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Standards in development (108)

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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
British Standard BS EN 7000-4 Aerospace series - Non-metallic materials - Rules for the drafting and presentation of material standards Part 4. Plastic transparenciesPublic Comment
BS 2SP 68 to 2SP 71 Specification for 100° countersunk precision head aluminium and aluminium alloy rivetsApproval
BS 2SP 77 to 2SP 80+A4 Specification for snap head aluminium and aluminium alloy rivetsApproval
BS 2SP 81 and 2SP 82+A3 Specification for snap head high nickel-copper alloy rivetsApproval
BS 2SP 87 and 2SP 88+A1 Specification for 100° countersunk head high nickel-copper alloy rivetsApproval
BS 2SP 91 to 92+A4 Specification for carbon steel worm drive clamps for aircraftApproval
BS 2X35:2003+A1 Selectively rentovable interntediate coating for aerospace purposesnull
BS 3A 117:1962+A1 Specification for corrosion-resisting steel pan head bolts (Unified threads) for aircraftApproval
BS 3S 98 Specification for 2.5 % nickel-chromium -molybdenum (high carbon) steelbillets, bars, forging and parts 1160-1310 MPa: limiting rulingsection.Accepted
BS 5X 17:1998+A1 Specification for oleoresinous varnish for aerospace purposesnull
BS A 401 Machine Screws, Pan and 100° Countersunk Head, Hexalobular Recess,Unified Threads below .250 inch, Various materials, for AircraftIdea
BS EN 2155-20 - Aerospace series - Test methods for transparent materials for aircraft glazing Part 20. Determination of retention of strength after crazing for as-cast acrylicsAccepted
BS EN 2155-22 - Aerospace series Test methods for transparent materials for aircraft glazing Part 22. Determination of thermal relaxation of stretched acrylic sheetAccepted
BS EN 2161 Aerospace series - Heat resisting alloy CO-CH1401 (CoCr26Ni11W) - Not heat treated - Precision castingsPublic Comment
BS EN 2263 Polymethyl methacrylate (as cast) sheets for aircraft glazing.Accepted
BS EN 2284 Aerospace series Sulfuric acid anodising of aluminium and wrought aluminium alloysIdea
BS EN 2342 Aerospace series. Heat and crazing resistant acrylic sheet for aircraft glazing.Accepted
BS EN 2512 Aerospace Series - Aluminium alloy AL-P7175 - T7351 - Plate - 6 mm < a <or= 100 mmPublication
BS EN 2633 Aerospace series - Aluminium alloy AL-P2024- - T3511 - Extruded bars and sections - 1,2 mm ? De ? 160 mm with peripheral coarse grain controlPublication
BS EN 2704 Aerospace series - Aluminium alloy AL-P2024 - T3511 - Drawn bar - De ? 75 mmPublication
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 3105 Aerospace series Sealants Test methods Determination of the corrosive effect of sealants on metallic materialsAccepted
BS EN 3110 Aerospace series. Sealants. Method of manufacture of moulded plates.Idea
BS EN 3631 Aerospace series - Fluid fittings, flanged, 90° elbowed - Sealing by O-ring for 0,8 mm thick tubesPublication
BS EN 3635 Aerospace series - Weld lip - Geometrical configurationPublication
BS EN 3825 Aerospace series - Fluorosilicone rubber (FVMQ) - Hardness 60 IRHDPublication
BS EN 3826 Aerospace series - Fluorosilicone rubber (FVMQ) - Hardness 70 IRHDPublication
BS EN 3827 Aerospace series - Fluorosilicone rubber (FVMQ) - Hardness 80 IRHDPublication
BS EN 3875 Aerospace Series - Metallic Materials - Filler metal for brazing - T Technical SpecificationApproval
BS EN 3879 Aerospace series - Metallic materials - Filler metal for welding - Technical SpecificationPublic Comment
BS EN 3982 Aerospace series - Aluminium alloy AL-P7050- T7451 - Plate - 6 mm < a <or= 160 mmApproval
BS EN 3997 Aerospace series - Aluminium alloy AL-P2024-T3 - Sheet and strip 0,4 mm < a < 6 mmPublication
BS EN 4107 Aerospace series Non-metallic materials Structural adhesive systems Foaming adhesives Technical specificationAccepted
BS EN 4121 Aerospace series - Shank nuts, serrated, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1 100 MPa (at ambient temperature) / 650 °CApproval
BS EN 4184 Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 45°, welded ends, doublePublic Comment
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 mmApproval
BS EN 4400-4 Aerospace series - Aluminium and aluminium- and magnesium- alloys - Technical specification Part 4:Aluminium and aluminium alloy tubePublic Comment
BS EN 4400-9 Aerospace series Aluminium and magnesium alloy castings Technical specification Part 9: Pre-production and production castings Part 9: Pre-production and production castingsnull
BS EN 4440 Aerospace series Rubber panels and calendered sheets DimensionsAccepted
BS EN 4478 Aerospace series - Sealing compounds, two-component polysulphide-polymer base suitable for blow gun or spatula application for temperatures from -55 ?C to 120 ?C - PropertiesIdea
BS EN 4479 Aerospace series -Sealing compounds, two-component polysulphide-polymer base suitable forblow gun, spatula or roll application for temperatures from -55 ?C to 120 ?C - PropertiesIdea
BS EN 4480 Aerospace series -Sealing compounds, two component polysulphide-polymer base suitable forbrush application for temperatures from -55 ?C to 135 ?C - PropertiesIdea
BS EN 4481 Aerospace series -Sealing compounds, two component polysulphide-polymer base suitable forblow gun or spatula application for temperatures from -55 ?C to 135 ?C - PropertiesIdea
BS EN 4482 Aerospace series -Sealing compounds, two component polysulphide-polymer base suitable forblow gun, spatula or roll application for temperatures from -55 ?C to 135 ?C - PropertiesIdea
BS EN 4485 Aerospace series - Sealing compounds, two component polysulphide-polymer base suitable for blow gun, spatula or roll application for temperatures from -55 °C to 95 °C corrosion inhibiting - PropertiesIdea
BS EN 4548 Aerospace series - Structural adhesive system - Adhesive film / Anticorrosion primer - Epoxy based - For continuous use up to 120 °CIdea
BS EN 4677-002 Aerospace series - Welded and brazed assemblies for aerospace constructions Electron beam welding machine Part 002 : Qualification specificationsPublic Comment
BS EN 4723 Aerospace series - Standardized measurement methods for comfort and living space criteria for aircraft passenger seatsPublic Comment
BS EN 4725 Aerospace series - Aluminium alloy AL-P2024 - Al Cu4Mg1 - T351 - Plate - 6 mm < a ? 150 mmPublication
BS EN 4726 Aerospace series — Acceptance of the cosmetic variations in appearanceof aircraft cabin partsPublic Comment
BS EN 4727 Aerospace series — Standardized passenger seat weight informationnull
BS EN 4826 Aerospace series - Zinc-nickel (12/16% Ni) plating of steels with specified tensile strength ? 1 450 MPa, copper, copper alloys and nickel alloys and aluminium alloys for parts and fastenersPublication
BS EN 6031 Fibre reinforced plastics - Test methods - Determination of in-plane shear properties (+/- 45° tensile test)Publication
BS EN 6032 Aerospace series - Fibre reinforced plastics - Test method - Determination of the glass transition temperaturesApproval
BS EN 6033 Aerospace series - Carbon fibre reinforced plastics - Test method - Determination of interlaminar fracture toughness energy - Mode I GicApproval
BS EN 6034 Aerospace series - Carbon fibre reinforced plastics - Test method - Determination of interlaminar fracture toughness energy - Mode II GiicApproval
BS EN 6035 Aerospace series - Fibre reinforced plastics - Test method - Determination of notched and unnotched tensile strengthPublication
BS EN 6036 Aerospace series - Fibre reinforced plastics - Test method - Determination of notched, unnotched and filled hole compression strengthApproval
BS EN 6037 Fibre reinforced plastics - Test method - Determination of bearing strengthPublication
BS EN 6038 Fibre reinforced plastics - Test method - Determination of the compression strength after impactPublication
BS EN 6094 Aerospace series - Washer, spring, countersunknull
BS EN 7000-5 Aerospace series - Non-metallic materials - Rules for the drafting and presentation of material standards Part 5. Glass transparenciesPublic Comment
BS EN 8.5031 Aerospace series - Non-metallic materials - Cast acrylic sheet - High moisture absorption - Propertiesnull
BS EN 8.5032 Aerospace series - Non-metallic materials - Heat and crazing resistant cast acrylic, crosslinked and high moisture absorption - Propertiesnull
BS EN 8.5033 Aerospace series - Non-metallic materials - Heat and crazing resistant cast acrylic, crosslinked, multiaxially stretched, and high moisture absorption - Propertiesnull
BS EN 8.5034 Aerospace series - Non-metallic materials - Impact resistant flame retardent polyphenol sulphone (PPSU) sheets - Propertiesnull
BS EN 9101 Quality Management Systems - Audit Requirements for Aviation, Space, and Defence OrganisationsPublic Comment
BS EN 9102 Aerospace First Article Inspection RequirementsPublic Comment
BS EN 9103 Aerospace series - Quality management systems - Variation management of key characteristicsPublic Comment
BS EN 9104-002 Aerospace series - Quality management systems Part 002: Requirements for Oversight of Aerospace Quality Management System Certification/Registrations ProgramsPublic Comment
BS EN 9110 Quality Management Systems - Requirements for Aviation Maintenance OrganizationsPublication
BS EN 9114 Direct Ship Guidance for Aerospace CompaniesPublication
BS EN 9116 Aerospace Series – Notice of Change (NOC) RequirementsPublic Comment
BS EN 9117 Aerospace Series - Delegated Product Release VerificationPublic Comment
BS EN 9131 Aerospace Series Quality Management Systems Nonconformance Data Definition and DocumentationPublic Comment
BS EN 9132 Aerospace series - Data Matrix Quality Requirements for Parts MarkingPublic Comment
BS EN 9133 Aerospace Series – Qualification Procedure for Aerospace StandardProductsPublic Comment
BS EN 9136 Aerospace Series – Root Cause Analysis and Problem Solving (9S Methodology)Public Comment
BS EN 9139 Aerospace Series - Quality Management Systems - Development of Process-Based Bodies of KnowledgePublic Comment
BS EN 9239 Aerospace Series - Programme Management - Guide for the Risk ManagementPublic Comment
BS EN 9277 Aerospace series - Programme management - Guide for the management of Systems EngineeringApproval
BS EN 9300-002 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 002: RequirementsPublic Comment
BS EN 9300-005 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 005: Authentication and VerificationPublic Comment
BS EN 9300-007 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 007: Terms and ReferencesPublic Comment
BS EN 9300-010 Aerospace series - LOTAR - LOng Term Archiving and Retrieval of digital technical product documentation such as 3D, CAD and PDM data. PART 010: Overview Data FlowApproval
BS EN 9300-015 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 115: explicit CAD assembly structurePublic Comment
BS EN 9300-100 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 100: Common concepts for Long term archiving and retrieval of CAD 3D mechanical informationPublic Comment
BS EN 9300-110 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 110: CAD mechanical 3D Explicit geometry informationPublic Comment
BS EN 9300-120 Aerospace series - LOTAR - LOng Term Archiving and Retrieval of digital technical product documentation such as 3D, CAD and PDM data Part 120: CAD 3D explicit geometry with product and manufacturing informationPublic Comment
BS EN 9320 Aerospace series — Programme Management — General guidelines for acquisition and supply of open systemsPublication
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)Public 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 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 55 and 56:1953/AMD1 Specifications for double coil spring washers for aircraftnull
BS X 38:2005+A1 purposes - Specificationnull
BSEN9300-1 Long Term Archiving and Retrieval of digital technical productdocumentat ion such as 3D, CAD and PDM data within the aerospaceindustry Part 1 StructurePublic Comment
BSEN9300-2 Long Term Archiving and Retrieval of digital technical productdocumentat ion such as 3D, CAD and PDM data within the aerospaceindustry Part 2 RequirementsPublic Comment
BSEN9300-4 Long Term Archiving and Retrieval of digital technical productdocumentat ion such as 3D, CAD and PDM data within the aerospaceindustry Part 4 Description MethodsPublic Comment
PD CEN/TR 4541 Instruction for the installation of airframe bearingsPublic Comment

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Published standards (141)

Sort by: Reference | Title | Status

Standard referenceNameStatus
BS EN 2826:2011Aerospace series. Burning behaviour of non metallic materials under the influence of radiating heat and flames. Determination of gas components in the smokeCurrent
BS EN 2825:2011Aerospace series. Burning behaviour of non metallic materials under the influence of radiating heat and flames. Determination of smoke densityCurrent
BS EN 2824:2011Aerospace series. Burning behaviour of non-metallic materials under the influence of radiating heat and flames. Determination of smoke density and gas components in the smoke of materials. Test equipment apparatus and mediaCurrent
BS EN 3844-2:2011Aerospace series. Flammability of non metallic materials - Small burner test, horizontal. Determination of the horizontal flame propagation Current
BS EN 4327:2001Aerospace series. Heat resisting alloy CO-WH1401 (CoCr26Ni11W8). Filler metal for welding. Wire and rodCurrent
BS EN 4383:2006Aerospace series. Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3). Non heat treated. Remelting stockCurrent
BS EN 3671:2007Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb). Non heat treated. Forging stock. a or D = 250 mmCurrent
BS EN 4382:2006Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb). Solution treated. Seamless tubes. For hydraulic application. D = 50 mm, a = 3 mmCurrent
BS EN 3866:2013Aerospace series. Non-metallic materials. Glass tranparencies. Test methods. Determination of ream and surface rippleCurrent
BS EN 3862:2013Aerospace series. Non-metallic materials. Glass transparencies. Material standard. Chemically tempered soda lime float glassCurrent
BS EN 3861:2013Aerospace series. Non-metallic materials. Glass transparencies. Material standard. Thermally tempered soda lime float glassCurrent
BS EN 3863:2013Aerospace series. Non-metallic materials. Glass transparencies. Test methods. Determination of flatnessCurrent
BS EN 3864:2013Aerospace series. Non-metallic materials. Glass transparencies. Test methods. Determination of modulus of ruptureCurrent
BS EN 3102:2013Aerospace series. Sealants. Test methods. Determination of low-temperature flexibilityCurrent
BS EN 4700-007:2010Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification - Remelting stockCurrent
BS EN 2076-1:1991Aluminium and magnesium alloy ingots and castings. Technical specification - General requirementsCurrent
BS EN 2076-2:1991Aluminium and magnesium alloy ingots and castings. Technical specification - Ingots for remeltingCurrent
BS EN 2076-3:1991Aluminium and magnesium alloy ingots and castings. Technical specification - Pre-production and production castingsCurrent
BS 2B 27:2002Copper-zinc-aluminium-nickel-silicon alloy tubeWithdrawn
BS EN 3947:1998Nickel base alloy NI-B15701 (NiPd34Au30). Filler metal for brazing. Rolled foilCurrent
BS EN 3948:1998Nickel base alloy NI-B15701 (NiPd34Au30). Filler metal for brazing. WireCurrent
BS EN 3931:1998Nickel base alloy NI-B31001 (NiCr19Si10). Filler metal for brazing. TapeCurrent
BS EN 3928:1998Nickel base alloy NI-B40001 (NiSi5B3). Filler metal for brazing. TapeCurrent
BS EN 4105:1998Nickel base alloy NI-B40002 (NiSi4B2). Filler metal for brazing. TapeCurrent
BS EN 3917:1998Nickel base alloy NI-B41201 (NiCr14Si5B3C). Filler metal for brazing. Powder or pasteCurrent
BS EN 3918:1998Nickel base alloy NI-B41201 (NiCr14Si5B3C). Filler metal for brazing. TapeCurrent
BS EN 3919:1998Nickel base alloy NI-B41202 (NiCr14Si5B3). Filler metal for brazing. Amorphous foilCurrent
BS EN 3922:1998Nickel base alloy NI-B41203 (NiCr7Si5B3). Filler metal for brazing. Borided foilCurrent
BS EN 3924:1998Nickel base alloy NI-B41203 (NiCr7Si5B3). Filler metal for brazing. TapeCurrent
BS EN 3944:1998Nickel base alloy NI-B41204 (NiCr13Si4B3). Filler metal for brazing. TapeCurrent
BS EN 3940:1998Nickel base alloy NI-B46001 (NiCo20Si5B3). Filler metal for brazing. TapeCurrent
BS HR 506:1989Nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy wire: softened (nickel base, Cr 19.5, Co 18, Ti 2.5, Al 1.5)Withdrawn
BS HR 205:1989Nickel-copper alloy sheet and strip: annealed (Nickel base, Cu 31)Withdrawn
BS 2L 500:1973Procedure for inspection and testing of wrought magnesium-base alloysWithdrawn
BS B 100:1992Procedure for inspection, testing and acceptance of wrought copper alloysWithdrawn
BS 2B 100:2009Procedure for inspection, testing and acceptance of wrought copper alloysCurrent
BS 3L 500:2011Procedure for inspection, testing and acceptance of wrought magnesium base alloysCurrent
BS 3V 4:1929Specification for aircraft material. AshWithdrawn
BS 6V 3:1943Specification for aircraft material. High strength plywood for aircraftWithdrawn
BS 2B 8:1930Specification for aircraft material. Phosphor bronze castings for bearings (including solid and cored sticks)Withdrawn
BS 2B 21:1933Specification for aircraft material. White metal (88/8/4) ingots (suitable for bearings)Withdrawn
BS 2L 508:1973Specification for bars and extruded sections of magnesium-1¼% zinc-zirconium alloy (suitable for welding by inert-gas shielded arc techniques) (not exceeding 50 mm diameter or minor sectional dimension) (Zn 1.25, Zr 0.6)Withdrawn
BS 2L 505:1973Specification for bars and extruded sections of magnesium-3% zinc-zirconium alloy (not exceeding 100 mm diameter or minor sectional dimension) (Zn 3.0, Zr 0.6)Withdrawn
BS L 512:1973Specification for bars and extruded sections of magnesium-6% aluminium-zinc alloy (not exceeding 150 mm diameter or minor sectional dimension) (Al 6.0, Zn 1.0)Withdrawn
BS HC 301:1973Specification for cobalt base chromium-nickel-tungsten alloy castings (Cr 25.5, Ni 10.5. W 7.5)Current
BS 2HR 40:2010Specification for cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy billets, bars and forgings (cobalt base Cr 20, W 15, Ni 10, Mn 1.5)Current
BS HR 40:1972Specification for cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy billets, bars and forgings (cobalt base, Cr 20, W 15, Ni 10, Mn 1.5)Withdrawn
BS HR 240:1972Specification for cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy plate, sheet and strip (cobalt base Cr 20, W 15, Ni 10, Mn 1.5)Withdrawn
BS 2HR 240:2011Specification for cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy plate, sheet and strip (Cobalt base, Cr 20, W 15, Ni 10, Mn 1.5)Current
BS HC 502:1981Specification for copper base aluminium-nickel-iron alloy castings (620 MPa) (Al 9.5, Ni 5, Fe 5)Current
BS 2B 23:2009Specification for copper-aluminium-nickel-iron alloy rods, bars, sections, forging stock and forgingsCurrent
BS B 23:1991Specification for copper-aluminium-nickel-iron alloy rods, sections, forging stock and forgingsWithdrawn
BS B 32:1991Specification for copper-beryllium alloy rods, sections and parts (solution treated (W) and precipitated)Withdrawn
BS B 28:1991Specification for copper-beryllium alloy strip, foil and parts (solution treated (W) and precipitated)Withdrawn
BS B 31:1991Specification for copper-beryllium alloy strip, foil and parts (solution treated, cold rolled: full hard (W(H)) and precipitated)Withdrawn
BS B 30:1991Specification for copper-beryllium alloy strip, foil and parts (solution treated, cold rolled: half hard (W(1/2H)) and precipitated)Withdrawn
BS B 29:1991Specification for copper-beryllium alloy strip, foil and parts (solution treated, cold rolled: quarter hard (W(1/4H)) and precipitated)Withdrawn
BS B 33:1991Specification for copper-beryllium alloy wire and springs (solution treated (W) and precipitated)Withdrawn
BS B 26:1991Specification for copper-nickel-silicon alloy rods and sections (cold worked and heat treated)Withdrawn
BS B 25:1991Specification for copper-nickel-silicon alloy rods, sections, forging stock and forgings (heat treated)Withdrawn
BS 2B 24:2009Specification for copper-tin-phosphorous alloy rods and sectionsCurrent
BS B 24:1991Specification for copper-tin-phosphorous alloy rods and sectionsWithdrawn
BS 3B 27:2009Specification for copper-zinc-aluminium-nickel-silicon alloy tubeCurrent
BS B 27:1991Specification for copper-zinc-aluminium-nickel-silicon alloy tubeWithdrawn
BS L 514:1973Specification for forging stock and forgings of magnesium-3% zinc-zirconium alloy (Zn 3.0, Zr 0.6)Withdrawn
BS L 513:1973Specification for forging stock and forgings of magnesium-6% aluminium-zinc alloy (Al 6.0, Zn 1.0)Current
BS 3L 125:1970Specification for ingots and castings of magnesium - 10% aluminium-zinc-manganese alloy (solution treated and precipitation treated) (Al 10, Zn 0.5, Mn 0.3)Withdrawn
BS 3L 124:1970Specification for ingots and castings of magnesium - 10% aluminium-zinc-manganese alloy (solution treated) (Al 10, Zn 0.5, Mn 0.3)Withdrawn
BS 3L 122:1970Specification for ingots and castings of magnesium-8% aluminium-zinc-manganese alloy (solution treated) (Al 8, Zn 0.5, Mn 0.3)Current
BS 2L 126:1970Specification for ingots and castings of magnesium-cerium-zinc-zirconium alloy (precipitation treated) (rare earth metals 3.0, Zn 2.3, Zr 0.6)Current
BS 2L 128:1970Specification for ingots and castings of magnesium-zinc-cerium-zirconium alloy (precipitation treated) (Zn 4.5, rare earth metals 1.2, Zr 0.7)Current
BS 2L 127:1970Specification for ingots and castings of magnesium-zinc-zirconium alloy (precipitation treated) (Zn 4.5, Zr 0.7)Withdrawn
BS 2HC 209:1989Specification for low carbon, precipitation hardening nickel-chromium-aluminium-molybdenum-niobium alloy castings (Nickel base Cr 11.5, Al 6.0, Mo 4.0, Nb 2.0)Current
BS 5V 7:1952Specification for mahogany for use in airscrewsWithdrawn
BS 2HR 6:2010Specification for nickel-chromium- iron-molybdenum-cobalt-tungsten heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 21.7, Fe 18.5, Mo 9, Co 1.5, W 0.6)Current
BS 3HR 201:2009Specification for nickel-chromium- titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 2.2, Al 1.4)Current
BS 2HC 203:1989Specification for nickel-chromium-aluminium-molybdenum-niobium alloy castings (Nickel base Cr 13.0, Al 6.0, Mo 4.5, Nb 2.3)Current
BS 2HR 4:2010Specification for nickel-chromium-cobalt-aluminium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 15, Co 14.2, Al 5, Mo 4, Ti 4)Current
BS HR 4:1972Specification for nickel-chromium-cobalt-aluminium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 15, Co 14.2, Al 5, Mo 4, Ti 4)Withdrawn
BS 2HR 209:2011Specification for nickel-chromium-cobalt-molybdenum- titanium-aluminium heat-resisting alloy plate, sheet and strip (Nickel base, Cr 18, Co 14, Mo 7, Ti 2.2, Al 2.1)Current
BS 2HC 211:1989Specification for nickel-chromium-cobalt-molybdenum-aluminium-titanium alloy castings (Nickel base Cr 15.5, Co 10.0, Mo 8,3, Al 4.2, Ti 3.6)Current
BS HR 209:1989Specification for nickel-chromium-cobalt-molybdenum-titanium-aluminium heat-resisting alloy sheet, strip and plate: softened (nickel base, Cr 18, Co 14, Mo 7, Ti 2.2, Al 2.1)Withdrawn
BS 3HR 502:2011Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn and solution treated wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)Current
BS 3HR 501:2011Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)Current
BS 3HR 503:2011Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy wire for thread inserts (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) (0.45 mm to 2 mm diameter)Current
BS 2HR 2:1973Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)Withdrawn
BS 2HR 502:1973Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy cold drawn and solution heat treated wire for springs (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)Withdrawn
BS 2HR 501:1973Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy cold drawn wire for springs (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)Withdrawn
BS 2HR 202:1973Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy sheet and strip (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)Withdrawn
BS 3HR 202:2009Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy sheet and strip (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)Current
BS 2HR 503:1973Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy wire for thread inserts (0.45 mm to 2 mm diameter) (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)Withdrawn
BS 2HR 506:2010Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy wire: softened (nickel base, Cr 19.5, Co 1.8, Ti 2.5, Al 1.5)Current
BS 3HR 2:2010+A2:2012Specification for nickel-chromium-cobalt-titanium-aluminiumheat-resistin g alloy billets, bars, forgings and parts (Nickel base, Cr19.5, Co 18.0 , Ti 2.5, Al 1.5)Current
BS 2HR 208:2009Specification for nickel-chromium-iron alloy plate, sheet and strip: annealed (nickel base, Cr 15.5, Fe 8)Current
BS HR 208:1989Specification for nickel-chromium-iron alloy sheet, strip and plate: annealed (Nickel base, Cr 15.5, Fe 8)Withdrawn
BS HR 6:1972Specification for nickel-chromium-iron-molybdenum-cobalt-tungsten heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 21.7, Fe 18.5, Mo 9, Co 1.5, W 0.6)Withdrawn
BS HR 204:1972Specification for nickel-chromium-iron-molybdenum-cobalt-tungsten heat-resisting alloy plate, sheet and strip (nickel base Cr 22, Fe 18.5, Mo 9, Co 1.5, W 0.6)Withdrawn
BS 2HR 204:2009Specification for nickel-chromium-iron-molybdenum-cobalt-tungsten heat-resisting alloy plate, sheet and strip (nickel base, Cr 21.7, Fe 18.5, Mo 9, Co 1.5, W 0.6)Current
BS HR 505:1981Specification for nickel-chromium-iron-titanium-niobium-aluminium heat-resisting alloy round wire for thread inserts (maximum diameter 2 mm) (nickel base, Cr 15.5, Fe 7.0, Ti 2.5, Nb/Ta 0.95, Al 0.70)Withdrawn
BS 2HR 505:2010Specification for nickel-chromium-iron-titanium-niobium-aluminium heat-resisting alloy round wire with a maximum diameter of 2 mm for thread inserts (nickel base Cr 15.5, Fe 7.0, Ti 2.5, Nb/Ta 0.95, Al 0.70)Current
BS 3HR 504:2011Specification for nickel-chromium-titanium heat-resisting alloy bar and wire for rivets and rivets (Maximum diameter or minor sectional dimension 20 mm) (Nickel base, Cr 19.5, Ti 0.4)Current
BS 2HR 504:1973Specification for nickel-chromium-titanium heat-resisting alloy bar, wire and rivets (nickel base, Cr 19.5, Ti 0.4)Withdrawn
BS HR 5:1972Specification for nickel-chromium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Ti 0.4)Withdrawn
BS 2HR 5:2010Specification for nickel-chromium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Ti 0.4)Current
BS 2HR 203:2009Specification for nickel-chromium-titanium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 0.4)Current
BS HR 203:1972Specification for nickel-chromium-titanium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 0.4)Withdrawn
BS 4HR 601:2010Specification for nickel-chromium-titanium-aluminium heat-resisting alloy bar and wire (maximum diameter or minor sectional dimension of 30 mm) for the manufacture of fasteners (nickel base, Cr 19.5, Ti 2.2, Al 1.4)Current
BS 3HR 601:1989Specification for nickel-chromium-titanium-aluminium heat-resisting alloy bar and wire for the manufacture of fasteners (maximum diameter or minor sectional dimension 30 mm) (nickel base Cr 19.5, Ti 2.2, Al 1.4)Withdrawn
BS 3HR 1:2010Specification for nickel-chromium-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Ti 2.2, Al 1.4)Current
BS 2HR 1:1973Specification for nickel-chromium-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Ti 2.2, Al 1.4)Withdrawn
BS 2HR 201:1974Specification for nickel-chromium-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 2.2, Al 1.4)Withdrawn
BS 2HC 204:1989Specification for nickel-cobalt-chromium-aluminium-titanium-molybdenum alloy castings (Nickel base Co 15.0, Cr 10.0, Al 5.5, Ti 4.8, Mo 3.0)Current
BS HR 3:1972Specification for nickel-cobalt-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 14.8, Mo 5, Al 4.7, Ti 1.2)Withdrawn
BS 2HR 3:2010Specification for nickel-cobalt-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 14.8, Mo 5, Al 4.8, Ti 1.2)Current
BS 2HR 10:2010Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)Current
BS HR 10:1972Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)Withdrawn
BS HR 206:1973Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)Withdrawn
BS 2HR 206:2009Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)Current
BS 2HC 208:1989Specification for nickel-cobalt-tungsten-chromium-aluminium-molybdenum-titanium-tantalum alloy castings (nickel base Co 10.0, W 10.0, Cr 9.0, Al 5.5, Mo 2.5, Ti 1.5, Ta 1.5)Current
BS 2HC 207:1989Specification for nickel-cobalt-tungsten-chromium-aluminium-tantalum-hafnium-titanium alloy castings (Nickel base Co 10.0, W 10.0, Cr 9.0, Al 5.5, Ta 2.5, Hf 1.5, Ti 1.5)Current
BS 2HR 205:2009Specification for nickel-copper alloy sheet and strip: annealed (nickel base, Cu 31)Current
BS 2HR 207:2009Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy plate, sheet and strip (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder)Current
BS HR 207:1973Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy plate, sheet and strip (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder)Withdrawn
BS 2HC 210:1989Specification for nickel-tungsten-aluminium-chromium-molybdenum alloy castings (Nickel base W 10.5, Al 6.0, Cr 6.0, Mo 2.0)Current
BS 2V 35:1966Specification for plywood for aeronautical purposesWithdrawn
BS HC 205:1974Specification for precipitation hardening nickel base chromium-cobalt-molybdenum-titanium alloy castings (Cr 20, Co 20, Mo 6, Ti 2)Current
BS HC 206:1975Specification for precipitation hardening nickel base chromium-cobalt-molybdenum-titanium alloy precision castings (Cr 20, Co 20, Mo 6, Ti 2)Current
BS HC 202:1973Specification for precipitation hardening nickel base chromium-niobium-molybdenum-iron-tungsten alloy castings (Cr 20.0, Nb 6.6, Mo 6.0, Fe 3.0, W 2.5)Current
BS 3J 12:1991Specification for pressure-sensitive adhesive identification tapeCurrent
BS 4J 11:1991Specification for pressure-sensitive adhesive paper masking tapeCurrent
BS 2F 66:1982Specification for rubber bonded cork sheetsCurrent
BS L 515:1973Specification for sheet and strip of magnesium-1¼% zinc-zirconium alloy (suitable for welding by inert-gas shielded arc techniques) (Zn 1.25, Zr 0.6)Withdrawn
BS 2L 504:1973Specification for sheet and strip of magnesium-3% zinc-zirconium alloy (Zn 3.0, Zr 0.6)Withdrawn
BS M 22:1949Specification for silica gel acid activated for aircraft purposesCurrent
BS 2V 37:1968Specification for Sitka spruce as finished timberWithdrawn
BS V 38:1967Specification for Sitka spruce as rough timberWithdrawn
BS 2L 509:1973Specification for tube of magnesium-1¼% zinc-zirconium alloy (suitable for welding by inert-gas shielded arc techniques) (Zn 1.25, Zr 0.6)Withdrawn
BS EN 2103-2:1991Steel, nickel base and cobalt base alloy remelting stock and castings. Technical specification - Remelting stockCurrent
BS EN 2103-3:1992Steel, nickel base and cobalt base alloy remelting stock and castings. Technical specification - Pre-production and production castingsCurrent
BS EN 2103-1:1992Steel, nickel base and cobalt base alloy remelting stock and castings. Technical specification. - General requirementsCurrent
BS EN 2310:1991Test methods for the flame resistance rating of non-metallic materialsCurrent

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