ASD-STAN
| Registration number (WIID) | Project No. | Title | Status |
|---|---|---|---|
| 17197 | EN 3481:2019 | Aerospace series - Steel X8CrNiTi18-10 (1.4878/1.4544) - Annealed - Reference heat treatment: softened - Hollow bars - 5 mm ≤ a ≤ 12 mm | Izstrādē |
| 64249 | EN 4859:2019 | Aerospace series - Sensor based clamp load determination / high tensile bolts - Technical specification | Izstrādē |
| 17225 | prEN 3509 | Steel FE-PL48 - Hardened and tempered - 1050 <or= RM <or= 1250 MPa - Bar for machining - DE <or= 40 mm | Izstrādē |
| 17043 | prEN 3318 | Titanium alloy TI-P64 - Not heat treated - Reference heat treatment - Annealed - Grade 2 forging stocks - DE <or= 360 mm | Izstrādē |
| 17181 | prEN 3462 | Titanium TI-P11 - Annealed - 540 <or= RM <or= 770 MPa - Bar for machining - DE <or= 150 mm | Izstrādē |
| 17127 | EN 3389:2009 | Aerospace series - Fasteners, externally threaded, in heat resisting nickel base alloy NI-PH1302 (Waspaloy) - Classification: 1 210 MPa/730 °C - Manufacturing method optional - Technical specification | Izstrādē |
| 16990 | EN 3218-007:2006 | Aerospace series - Connectors, rectangular, with metallic shells and screw-locking - Part 007: Plug with rear-removable size 20 crimp contacts - Product standard | Izstrādē |
| 17073 | prEN 3348 | Aluminium alloy <2024> - Solution treated and artificially aged <T62> - Plate - 6 <or= A <or= 50 mm | Izstrādē |
| 16885 | prEN 3122 | Aluminium alloy AL-C27 - Solution treated and artificially aged (T6) - High strength - Structural precision castings | Izstrādē |
| 17039 | EN 3314:2019 | Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Bar for machining - D ≤ 75 mm | Izstrādē |
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