NA 131
DIN Standards Committee Aerospace
DIN 65038-1 [Withdrawn] referenced in following documents:
| Document number | Edition | Title |
|---|---|---|
| DIN 65038-2 | 1983-08 | Aerospace; bars of steel, nickel alloys and cobalt alloys for aircraft; technical specification; sampling More |
| LN 671 | 1987-08 | Aerospace; bright round steel; tolerances according to ISO tolerance class h9; dimensions, masses More |
| WL 1.3934 | 1981-03 | Precipitation-hardening nickel-manganese-chromium steel with large thermal expansion, with about 0.7 C-12 Ni-5 Mn-3 Cr-1 V; rods and forgings More |
| WL 1.4044 | 1981-03 | Stainless heat-treatable chromium steel with about 0.2 C-17 Cr-2 Ni; rods and forgings More |
| WL 1.4574-3 | 1985-10 | Aerospace; ultrahigh-strenght precipitation hardening stainless chromium-nickel-molybdenum-aluminium steel with approx. 0,07C-15Cr-7Ni-2,5Mo-1Al; bar and forging More |
| WL 1.4911 | 1981-03 | High temperature heat-treatable chromium-cobalt-molybdenum steel with about 0.1 C-11 Cr-6 Co-0.8 Mo-0.4 Nb-0.4 V; rods and forgings More |
| WL 1.4914 | 1981-03 | High temperature heat-treatable chromium-molybdenum steel with about 0.15 C-11 Cr-0.7 Mo-0.4 Nb-0.4 V; rods and forgings More |
| WL 1.4933-2 | 1981-03 | High temperature heat-treatable chromium-nickel-molybdenum steel with about 0.1 C-12 Cr-2.5 Ni-1.8 Mo-0.3 V, air molten; rods and forgings More |
| WL 1.4939-2 | 1981-03 | High temperature heat-treatable chromium-nickel-molybdenum steel with about 0.1 C-12 Cr-2.5 Ni-1.8 Mo-0.3 V, remelted; rods and forgings More |
| WL 1.4944-2 | 1984-07 | High temperature precipitation-hardening nickel-chromium-titanium steel with about 0.06C-25Ni-15Cr-2.1Ti-1.2Mo; rods and forgings More |
