Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
€165.00
Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
Specification for aircraft material. ¾ per cent nickel-chromium case-hardening steel
€95.00
Specification for 3 per cent chromium-molybdenum-vanadium steel (vacuum remelted - air hardening) (157 kgf/mm2 (100 tonf/in2): limiting ruling section 30 mm (1? in))
Specification for 1½ per cent nickel-chromium-molybdenum steel (110/130 kgf/mm2 (70/83 tonf/in2): limiting ruling section 70 mm (2¾ in))
Specification for 12 per cent chromium corrosion-resisting steel (60/80 kgf/mm2 (38/51 tonf/in2): limiting ruling section 150 mm (6in))
Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel (precipitation hardening) billets, bars, forgings and parts (1130-1330 MPa)
Specification for patented cold drawn carbon steel wire and springs (high duty unground wire)
Specification for patented cold drawn carbon steel wire and springs (high duty ground wire)
Specification for carbon steel wire and springs (high duty unground wire - hardened and tempered)
Specification for chromium-vanadium steel wire and springs (high duty ground wire - hardened and tempered)
Specification for austenitic chromium-nickel steel wire and springs
Inspection and testing procedure for steel sheet and strip
€269.00
Specification for carbon-manganese steel sheet and strip (93/116 hbar)
Specification for carbon-manganese steel sheet and strip (116/131 hbar)
