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Titanium

Standards in development (59)

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Standard TitleStatus
British Standard BS EN 2178 - Aerospace series - Heat resisting alloy FE-PA2501 (X4NiCrMoTi43-13) - Solution treated and precipitated - Bar and section - De < 200 mmPublic Comment
BS 3TA 11:2009/Amd 1 Specification for bar and section for machining of titanium-aluminium -vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)Public Comment
BS EN 1424 Road marking materials - Premix glass beadsAccepted
BS EN 1424 Road marking materials - Premix glass beadsAccepted
BS EN 1436 Road marking materials - Road marking performance for road users and test methodsPublic Comment
BS EN 1463-1:2009+COR 1 Road marking materials - Retroreflecting road studs Part 1: Initial performance requirementsnull
BS EN 1871 Road marking materials - Physical propertiesApproval
BS EN 2033 Strips, cold rolled in steel - Thickness 0,1 mm <or= a <or= 2,5 mm - DimensionsApproval
BS EN 2161 Aerospace series - Heat resisting alloy CO-CH1401 (CoCr26Ni11W) - Not heat treated - Precision castingsPublic Comment
BS EN 2285 Bushes, plain, aluminium alloy, with self-lubricating liner - Dimensions and loadsTechnical Review
BS EN 2286 Bushes, flanged aluminium alloy, with self-lubricating liner - Dimensions and loadsTechnical Review
BS EN 2589 Steel - Sheet and strip, cold rolled - Thickness 0,1 mm <or= a <or= 3 mm - DimensionsApproval
BS EN 2590 Aerospace series - Steel - Sheets and plates, hot rolled - DimensionsApproval
BS EN 2811 Aerospace series - Nuts, hexagon, slotted/ castellated in steel cadmiumplated - Classification: 1 100 MPa/235 °CPublication
BS EN 2879 Aerospace series - Nuts, anchor, self-locking, air resistant, sealing, floating, two lug, with counterbore, in corrosion resisting steel, passivated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature) / 235°CPublication
BS EN 2959 Aerospace series - Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Solution treated and cold worked - Bar for forged fasteners - 3 mm < D < 30 mmPublic Comment
BS EN 3572 PTFE flexible hose assembly with convoluted inner tube and titanium 8 degrees 30 mn coupling - Product standardPublication
BS EN 3672 Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated, for 30° swage - Classification: 1 210 MPa (at ambient temperature)/730 °CPublication
BS EN 3875 Aerospace Series - Metallic Materials - Filler metal for brazing - T Technical SpecificationPublication
BS EN 3879 Aerospace series - Metallic materials - Filler metal for welding - Technical SpecificationPublic Comment
BS EN 3902 Washers for rivet assemblies, in aluminium alloy, anodized, metric seriesPublication
BS EN 3903 Washers, laminated, in corrosion resisting steelPublication
BS EN 3908 Aerospace series - Nipples, lubricating, axial type, in corrosionresisting steel, passivatedPublication
BS EN 4178 Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °CPublication
BS EN 4184 Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 45°, welded ends, doublePublic Comment
BS EN 4297 Aerospace series - Nuts, hexagon, self-locking by plastic ring, normal height, normal across flats, in corrosion resisting steel, passivated - Classification: 900 MPa (at ambient temperature) / 120 °CPublication
BS EN 4309 Nuts, hexagon, self-locking by plastic ring, normal height, normqal across flats, in alloy steel, cadmium plated-Classification: 900 MPa (at ambiant temperature) / 120°Publication
BS EN 4400-4 Aerospace series - Aluminium and aluminium- and magnesium- alloys - Technical specification Part 4:Aluminium and aluminium alloy tubePublic Comment
BS EN 4677-002 Aerospace series - Welded and brazed assemblies for aerospace constructions Electron beam welding machine Part 002 : Qualification specificationsPublic Comment
BS EN 4691-1 Aerospace series - Tie rod with integrated bolts Part 1: Technical specificationPublication
BS EN 4691-2 Aerospace series - Tie rod with integrated bolts Part 2: Overview construction kitPublication
BS EN 4692 Aerospace series - Tie Rod with integrated bolts - Locking clipPublication
BS EN 4693 Aerospace series - Tie rod with integrated bolts - Assembly code A, Band CPublication
BS EN 4694 Aerospace series - Tie rod with integrated bolts - Assembly code D, Eand FPublication
BS EN 4695 Aerospace series - Tie Rod with integrated bolts - Assembly Code G, Hand KPublication
BS EN 4801 Aerospace series - Flange couplings - Swivel flange with 3 fastening holes, in heat resisting steel - Inch seriesApproval
BS EN 4802 Aerospace series - Flange couplings - Swivel flange with 3 fastening holes, in nickel alloy - Inch seriesApproval
BS EN 4803 Aerospace series - Flange couplings - Swivel flange with 4 fastening holes, in heat resisting steel - Inch seriesApproval
BS EN 4804 Aerospace series - Flange couplings - Swivel flange with 4 fastening holes, in nickel alloy - Inch seriesApproval
BS EN 4805 Aerospace series - Flange couplings - Weld coupling, Straight, in heat resisting steel - Inch seriesApproval
BS EN 4806 Aerospace series - Flange couplings - Weld coupling, Straight, in nickel alloy - Inch seriesApproval
BS EN 4807 Aerospace series - Flange couplings - Weld coupling, 90° elbow, in heat resisting steel - Inch seriesApproval
BS EN 4808 Aerospace series - Flange couplings - Weld coupling, 90° elbow,in nickel alloy - Inch seriesApproval
BS EN 4809 Aerospace series - Flange couplings - Gasket seal with fluorocarbon seal on aluminium plate with 3 fastening holes, - Inch seriesApproval
BS EN 4810 Aerospace series - Flange couplings - Gasket seal with nickel alloy C seal on heat resisting steel plate with 3 fastening holes, - Inch seriesApproval
BS EN 4811 Aerospace series - Flange couplings - Gasket seal with fluorocarbon seal on aluminium plate with 4 fastening holes - Inch seriesApproval
BS EN 4812 Aerospace series - Flange couplings - Gasket seal with nickel alloy C seal on heat resisting steel plate with 4 fastening holes - Inch seriesApproval
BS EN 4813 Aerospace series - Flange couplings - Cap, in heat resisting steel - Inch seriesApproval
BS EN 4814 Aerospace series - Flange couplings up to 21 000 kPa - Technical specification - Inch seriesApproval
BS EN 4816 Aerospace series - Flange couplings - Gasket seal with nickel alloy C seal - Technical specification - Inch seriesApproval
BS EN 6029 Aerospace series - Rod-ends, adjustable, single fork with UNJ threaded shank min. engagement: 1,5 x thread diameter in corrosion resisting steel - Dimensions and loads - Inch seriesPublication
BS EN 6101 Aerospace series - Rivet, 100° medium flush head, close tolerance - Inch seriesPublication
BS EN 6105 Aerospace series - Stud with shoulderPublication
BS EN 6138 Aerospace series - Cap, protective, non metallic for fitting ends ? 3 000 PSI hydraulic systemsTechnical Review
BS ISO 15872 Aerospace - UNJ threads - GaugingPublic Comment
BS ISO 3203 Aerospace - Bolts, normal bihexagonal head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa - DimensionsPublic Comment
BS ISO 7481 Aerospace - Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C - Test methodsPublic Comment
BS SP 94:1964/Amd 3 Specification for bronze oil-retaining bushes and thrust washers - For aircraftApproval
PD CEN/TR 4541 Instruction for the installation of airframe bearingsPublic Comment

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Published standards (121)

Sort by: Reference | Title | Status

Standard referenceNameStatus
BS EN 4058:2001Aerospace series. Filler rods and filler wires for welding in titanium and titanium alloys. Diameter 0,5 mm = D = 5,0 mm. DimensionsCurrent
BS EN 2954-001:2010Aerospace series. Macrostructure of titanium and titanium alloy wrought products - General requirementsCurrent
BS EN 2954-002:2010Aerospace series. Macrostructure of titanium and titanium alloy wrought products - Macrostructure of bar, section, forging stock and forgingsCurrent
BS EN 4104:2001Aerospace series. Nickel base alloy NI-B40002. Filler metal for brazing. Powder or paste.Current
BS EN 2617:2001Aerospace Series. Plates in titanium and titanium alloys. Thickness 6 mm < a = 100 mm. DimensionsCurrent
BS EN 2955:1993Aerospace series. Recycling of titanium and titanium alloy scrapCurrent
BS EN 4267:2001Aerospace series. Round bar in titanium and titanium alloys. Diameter 6 mm = D = 160 mm. DimensionsCurrent
BS EN 2339:2001Aerospace series. Sheets, cold rolled in titanium and titanium alloys. Thickness 0,2 mm = a = 6 mm. DimensionsCurrent
BS EN 2338:2001Aerospace series. Sheets, hot rolled in titanium and titanium alloys. Thickness 0,8 mm = a = 6 mm. DimensionsCurrent
BS EN 3688:2001Aerospace series. T-ring fillers in titanium alloy for welded pipes. 14000 kPa nominal pressureCurrent
BS EN 3114-003:2006Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products - Microstructure of plateCurrent
BS EN 3114-004:2006Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products - Microstructure of sheet for superplastic formingCurrent
BS EN 3114-002:2007Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products - Microstructure of bars, sections, forging stock and forgingsCurrent
BS EN 3114-001:2006Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products - General requirementsCurrent
BS EN 3683:2007Aerospace series. Test methods. Titanium alloy wrought products. Determination of primary a content. Point count method and line intercept methodCurrent
BS EN 3684:2007Aerospace series. Test methods. Titanium alloy wrought products. Determination of ß transus temperature. Metallographic methodCurrent
BS EN 2003-009:2007Aerospace series. Test methods. Titanium and titanium alloys - Determination of surface contaminationCurrent
BS EN 3464:2012Aerospace series. Titanium alloy (Ti-6Al-4V). Annealed. Plate. 6 mm < a = 100 mmCurrent
BS EN 3351:2012Aerospace series. Titanium alloy Ti-4Al-4Mo-2Sn. Solution treated and aged. Forgings. De = 150 mmCurrent
BS EN 3312:2012Aerospace series. Titanium alloy Ti-6Al-4V. Annealed. Forgings De = 150 mmCurrent
BS EN 3354:2013Aerospace series. Titanium alloy Ti-6Al-4V. Annealed. Sheet for superplastic forming. a = 6 mmCurrent
BS EN 3965:2001Aerospace series. Titanium alloy TI-B17001. Filler metal for brazing. Rolled foilCurrent
BS EN 3459:2010Aerospace series. Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn). Solution treated and aged. Plate. 6 mm < a = 50 mmCurrent
BS EN 3464:2009Aerospace series. Titanium alloy TI-P64001 (Ti-6AI-4V). Annealed. Plate. 6 mm < a = 100 mWithdrawn
BS EN 3813:2013Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bar and wire for forged fasteners. De = 50 mmCurrent
BS EN 3311:2009Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bar for machining. D < 110 mmCurrent
BS EN 3355:2012Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Extruded section. De = 150 mm. 900 MPa = Rm = 1 160 MPaCurrent
BS EN 3456:2012Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Sheet and strip, hot rolled. a = 6 mmCurrent
BS EN 3310:2011Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Not heat treated. Forging stock, for annealed forgings. De = 360 mmCurrent
BS EN 3120:2012Aerospace series. Titanium alloy TI-P64003. Cold worked and stress relieved. Seamless tube for pressure systems. 4 mm = D = 51 mm. 690 MPa = Rm = 1 030 MPaCurrent
BS EN 3893:2001Aerospace series. Titanium alloy TI-W19001. Filler metal for weldingCurrent
BS EN 3892:2001Aerospace series. Titanium alloy TI-W64001. Filler metal for weldingCurrent
BS EN 3456:2009Aerospace series. Titanium alloy TIP64001 (Ti-6Al-4V). Annealed. Sheet and strip, hot rolled. a 3L 6 mmWithdrawn
BS EN 4800-007:2010Aerospace series. Titanium and titanium alloys - Remelting stockCurrent
BS EN 4800-008:2010Aerospace series. Titanium and titanium alloys. Technical specification - Pre-production and production castingsCurrent
BS EN 4800-005:2010Aerospace series. Titanium and titanium alloys. Technical specification - Forging stockCurrent
BS EN 4800-001:2010Aerospace series. Titanium and titanium alloys. Technical specification - Plate, sheet and stripCurrent
BS EN 4800-006:2010Aerospace series. Titanium and titanium alloys. Technical specification - Pre-production and production forgingsCurrent
BS EN 4800-002:2010Aerospace series. Titanium and titanium alloys. Technical specification - Bar and sectionCurrent
BS EN 4800-003:2010Aerospace series. Titanium and titanium alloys. Technical specification - TubeCurrent
BS EN 4800-004:2010Aerospace series. Titanium and titanium alloys. Technical specification - WireCurrent
BS EN 3976:2006Aerospace series. Titanium and titanium alloys. Test method. Chemical analysis for the determination of hydrogen contentCurrent
BS EN 2003-010:2007Aerospace series. Titanium and titanium alloys. Test methods - Sampling for determination of hydrogen contentCurrent
BS EN 4675:2011Aerospace series. Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe). Rm = 1 300 MPa. Bars. De < 110 mmCurrent
BS EN 4342:2001Aerospace series. Titanium TI-W99001. Filler metal for welding. Wire and rodCurrent
BS EN 4685:2011Aerospace series. Titanium Ti10V2Fe3Al. Bars. D < 110 mm. Rm = 1240 MPaCurrent, Work in Hand
BS 2TA 100:1973Procedure for inspection and testing of wrought titanium and titanium alloysWithdrawn
BS 3TA 100:2009Procedure for inspection, testing and acceptance of wrought titanium and titanium alloysCurrent
BS 2TA 3:1973Specification for bar and section for machining of commercially pure titanium (tensile strength 390-540 N/mm2)Withdrawn
BS 3TA 7:2009Specification for bar and section for machining of commercially pure titanium (tensile strength 540-740 MPa)Current
BS 2TA 7:1973Specification for bar and section for machining of commercially pure titanium (tensile strength 540-740 N/mm2)Withdrawn
BS 3TA 11:2009Specification for bar and section for machining of titanium-aluminium -vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)Current, Work in Hand
BS 2TA 49:2009Specification for bar and section for machining of titanium-aluminium- molybdenum-tin-silicon-carbon alloy (Tensile strength 1000-1200 MPa) (Limiting ruling section over 100 mm up to and including 150 mm)Current
BS TA 49:1973Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 N/mm2) (limiting ruling section over 100 mm up to and including 150 mm)Withdrawn
BS 2TA 46:2009Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 MPa) (limiting ruling section over 25 mm up to and including 100 mm)Current
BS TA 46:1973Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 N/mm2) (limiting ruling section over 25 mm up to and including 100 mm)Withdrawn
BS 2TA 45:2009Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1100-1280 MPa) (limiting ruling section 25 mm)Current
BS TA 45:1973Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1100-1280 N/mm2) (limiting ruling section 25 mm)Withdrawn
BS 2TA 11:1974Specification for bar and section for machining of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)Withdrawn
BS 2TA 22:1973Specification for bar and section for machining of titanium-copper alloy (tensile strength 540-770 N/mm2)Withdrawn
BS TA 53:1973Specification for bar and section for machining of titanium-copper alloy (tensile strength 650-880 N/mm2) (limiting ruling section 75 mm)Withdrawn
BS 2TA 40:2009Specification for bar for machining of titanium- aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm)Current
BS 2TA 38:2009Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon- carbon alloy (tensile strength 1250-1420 MPa) (limiting ruling section 25 mm)Current
BS TA 40:1971Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm2) (limiting ruling section over 25 mm up to and including 75 mm)Withdrawn
BS TA 38:1971Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 N/mm2) (limiting ruling section 25 mm)Withdrawn
BS 3TA 28:2009+A1:2015Specification for forging stock and wire of titanium-aluminium-vanadium alloy (tensile strength 1100-1300 MPa) (limiting ruling section 20 mm)Current
BS 2TA 28:1974Specification for forging stock and wire of titanium-aluminium-vanadium alloy (tensile strength 1100-1300 MPa) (limiting ruling section 20 mm) (primarily intended for the manufacture of fasteners complying with the requirements of the 'A' series of British Standards)Withdrawn
BS 2TA 4:1973Specification for forging stock of commercially pure titanium (tensile strength 390-540 N/mm2)Withdrawn
BS 2TA 8:1973Specification for forging stock of commercially pure titanium (tensile strength 540-740 N/mm2)Withdrawn
BS 2TA 50:2009Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 MPa) (limiting ruling section over 100 mm up to and including 150 mm)Current
BS 2TA 47:2009Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 MPa) (limiting ruling section 100 mm)Current
BS 2TA 41:2009Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm)Current
BS TA 50:1973Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 N/mm2) (limiting ruling section over 100 mm up to and including 150 mm)Withdrawn
BS TA 47:1973Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 N/mm2) (limiting ruling section 100 mm)Withdrawn
BS TA 41:1971Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm2) (limiting ruling section over 25 mm up to and including 75 mm)Withdrawn
BS 2TA 39:2009Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 MPa) (limiting ruling section 25 mm)Current
BS TA 39:1971Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 N/mm2) (limiting ruling section 25 mm)Withdrawn
BS 2TA 12:1974Specification for forging stock of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)Withdrawn
BS 3TA 12:2009Specification for forging stock of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)Withdrawn
BS TA 43:1972Specification for forging stock of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 N/mm2) (limiting ruling section 65 mm)Withdrawn
BS 2TA 23:1973Specification for forging stock of titanium-copper alloy (tensile strength 540-770 N/mm2)Withdrawn
BS TA 54:1973Specification for forging stock of titanium-copper alloy (tensile strength 650-880 N/mm2) (limiting ruling section 75 mm)Withdrawn
BS 2TA 5:1973Specification for forgings of commercially pure titanium (tensile strength 390-540 N/mm2)Withdrawn
BS 2TA 9:1973Specification for forgings of commercially pure titanium (tensile strength 540-740 N/mm2)Withdrawn
BS 2TA 51:2009Specification for forgings of titanium-aluminium- molybdenum-tin-silicon alloy (tensile strength 1000-1200 MPa) (limiting ruling section over 100 mm up to and including 150 mm)Withdrawn
BS 2TA 42:2009Specification for forgings of titanium-aluminium- molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm)Current
BS 2TA 48:2009Specification for forgings of titanium-aluminium-molybdenum- tin-silicon-carbon alloy (tensile strength 1050-1200 MPa) (limiting ruling section 100 mm)Withdrawn
BS TA 51:1973Specification for forgings of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 N/mm2) (limiting ruling section over 100 mm up to and including 150 mm)Withdrawn
BS TA 48:1973Specification for forgings of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1200 N/mm2) (limiting ruling section 100 mm)Withdrawn
BS TA 42:1971Specification for forgings of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm2) (limiting ruling section over 25 mm up to and including 75 mm)Withdrawn
BS 3TA 13:2009Specification for forgings of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)Withdrawn
BS 2TA 13:1974Specification for forgings of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)Withdrawn
BS TA 44:1972Specification for forgings of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 N/mm2) (limiting ruling section 65 mm)Withdrawn
BS 2TA 24:1973Specification for forgings of titanium-copper alloy (tensile strength 540-770 N/mm2)Withdrawn
BS TA 55:1973Specification for forgings of titanium-copper alloy (tensile strength 650-880 N/mm2) (limiting ruling section 75 mm)Withdrawn
BS TA 57:1974Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (maximum thickness 65 mm)Withdrawn
BS 2TA 57:2009Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (thickness over 50 mm up to and including 65 mm)Current
BS 2TA 56:2009Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)Current
BS TA 56:1974Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)Withdrawn
BS TA 58:1974Specification for plate of titanium-copper alloy (tensile strength 520-640 MPa) (maximum thickness 10 mm)Withdrawn
BS 2TA 58:2009Specification for plate of titanium-copper alloy (tensile strength 520-640 MPa) (maximum thickness 10 mm)Current
BS 2TA 1:1974Specification for sheet and strip of commercially pure titanium (tensile strength 290-420 MPa)Withdrawn
BS 3TA 1:2009Specification for sheet and strip of commercially pure titanium (tensile strength 290-420 MPa)Current
BS 3TA 2:2009Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 MPa)Current
BS 2TA 2:1973Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 N/mm2)Withdrawn
BS 3TA 6:2009Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 MPa)Current
BS 2TA 6:1973Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 N/mm2)Withdrawn
BS 2TA 52:2009Specification for sheet and strip of titanium- copper alloy (tensile strength 690-920 MPa)Current
BS TA 59:1980Specification for sheet and strip of titanium-aluminium-vanadium alloy (tensile strength 920 MPa to 1180 MPa)Withdrawn
BS 3TA 21:2009Specification for sheet and strip of titanium-copper alloy (tensile strength 540-700 MPa)Current
BS 2TA 21:1973Specification for sheet and strip of titanium-copper alloy (tensile strength 540-700 MPa)Withdrawn
BS TA 52:1973Specification for sheet and strip of titanium-copper alloy (tensile strength 690-920 N/mm2)Withdrawn
BS 2TA 59:2009Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 920-1180 MPa)Current
BS 3TA 10:2009Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 960-1270 MPa)Current
BS 2TA 10:1974Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 960-1270 MPa)Withdrawn
BS EN 2545-2:1995Titanium and titanium alloy remeling stock and castings. Technical specification - Remelting stockCurrent
BS EN 2545-1:1995Titanium and titanium alloy remelting stock and castings. Technical specification - General requirementsCurrent
BS EN 2545-3:1995Titanium and titanium alloy remelting stock and castings. Technical specification - Pre-production and production castingsCurrent
BS EN 2858-2:1994Titanium and titanium alloys. Forging stock and forgings. Technical specification. - Forging stockCurrent
BS EN 2858-1:1994Titanium and titanium alloys. Forging stock and forgings. Technical specifications - General requirementsCurrent
BS EN 2858-3:1994Titanium and titanium alloys. Forging stock and forgings. Technical specifications - Pre-production and production forgingsCurrent

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