Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,14 C, 3 Ni, 1 Cr, 0,2 Mo, consumable electrode remelted; bars and forgings; design and production data, conversion
Edition 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
Edition 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; design and production data, conversion
Edition 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
Edition 1992-08

Aerospace; heat-resisting nickel alloy with approx. 0,05C-19Cr-18Fe-5Nb-3Mo; vacuum melted and consumable electrode remelted; sheets, strips, bars, forgings, filler wire for welding and bars and wire for screws and bolts; design and production data, conversion
Edition 1993-02

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
Edition 1992-08

Aerospace series - Wrought copper alloys with approx. 14 Ni - 3 Al - 1 Fe - Part 100: Bars and forgings; design and production data, conversion
Edition 2012-10

Aerospace series - High temperature nickel alloy with approx. 0,2 C - 20 Cr - Part 100: Welding filler metal - Notes for design and production, cross-reference
Edition 2012-10