NA 131
DIN Standards Committee Aerospace
DIN EN 7010 [CURRENT] references following documents:
| Document number | Edition | Title |
|---|---|---|
| WL 1.7224-1 | 1992-03 | Aerospace; hardened and tempered chromium-molybdenum steel with approx. 0,35C-1Cr-0,2Mo; bars and wire for bolts and nuts to be cold or hot formed More |
| WL 1.7784-3 | 2012-10 | Aerospace series - Ultrahigh-strength chromium-molybdenum-vanadium steel with approx. 0,4 C - 5 Cr - 1,3 Mo - 0,5 V - Part 3: Bar and wire for cold-or-hot-formed bolts and nuts More |
| WL 2.4668-2 | 1984-07 | High temperature nickel alloy with about 0.05C-19Cr-18Fe-5Nb-3Mo; rods and forgings More |
| WL 3.7164-2 | 1990-11 | Aerospace; titanium alloy with approx. 6Al-4V; bars and forgings More |
| DIN EN ISO 10664 | 2015-01 | Hexalobular internal driving feature for bolts and screws (ISO 10664:2014); German version EN ISO 10664:2014 More |
| DIN EN ISO 4757 | 1994-10 | Cross recesses for screws (ISO 4757:1983); German version EN ISO 4757:1994 More |
| DIN ISO 1891 | 2009-09 | Fasteners - Terminology (ISO 1891:2009) More |
| ISO 8168 | 2016-08 | Aerospace - Bolts, with MJ threads, made of heat and corrosion resisting steel, strength class 1 100 MPa - Procurement specification More |
| ISO 9152 | 1998-11 | Aerospace - Bolts, with MJ threads, in titanium alloys, strength class 1100 MPa - Procurement specification More |
