NA 131
DIN Standards Committee Aerospace
DIN 65038-2 [CURRENT] referenced in following documents:
| Document number | Edition | Title |
|---|---|---|
| WL 1.6722-100 | 1992-08 | Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr, 0,2 Mo, comsumable electrode remelted; bars and forgings; design and production data, conversion More |
| WL 1.6723-1 | 1992-08 | Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr, 0,2 Mo; bars and forgings More |
| WL 1.6723-100 | 1992-08 | Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr, 0,2 Mo; bars and forgings; design and production data, conversion More |
| WL 1.6944-2 | 1984-07 | Ultra high-strength nickel-chromium-molybdenum steel with about 0.38C-1.8Ni-0.8Cr-0.35Mo-0.1V; rods and forgings More |
| WL 1.6974-1 | 1992-08 | Aerospace; high-strength hardened and tempered nickel-cobalt steel with approx. 0,3 C, 8 Ni, 4,5 Co, 1 Cr, 1 Mo, consumable electrode remelted; bars and forgings More |
| 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 2.4630-100 | 1993-08 | Aerospace; heat-resisting nickel alloy with approx. 0,1 C - 20 Cr - 0,4 Ti; sheet, strip, bars, forgings, tubes, wire and rivets; design and production data, conversion More |
| WL 2.4630-2 | 1993-08 | Aerospace; heat-resisting nickel alloy with approx. 0,1 C - 20 Cr - 0,4 Ti; bars and forgings More |
| WL 2.4631-100 | 1993-08 | Aerospace; heat-resisting nickel alloy with approx. 0,1 C - 20 Cr - 2,3 Ti - 1,4 Al; sheet, strip, bars and forgings; design and production data, conversion More |
| WL 2.4631-2 | 1993-08 | Aerospace; heat-resisting nickel alloy with approx. 0,1 C - 20 Cr - 2,3 Ti - 1,4 Al, consumable electrode remelted; bars and forgings More |
