NA 131
DIN Standards Committee Aerospace
DIN 65038-2 [CURRENT] referenced in following documents:
Document number | Edition | Title |
---|---|---|
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 1.4943-100 | 1992-08 | Aerospace; high-strength precipitation-hardening nickel-chromium-titanium steel with aprox. 0,03 C, 25 Ni, 15 Cr, 1,8 Ti, consumable electrode remelted; sheets, plate, strip, bars, forgings and filler metal for welding; design and production data, conversion More |
WL 1.4943-2 | 1992-08 | Aerospace; heat-resisting precipitation-hardening nickel-chromium-titanium steel with approx. 0,03 C, 25 Ni, 15 Cr, 1,8 Ti, consumable elektrode remelted; bars 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 |
WL 1.4944-3 | 1984-07 | High temperature precipitation-hardening nickel-chromium-titanium steel with about 0.06C-25Ni-15Cr-2.1Ti-1.2Mo; rods and wire for screws and nuts More |
WL 1.5924-1 | 1992-08 | Aerospace; case-hardening chromium-nickel-steel with approx. 0,15 C, 1,5 Cr, 1,5 Ni; bars and forgings More |
WL 1.6657-1 | 1992-08 | Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,14 C, 3 Ni, 1 Cr, 0,2 Mo; bars and forgings More |
WL 1.6657-100 | 1992-08 | Aerospace; case-hardening nickel-chromium-molydenum steel with approx. 0,14 C, 3 Ni, 1 Cr, 0,2 Mo; bars and forgings; design and production data, conversion More |
WL 1.6658-1 | 1992-08 | Aerospace; case-hardening nickel-chromium-molydenum steel with approx. 0,14 C, 3 Ni, 1 Cr, 0,2 Mo, consumable electrode remelted; bars and forgings More |
WL 1.6722-1 | 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 More |