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49.025.10 Steels
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BS 2S 130:1976
Specification for 18/9 chromium-nickel corrosion-resisting steel (niobium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm)
Specification for 18/9 chromium-nickel corrosion-resisting steel (niobium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm)
Released: 1976-08-31
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BS 4S 14:1964+A2:2015
Specification for Carbon case-hardening steel
Specification for Carbon case-hardening steel
Released: 2015-09-30
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BS EN 2448:2008
Aerospace series. Steel FE-PL1503 (35CrMo4). 900 MPa ≤ Rm ≤ 1100 MPa. Bars. De ≤ 40 mm
Aerospace series. Steel FE-PL1503 (35CrMo4). 900 MPa ≤ Rm ≤ 1100 MPa. Bars. De ≤ 40 mm
Released: 2009-09-30
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BS 2S 142:1977
Specification for 1% chromium-molybdenum steel billets, bars, forgings and parts (900-1100 MPa: limiting ruling section 40 mm)
Specification for 1% chromium-molybdenum steel billets, bars, forgings and parts (900-1100 MPa: limiting ruling section 40 mm)
Released: 1977-04-29
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BS 2HR 53:2010
Specification for nickel-iron-chromium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (Ni/Co 42.5, Cr 12.5, Mo 5.8, Ti 3.0, Fe remainder)
Specification for nickel-iron-chromium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (Ni/Co 42.5, Cr 12.5, Mo 5.8, Ti 3.0, Fe remainder)
Released: 2010-01-31
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BS EN 3330:2009
Aerospace series. Steel FE-PL1503 (35CrMo4). Annealed. Bar and wire. De ≤ 40 mm. For prevailing torque nuts
Aerospace series. Steel FE-PL1503 (35CrMo4). Annealed. Bar and wire. De ≤ 40 mm. For prevailing torque nuts
Released: 2009-07-31
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BS EN 3973:2006
Aerospace series. Steel FE-CM3801 (X5CrNiCuNb16-4). Homogenized, solution treated and precipitation hardened. Investment casting. De ≤ 50 mm. Rm ≥ 1030 MPa
Aerospace series. Steel FE-CM3801 (X5CrNiCuNb16-4). Homogenized, solution treated and precipitation hardened. Investment casting. De ≤ 50 mm. Rm ≥ 1030 MPa
Released: 2007-01-31
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BS EN 4642:2009
Aerospace series. Steel FE-PM 3504 (X4CrNiMo16-5-1). Air melted. Hardened and tempered. Sheet and plate. 0,6 mm ≤ a ≤ 50 mm. 900 MPa ≤ Rm ≤ 1050 MPa
Aerospace series. Steel FE-PM 3504 (X4CrNiMo16-5-1). Air melted. Hardened and tempered. Sheet and plate. 0,6 mm ≤ a ≤ 50 mm. 900 MPa ≤ Rm ≤ 1050 MPa
Released: 2009-07-31
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BS EN 4721:2014
Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted and electroslag remelted (ESR). Hardened and tempered. Bar. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa
Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted and electroslag remelted (ESR). Hardened and tempered. Bar. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa
Released: 2014-10-31
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BS EN 4216:2007
Aerospace series. Steel FE-CM3801 (GX5CrNiCuNb16-4). Homogenized, solution treated and precipitation hardened, investment casting De ≤ 50 mm, Rm ≥ 900 MPa
Aerospace series. Steel FE-CM3801 (GX5CrNiCuNb16-4). Homogenized, solution treated and precipitation hardened, investment casting De ≤ 50 mm, Rm ≥ 900 MPa
Released: 2008-06-30
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20/30410756 DC
BS EN 4860. Aerospace series. Environmental testing. Test Xb: Abrasion of markings, letterings, surfaces and materials caused by rubbing of fingertips and hands
BS EN 4860. Aerospace series. Environmental testing. Test Xb: Abrasion of markings, letterings, surfaces and materials caused by rubbing of fingertips and hands
Released: 2020-01-16
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BS EN 3482:2019
Aerospace series. Steel X8CrNiTi18-10 (1.4878/1.4544). Annealed. Reference heat treatment: softened. Forging stock. De ≤ 100 mm
Aerospace series. Steel X8CrNiTi18-10 (1.4878/1.4544). Annealed. Reference heat treatment: softened. Forging stock. De ≤ 100 mm
Released: 2019-12-04
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