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Engineering > Aircraft & space vehicle engineering > Aerospace construction materials > Titanium
Standards in development (52)
Published standards (121)
Proposed standard (1)ReferenceTitleASD STANDprEN 3308 Aerospace series — Bolts, normal hexagonal head, coarse tolerance normal shank, short thread, threaded to head, in titanium alloy, anodized,
MoS2 lubricated — Classification: 1 100 MPa (at ambient temperature) / 315 °CComment deadline: 7/31/2015[ back to top ]
Standards in development (52)Sort by: Title | StatusStandard 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 2SP 90:2008/Amd 1 Specification for corrosion-resisting steel split cotter pins foraircraft - Inch seriesnull BS 3A 117:1962+A2 Specification for corrosion-resisting steel pan head bolts (Unified threads) for aircraftPublic Comment
BS 3TA 28:2009/Amd 1 Specification for forging stock and wire of titanium-aluminium-vanadiumalloy (tensile strength 1100-1300 MPa) (limiting ruling section 20 mm)Public Comment
BS 4A 114:1999+A2 Specification for corrosion-resisting steel, mushroom-headed,slotted-drive, bolts, strength class 880 MPaPublic Comment
BS A 401 Machine Screws, Pan and 100° Countersunk Head, Hexalobular Recess,Unified Threads below .250 inch, Various materials, for AircraftPublic Comment
BS A31-54:1951/Amd 7 Specification for British Association (B.A.) low tensile screws and nutsfor aeronautical purposesIdea
BS EN 1424 Road marking materials - Premix glass beadsAccepted
BS EN 1463-1:2009+COR 1 Road marking materials - Retroreflecting road studs Part 1: Initial performance requirementsnull BS EN 1463-3 Road marking materials Part 3: Active road studsIdea
BS EN 1871 Road marking materials - Physical propertiesApproval
BS EN 2161 Aerospace series - Heat resisting alloy CO-CH1401 (CoCr26Ni11W) - Not heat treated - Precision castingsPublic Comment
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 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 4072 Aerospace series — Screws, 100 ° countersunk normal head, offset cruciform recess, close tolerance normal shank,short thread, in titanium alloy, aluminium IVD coated - Classification : 1100 Mpa (at ambient temperature) / 425°CApproval
BS EN 4073 Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1100 MPa (at ambient temperature) / 235 °CPublication
BS EN 4128 Bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in heat resisting nickel base alloy, aluminium IVD coated - Classification : 1250 MPa (at ambient temperature) / 425 °CApproval
BS EN 4138 Screws, pan head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification : 1100 MPa (at ambient temperature) / 235 °CApproval
BS EN 4162 Screws, 100 ° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1100 MPa (at ambient temperature) / 235 °CApproval
BS EN 4163 Screws, 100 ° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated - Classification : 1100 MPa (at ambient temperature) / 235°CApproval
BS EN 4376 Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) - Solution treated and precipitation treated - Bar and section - De <or= 200 mmPublication
BS EN 4377 Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) - Non heat treated - Forging stock - a or D <or= 300 mmPublication
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 4697 Aerospace series - General and Installation Requirements for Passenger Seat FittingsApproval
BS EN 4710-001 Aerospace series - Quick release fastening systems for non-structural applications Part 01: Technical specificationPublication
BS EN 4710-002 Aerospace series - Quick release fastening systems for non-structural applications Part 002: Spring clamp stud combinationPublication
BS EN 4710-003 Aerospace series - Quick release fastening systems for non-structural applications Part 003: Spring clampPublication
BS EN 4710-004 Aerospace series - Quick release fastening systems for non-structural applications Part 004: Spring clamp - One way tolerance compensationPublication
BS EN 4710-005 Aerospace series - Quick release fastening systems for non-structural applications Part 05: Spring clamp - Two ways tolerance compensationPublication
BS EN 4710-006 Aerospace series - Quick release fastening systems for non-structural applications Part 06: Stud - quick-release and lockingPublication
BS EN 4710-007 Aerospace series - Quick release fastening systems for non-structural applications Part 07: Retaining grommetPublication
BS EN 6094 Aerospace series - Washer, spring, countersunknull BS EN 6123 Fitting end, 24° internal cone, external thread, flareless type, size 04 up to 20, tube diameter 1/4 inch <= D <= 1 1/4Approval
BS EN STAN 8.4301 Aerospace series - Welded and brazed assemblies for aerospace constructi ons - Joints of metallic materials by electron beam welding - Quality ofwelded assembliesnull BS ISO 10959 Aerospace - MJ threads - GaugingPublic Comment
BS ISO 12260 Aerospace - Screws, pan head, internal offset cruciform ribbed or unribbed drive, stepped shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa - DimensionsPublic Comment
BS ISO 12261 Aerospace - Screws, pan head, internal offset cruciform ribbed or unribbed drive, 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 12289 Aerospace - Rivets, solid, in corrosion-resisting steel - Procurement specificationPublic Comment
BS ISO 16130 Aerospace series - Dynamic testing of the locking behaviour of bolted connections under transverse loading conditions (vibration test)Publication
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 3209 Aerospace - Nuts, anchor, self-locking, floating, two lug, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature )/235 degrees C, 1 100 MPa (at ambient temperature )/315 degrees C and 1 100 MPa (at ambient temperature)Public Comment
BS ISO 7481 Aerospace - Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C - Test methodsPublic Comment
BS ISO 8168 Aerospace - Bolts, with MJ threads, made of heat and corrosion resisting steel, strength class 1 100 MPa - Procurement specificationAccepted
BS ISO 9609 Aerospace - Nuts, hexagonal, plain, reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature) /120 degrees C, 450 MPa (at ambient temperature) /235 degrees C, 600 MPa (at ambient temperature) /425 degreesPublic Comment
BS ISO 9618 Aerospace - Nuts, hexagonal, slotted (castellated), reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/120 degrees C, 450 MPa (at ambient temperature)/235 degrees C, 600 MPa (at ambient temperaturePublic Comment
BS SP 33-39:1951+A5 Specifications for turnbarrels, tension rods and swaged cable-endconnections for aircraftPublication
BS SP 55 and 56:1953/AMD1 Specifications for double coil spring washers for aircraftIdea
BS SP 94:1964/Amd 3 Specification for bronze oil-retaining bushes and thrust washers - For aircraftnull PD CEN/TR 4541 Instruction for the installation of airframe bearingsPublic Comment[ back to top ]
Published standards (121)Sort by: Reference | Title | StatusStandard referenceNameStatusBS EN 4058:2001Aerospace series. Filler rods and filler wires for welding in titanium and titanium alloys. Diameter 0,5 mm = D = 5,0 mm. DimensionsCurrentBS EN 2954-002:2010Aerospace series. Macrostructure of titanium and titanium alloy wrought products - Macrostructure of bar, section, forging stock and forgingsCurrentBS EN 2954-001:2010Aerospace series. Macrostructure of titanium and titanium alloy wrought products - General requirementsCurrentBS EN 4104:2001Aerospace series. Nickel base alloy NI-B40002. Filler metal for brazing. Powder or paste.CurrentBS EN 2617:2001Aerospace Series. Plates in titanium and titanium alloys. Thickness 6 mm < a = 100 mm. DimensionsCurrentBS EN 2955:1993Aerospace series. Recycling of titanium and titanium alloy scrapCurrentBS EN 4267:2001Aerospace series. Round bar in titanium and titanium alloys. Diameter 6 mm = D = 160 mm. DimensionsCurrentBS EN 2339:2001Aerospace series. Sheets, cold rolled in titanium and titanium alloys. Thickness 0,2 mm = a = 6 mm. DimensionsCurrentBS EN 2338:2001Aerospace series. Sheets, hot rolled in titanium and titanium alloys. Thickness 0,8 mm = a = 6 mm. DimensionsCurrentBS EN 3688:2001Aerospace series. T-ring fillers in titanium alloy for welded pipes. 14000 kPa nominal pressureCurrentBS EN 3114-002:2007Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products - Microstructure of bars, sections, forging stock and forgingsCurrentBS EN 3114-001:2006Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products - General requirementsCurrentBS EN 3114-004:2006Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products - Microstructure of sheet for superplastic formingCurrentBS EN 3114-003:2006Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products - Microstructure of plateCurrentBS EN 3683:2007Aerospace series. Test methods. Titanium alloy wrought products. Determination of primary a content. Point count method and line intercept methodCurrentBS EN 3684:2007Aerospace series. Test methods. Titanium alloy wrought products. Determination of ß transus temperature. Metallographic methodCurrentBS EN 2003-009:2007Aerospace series. Test methods. Titanium and titanium alloys - Determination of surface contaminationCurrentBS EN 3464:2012Aerospace series. Titanium alloy (Ti-6Al-4V). Annealed. Plate. 6 mm < a = 100 mmCurrentBS EN 3351:2012Aerospace series. Titanium alloy Ti-4Al-4Mo-2Sn. Solution treated and aged. Forgings. De = 150 mmCurrentBS EN 3312:2012Aerospace series. Titanium alloy Ti-6Al-4V. Annealed. Forgings De = 150 mmCurrentBS EN 3354:2013Aerospace series. Titanium alloy Ti-6Al-4V. Annealed. Sheet for superplastic forming. a = 6 mmCurrentBS EN 3965:2001Aerospace series. Titanium alloy TI-B17001. Filler metal for brazing. Rolled foilCurrentBS EN 3459:2010Aerospace series. Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn). Solution treated and aged. Plate. 6 mm < a = 50 mmCurrentBS EN 3464:2009Aerospace series. Titanium alloy TI-P64001 (Ti-6AI-4V). Annealed. Plate. 6 mm < a = 100 mWithdrawnBS EN 3813:2013Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bar and wire for forged fasteners. De = 50 mmCurrentBS EN 3311:2009Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bar for machining. D < 110 mmCurrentBS EN 3355:2012Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Extruded section. De = 150 mm. 900 MPa = Rm = 1 160 MPaCurrentBS EN 3456:2012Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Sheet and strip, hot rolled. a = 6 mmCurrentBS EN 3310:2011Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Not heat treated. Forging stock, for annealed forgings. De = 360 mmCurrentBS 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 MPaCurrentBS EN 3893:2001Aerospace series. Titanium alloy TI-W19001. Filler metal for weldingCurrentBS EN 3892:2001Aerospace series. Titanium alloy TI-W64001. Filler metal for weldingCurrentBS EN 3456:2009Aerospace series. Titanium alloy TIP64001 (Ti-6Al-4V). Annealed. Sheet and strip, hot rolled. a 3L 6 mmWithdrawnBS EN 4800-007:2010Aerospace series. Titanium and titanium alloys - Remelting stockCurrentBS EN 4800-008:2010Aerospace series. Titanium and titanium alloys. Technical specification - Pre-production and production castingsCurrentBS EN 4800-003:2010Aerospace series. Titanium and titanium alloys. Technical specification - TubeCurrentBS EN 4800-004:2010Aerospace series. Titanium and titanium alloys. Technical specification - WireCurrentBS EN 4800-002:2010Aerospace series. Titanium and titanium alloys. Technical specification - Bar and sectionCurrentBS EN 4800-005:2010Aerospace series. Titanium and titanium alloys. Technical specification - Forging stockCurrentBS EN 4800-006:2010Aerospace series. Titanium and titanium alloys. Technical specification - Pre-production and production forgingsCurrentBS EN 4800-001:2010Aerospace series. Titanium and titanium alloys. Technical specification - Plate, sheet and stripCurrentBS EN 3976:2006Aerospace series. Titanium and titanium alloys. Test method. Chemical analysis for the determination of hydrogen contentCurrentBS EN 2003-010:2007Aerospace series. Titanium and titanium alloys. Test methods - Sampling for determination of hydrogen contentCurrentBS EN 4675:2011Aerospace series. Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe). Rm = 1300 MPa. Bars. De < 110 mmCurrentBS EN 4342:2001Aerospace series. Titanium TI-W99001. Filler metal for welding. Wire and rodCurrentBS EN 4685:2011Aerospace series. Titanium Ti10V2Fe3Al. Bars. D < 110 mm. Rm = 1240 MPaCurrent, Work in HandBS 2TA 100:1973Procedure for inspection and testing of wrought titanium and titanium alloysWithdrawnBS 3TA 100:2009Procedure for inspection, testing and acceptance of wrought titanium and titanium alloysCurrentBS 2TA 3:1973Specification for bar and section for machining of commercially pure titanium (tensile strength 390-540 N/mm2)WithdrawnBS 3TA 7:2009Specification for bar and section for machining of commercially pure titanium (tensile strength 540-740 MPa)CurrentBS 2TA 7:1973Specification for bar and section for machining of commercially pure titanium (tensile strength 540-740 N/mm2)WithdrawnBS 3TA 11:2009Specification for bar and section for machining of titanium-aluminium -vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)CurrentBS 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)CurrentBS 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)WithdrawnBS 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)CurrentBS 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)WithdrawnBS 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)CurrentBS 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)WithdrawnBS 2TA 11:1974Specification for bar and section for machining of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)WithdrawnBS 2TA 22:1973Specification for bar and section for machining of titanium-copper alloy (tensile strength 540-770 N/mm2)WithdrawnBS TA 53:1973Specification for bar and section for machining of titanium-copper alloy (tensile strength 650-880 N/mm2) (limiting ruling section 75 mm)WithdrawnBS 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)CurrentBS 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)CurrentBS 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)WithdrawnBS 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)WithdrawnBS 3TA 28:2009Specification for forging stock and wire of titanium-aluminium-vanadium alloy (tensile strength 1100-1300 MPa) (limiting ruling section 20 mm)Current, Work in HandBS 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)WithdrawnBS 2TA 4:1973Specification for forging stock of commercially pure titanium (tensile strength 390-540 N/mm2)WithdrawnBS 2TA 8:1973Specification for forging stock of commercially pure titanium (tensile strength 540-740 N/mm2)WithdrawnBS 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)CurrentBS 2TA 47:2009Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 MPa) (limiting ruling section 100 mm)CurrentBS 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)CurrentBS 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)WithdrawnBS TA 47:1973Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 N/mm2) (limiting ruling section 100 mm)WithdrawnBS 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)WithdrawnBS 2TA 39:2009Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 MPa) (limiting ruling section 25 mm)CurrentBS 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)WithdrawnBS 2TA 12:1974Specification for forging stock of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)WithdrawnBS 3TA 12:2009Specification for forging stock of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)WithdrawnBS TA 43:1972Specification for forging stock of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 N/mm2) (limiting ruling section 65 mm)WithdrawnBS 2TA 23:1973Specification for forging stock of titanium-copper alloy (tensile strength 540-770 N/mm2)WithdrawnBS TA 54:1973Specification for forging stock of titanium-copper alloy (tensile strength 650-880 N/mm2) (limiting ruling section 75 mm)WithdrawnBS 2TA 5:1973Specification for forgings of commercially pure titanium (tensile strength 390-540 N/mm2)WithdrawnBS 2TA 9:1973Specification for forgings of commercially pure titanium (tensile strength 540-740 N/mm2)WithdrawnBS 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)WithdrawnBS 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)CurrentBS 2TA 48:2009Specification for forgings of titanium-aluminium-molybdenum- tin-silicon-carbon alloy (tensile strength 1050-1200 MPa) (limiting ruling section 100 mm)WithdrawnBS 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)WithdrawnBS TA 48:1973Specification for forgings of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1200 N/mm2) (limiting ruling section 100 mm)WithdrawnBS 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)WithdrawnBS 2TA 13:1974Specification for forgings of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)WithdrawnBS 3TA 13:2009Specification for forgings of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)WithdrawnBS TA 44:1972Specification for forgings of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 N/mm2) (limiting ruling section 65 mm)WithdrawnBS 2TA 24:1973Specification for forgings of titanium-copper alloy (tensile strength 540-770 N/mm2)WithdrawnBS TA 55:1973Specification for forgings of titanium-copper alloy (tensile strength 650-880 N/mm2) (limiting ruling section 75 mm)WithdrawnBS TA 57:1974Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (maximum thickness 65 mm)WithdrawnBS 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)CurrentBS 2TA 56:2009Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)CurrentBS TA 56:1974Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)WithdrawnBS TA 58:1974Specification for plate of titanium-copper alloy (tensile strength 520-640 MPa) (maximum thickness 10 mm)WithdrawnBS 2TA 58:2009Specification for plate of titanium-copper alloy (tensile strength 520-640 MPa) (maximum thickness 10 mm)CurrentBS 2TA 1:1974Specification for sheet and strip of commercially pure titanium (tensile strength 290-420 MPa)WithdrawnBS 3TA 1:2009Specification for sheet and strip of commercially pure titanium (tensile strength 290-420 MPa)CurrentBS 3TA 2:2009Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 MPa)CurrentBS 2TA 2:1973Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 N/mm2)WithdrawnBS 3TA 6:2009Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 MPa)CurrentBS 2TA 6:1973Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 N/mm2)WithdrawnBS 2TA 52:2009Specification for sheet and strip of titanium- copper alloy (tensile strength 690-920 MPa)CurrentBS TA 59:1980Specification for sheet and strip of titanium-aluminium-vanadium alloy (tensile strength 920 MPa to 1180 MPa)WithdrawnBS 2TA 21:1973Specification for sheet and strip of titanium-copper alloy (tensile strength 540-700 MPa)WithdrawnBS 3TA 21:2009Specification for sheet and strip of titanium-copper alloy (tensile strength 540-700 MPa)CurrentBS TA 52:1973Specification for sheet and strip of titanium-copper alloy (tensile strength 690-920 N/mm2)WithdrawnBS 2TA 59:2009Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 920-1180 MPa)CurrentBS 3TA 10:2009Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 960-1270 MPa)CurrentBS 2TA 10:1974Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 960-1270 MPa)WithdrawnBS EN 2545-2:1995Titanium and titanium alloy remeling stock and castings. Technical specification - Remelting stockCurrentBS EN 2545-1:1995Titanium and titanium alloy remelting stock and castings. Technical specification - General requirementsCurrentBS EN 2545-3:1995Titanium and titanium alloy remelting stock and castings. Technical specification - Pre-production and production castingsCurrentBS EN 2858-2:1994Titanium and titanium alloys. Forging stock and forgings. Technical specification. - Forging stockCurrentBS EN 2858-3:1994Titanium and titanium alloys. Forging stock and forgings. Technical specifications - Pre-production and production forgingsCurrentBS EN 2858-1:1994Titanium and titanium alloys. Forging stock and forgings. Technical specifications - General requirementsCurrent[ back to top ]
Committees (5)Sort by: Reference | NameCommittee ReferenceTitleACE/12Aerospace fasteners and fastening systemsACE/61/-/48Heat Resisting Alloys for Aerospace PurposesB/509/2Horizontal road markings and road studsACE/61Metallic materials for aerospace purposesACE/61/-/49Titanium and its Alloys for Aerospace Purposes[ back to top ]