 |