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Aluminium

Standards in development (88)

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Standard TitleStatus
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 2S 515:1969+A3 steel sheet and strip (softened) (foruse in the softened condition: 460/600 MPa) (suitable for welding)null
BS 2S 97:1964+A3 Specification for aircraft material. 2½ per centnickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting rulingsection 6 in)null
BS 2SP 68 to 2SP 71 Specification for 100° countersunk precision head aluminium and aluminium alloy rivetsPublication
BS 2SP 77 to 2SP 80+A4 Specification for snap head aluminium and aluminium alloy rivetsPublication
BS 2SP 81 and 2SP 82+A3 Specification for snap head high nickel-copper alloy rivetsPublication
BS 2SP 87 and 2SP 88+A3 Specification for 100° countersunk head high nickel-copper alloy rivetsPublication
BS 2SP 91 to 92+A4 Specification for carbon steel worm drive clamps for aircraftPublication
BS 2X35:2003+A1 Selectively rentovable interntediate coating for aerospace purposesPublic Comment
BS 3A 117:1962+A1 Specification for corrosion-resisting steel pan head bolts (Unified threads) for aircraftApproval
BS 3S 102:1969+A2 Specification for carbon-molybdenum steel (bar for the manufacture of forged bolts only)null
BS 3S 105:1969+A1 Specification for carbon steel (bar for the manufacture of forged boltsonly)null
BS 3S 144:1995+A2 Specification for chromium-nickel-copper-molybdenum corrosion resistingsteel (precipitation hardening) billets, bars, forgings and parts(1130-1330 MPa)null
BS 3S 145:1996+A2 Specification for Chromium-nickel-coppermolybdenum corrosion resistingsteel (precipitation hardening_ billets, bars, forgings and parts (1270MPa to 1470 MPa)null
BS 3S 95:1967+A1 Specification for 1½ per cent nickel-chromium-molybdenum steel (90/110 kgf/mm2 (57/70 tonf/in2): limiting ruling section 150 mm (6 in))null
BS 3S 98 Specification for 2.5 % nickel-chromium -molybdenum (high carbon) steelbillets, bars, forging and parts 1160-1310 MPa: limiting rulingsection.Public Comment
BS 4S 14:1964+A2 Specification for aircraft material - Carbon case-hardening steelnull
BS 4S 28:1964+A3 Specification for aircraft material - 4 per centnickel-chromium-molybdenum steel - (Air hardening) (100 tonf/sq in:limiting ruling section 2½ in)null
BS 5S 15:1964+A2 Specification for aircraft material - 3 per cent nickel case-hardening steelnull
BS 5S 99:1994+A1 Specification for 2.5% nickel-chromium-molybdenum (high carbon) steelbillets, bars, forgings and parts (1230-1420 MPa: limiting rulingsection 150 mm)null
BS 5X 17:1998+A1 Specification for oleoresinous varnish for aerospace purposesPublic Comment
BS 7S 1:1964+A2 Specification for aircraft material - Carbon steel bright bars for machining - (35/45 tonf/sq in; maximum size, 4 inches diameter or minor sectional dimension)null
BS A 401 Machine Screws, Pan and 100° Countersunk Head, Hexalobular Recess,Unified Threads below .250 inch, Various materials, for AircraftAccepted
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 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 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 3014 Self-locking serrated shank nuts in heat resisiting steel FE-PA92HT - Classification : 1100 MPa/650 °CApproval
BS EN 3015 Shank nuts, self-locking, serrated, in heat resisting steel FE-PA2601 (A 286), silver plated - Classification : 1 100 MPa (at ambient temperature)/650 °CApproval
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 3471 Aerospace series - Steel FE-PA18 - Quenched and cold drawn - Strip forspring - a ? 4,0 mmApproval
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 4234 Aerospace series - Clamps, worm drive - Dimensions, massesApproval
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 4725 Aerospace series - Aluminium alloy AL-P2024 - Al Cu4Mg1 - T351 - Plate - 6 mm < a ? 150 mmPublication
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 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 S 134:1965+A2 Specification for aircraft material. 3 per centchromium-molybdenum-vanadium steel (air hardening) (100 tonf/sq in:limiting ruling section 1? inches)null
BS S 148:1969+A2 Specification for low nickel-chromium steel (bar for the manufacture offorged bolts only))null
BS SP 55 and 56:1953/AMD1 Specifications for double coil spring washers for aircraftnull
BS X 38:2005+A1 purposes - SpecificationPublic Comment
PD CEN/TR 4541 Instruction for the installation of airframe bearingsPublic Comment

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Published standards (198)

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Standard referenceNameStatus
BS EN 4707:2014Aerospace series. Acid pickling of aluminum and aluminum alloy without hexavalent chromiumCurrent
BS EN 3347:2005Aerospace series. Aluminim alloy AL-P2024. T8511. Extruded bar and section. a or D = 150 mm with peripheral coarse grain controlCurrent
BS EN 3342:2005Aerospace series. Aluminim alloy AL-P6061. T4 or T42. Drawn or extruded bar and section. a or D = 150 mmCurrent
BS EN 3338:2005Aerospace series. Aluminim alloy AL-P7050. T74511. Extruded bar and section. a or D = 150 mm with peripheral coarse grain controlCurrent
BS EN 3344:2005Aerospace series. Aluminim alloy AL-P7050. T76511. Extruded bar and section. a or D = 150 mm with peripheral coarse grain controlCurrent
BS EN 2632:2005Aerospace series. Aluminim alloy AL-P7075. T73511. Extruded bar and section. a or D = 150 mm with peripheral coarse grain controlCurrent
BS EN 2072:2005Aerospace series. Aluminium AL-P1050A. H14. Sheet and strip. 0,4 mm = a = 6 mmCurrent
BS EN 2116:2009Aerospace series. Aluminium alloy 2017A-T42. Wire for solid rivets. D = 10 mmCurrent
BS EN 2115:2009Aerospace series. Aluminium alloy 2117-T42. Wire for solid rivets. D = 10 mmCurrent
BS EN 3115:2009Aerospace series. Aluminium alloy 7050-T73. Wire for solid rivets. D = 10 mmCurrent
BS EN 2395:2005Aerospace series. Aluminium alloy AL-P2014A-T4 or T42. Sheet and strip. 0,4 mm =a =6 mmCurrent
BS EN 2088:2005Aerospace series. Aluminium alloy AL-P2014A. T4 or T42. Clad sheet and strip. 0,4 mm = a = 6 mmCurrent
BS EN 2087:2005Aerospace series. Aluminium alloy AL-P2014A. T6 or T62. Clad sheet & strip 0,4 mm = a = 6 mmCurrent
BS EN 2635:2005Aerospace series. Aluminium alloy AL-P2014A. T6511. Extruded bar and section. a or D = 200 mm with peripheral coarse grain controlCurrent
BS EN 2090:2005Aerospace series. Aluminium alloy AL-P2024-T3. Clad sheet and strip 0,3 mm = a = 6 mmCurrent
BS EN 3997:2007Aerospace series. Aluminium alloy AL-P2024-T3. Sheet and strip 0,4 mm « a « 6 mmCurrent, Work in Hand
BS EN 4001:2007Aerospace series. Aluminium alloy AL-P2024-T351. Clad sheet and strip with improved chemical milling capability 1,6 mm = a = 6 mmCurrent
BS EN 3999:2007Aerospace series. Aluminium alloy AL-P2024-T351. Sheet and strip with improved chemical milling capability 1,6 mm = a = 6 mmCurrent
BS EN 2703:2005Aerospace series. Aluminium alloy AL-P2024-T4 or T42. Clad sheet and strip. 0,3 mm = a = 6 mmCurrent
BS EN 3998:2007Aerospace series. Aluminium alloy AL-P2024-T4 or T42. Sheet and strip. 0,3 mm = a = 6 mmCurrent
BS EN 4101:2005Aerospace series. Aluminium alloy AL-P2024-T4. Sheet and strip with improved stretch forming capability. 0,4 mm = a = 6 mmCurrent
BS EN 4211:2005Aerospace series. Aluminium alloy AL-P2024-T42. Clad plate. 6mm < a = 25mmCurrent
BS EN 4247:2005Aerospace series. Aluminium alloy AL-P2024-T42. Plate. 6 mm Current
BS EN 3474:2005Aerospace series. Aluminium alloy AL-P2024-T81. Sheet and strip. 0,25 mm = a = 6 mmCurrent
BS EN 4099:2005Aerospace series. Aluminium alloy AL-P2219-T6 or T62. Clad sheet and strip. 0,5 mm = a = 6 mmCurrent
BS EN 4100:2005Aerospace series. Aluminium alloy AL-P2219-T6 or T62. Sheet and strip. 0,5 mm = a = 6 mmCurrent
BS EN 4102:2005Aerospace series. Aluminium alloy AL-P2219-T81. Clad sheet and strip. 0,5 mm =a =6 mmCurrent
BS EN 4002:2007Aerospace series. Aluminium alloy AL-P2219-T81. Sheet and strip 0,5 mm = a = 6 mmCurrent
BS EN 4209:2005Aerospace series. Aluminium alloy AL-P2219-T851. Plate. 6 mm Current
BS EN 4283:2005Aerospace series. Aluminium alloy AL-P2219-T87. Plate. 6 mm < a = 40 mmCurrent
BS EN 4003:2006Aerospace series. Aluminium alloy AL-P2219-T87. Sheet and strip 0,5 mm = a = 6 mmCurrent
BS EN 3552:2005Aerospace series. Aluminium alloy AL-P2618A-T6 or T62. Clad sheet and strip. 0,4 mm = a = 6 mmCurrent
BS EN 2085:2004Aerospace series. Aluminium alloy AL-P2618A-T6. Hand and die forgings. a = 150 mmCurrent
BS EN 3553:2004Aerospace series. Aluminium alloy AL-P2618A-T6511. Extruded bar and section. a or D = 160 mmCurrent
BS EN 2086:2004Aerospace series. Aluminium alloy AL-P2618A-T851. Hand and die forgings. a = 150 mmCurrent
BS EN 2256:2004Aerospace series. Aluminium alloy AL-P2618A-T852. Hand and die forgings. a = 150 mmCurrent
BS EN 2486:2005Aerospace series. Aluminium alloy AL-P2618A. Forging stockCurrent
BS EN 4004:2007Aerospace series. Aluminium alloy AL-P3103-H16. Sheet and strip. 0,4 mm = a = 6 mmCurrent
BS EN 4005:2007Aerospace series. Aluminium alloy AL-P5052-O. Sheet and strip 0,3 mm = a = 6 mmCurrent
BS EN 2117:2009Aerospace series. Aluminium alloy AL-P5056A (5056A)-H32. Wire for solid rivets. D = 10 mmCurrent
BS EN 4212:2005Aerospace series. Aluminium alloy AL-P5086-H111. Plate. 6mm < a =8 0mmCurrent
BS EN 2693:2005Aerospace series. Aluminium alloy AL-P5086-H111. Sheet and strip. 0,3 mm =a =6 mmCurrent
BS EN 2694:2005Aerospace series. Aluminium alloy AL-P6061-T6 or T62. Sheet and strip. 0,4 mm = a = 6 mmCurrent
BS EN 4213:2005Aerospace series. Aluminium alloy AL-P6061-T651. Plate. 6mm Current
BS EN 2695:2005Aerospace series. Aluminium alloy AL-P6081-T6. Sheet and strip. 0,3 mm =a =6 mmCurrent
BS EN 4006:2007Aerospace series. Aluminium alloy AL-P6082-T4 or T42. Sheet and strip 0,4 mm = a = 6 mmCurrent
BS EN 4007:2005Aerospace series. Aluminium alloy AL-P6082-T6 or T62. Sheet and strip. 0,4 mm 3L a 3L 6 mmCurrent
BS EN 4202:2005Aerospace series. Aluminium alloy AL-P6082-T651. Plate. 6 mm < a = 25 mmCurrent
BS EN 4214:2005Aerospace series. Aluminium alloy AL-P7010-T651. Plate. 6 mm Current
BS EN 2681:2004Aerospace series. Aluminium alloy AL-P7010-T74. Hand and die forgings. a = 150 mmCurrent
BS EN 2687:2004Aerospace series. Aluminium alloy AL-P7010-T7451. Plate. 6 mm < a = 160 mmCurrent
BS EN 3339:2006Aerospace series. Aluminium alloy AL-P7010-T76. Die Forgings. a = 200 mmCurrent
BS EN 2684:2004Aerospace series. Aluminium alloy AL-P7010-T7651. Plate. 6 mm < a = 140 mmCurrent
BS EN 4287:2005Aerospace series. Aluminium alloy AL-P7010. Forging stockCurrent
BS EN 3983:2013Aerospace series. Aluminium alloy AL-P7050-. T7651. Plate. 6 mm < a = 160 mmCurrent
BS EN 4450:2005Aerospace series. Aluminium alloy AL-P7050-T762. Sheet. 0,8 mm =a =6 mmCurrent
BS EN 2092:2005Aerospace series. Aluminium alloy AL-P7075-T6 or T62. Clad sheet and strip. 0,4 mm =a =6 mmCurrent
BS EN 2696:2005Aerospace series. Aluminium alloy AL-P7075-T6 or T62. Sheet and strip. 0,4 mm =a =6 mmCurrent
BS EN 4215:2005Aerospace series. Aluminium alloy AL-P7175-T651. Plate. 6 mm Current
BS EN 2512:2014Aerospace series. Aluminium alloy AL-P7175. T7351. Plate. 6mm < a = 100 mmCurrent
BS EN 4293:2014Aerospace series. Aluminium alloy AL-P7175. T73511. Extruded bar and section. a or D = 150 mmCurrent
BS EN 2803:2005Aerospace series. Aluminium alloy AL-P7475-T761. Clad sheet and strip. 1,0 mm = a = 6 mmCurrent
BS EN 3332:2005Aerospace series. Aluminium alloy AL-P7475-T762. Clad sheet and strip. 1,0 mm = a = 6 mmCurrent
BS EN 3979:2005Aerospace series. Aluminium alloy AL-P8090-O2. Sheet for superplastic forming (SPF). 0,8 mm = a = 6 mmCurrent
BS EN 4286:2005Aerospace series. Aluminium alloy AL-P8090-T89. Die forgings. a = 125 mmCurrent
BS EN 4203:2005Aerospace series. Aluminium alloy AL-P8090-T89. Sheet. 0,6 mm = a = 6 mmCurrent
BS EN 4291:2005Aerospace series. Aluminium alloy AL-P8090. Forging stockCurrent
BS EN 4204:2005Aerospace series. Aluminium alloy AL-P8090. T841. Sheet. 0,6 mm = a = 6 mmCurrent
BS EN 3872:2005Aerospace series. Aluminium alloy AL-R39002-H112. Die forgings. a = 200mmCurrent
BS EN 4292:2005Aerospace series. Aluminium alloy AL-R39002. Forging stockCurrent
BS EN 4324:2002Aerospace series. Aluminium alloy AL-W42201. Filler metal for welding. RodCurrent
BS EN 4341:2001Aerospace series. Aluminium alloy AL-W46431. Filler metal for welding. Wire and rodCurrent
BS EN 2702:2005Aerospace series. Aluminium alloy. AL-P6061. T6 or T62. Drawn or extruded bar and section. a or D = 200 mmCurrent
BS EN 4313:2005Aerospace series. Aluminium aloy AL-P6013-T6. Sheet and strip. 0,5 mm =a =6 mmCurrent
BS EN 3719:2005Aerospace series. Aluminium or aluminium alloy conductors for electrical cables. Product standardWithdrawn
BS EN 2047:2001Aerospace series. Beaded L-section extruded, in aluminium and aluminium alloys. DimensionsCurrent
BS EN 2049:2001Aerospace series. Extruded channel section, in aluminium alloys. DimensionsCurrent
BS EN 2048:2001Aerospace series. Extruded L-section in aluminium alloys. DimensionsCurrent
BS EN 2066:2002Aerospace series. Extruded section in aluminium alloys. General tolerancesCurrent
BS EN 2050:2001Aerospace series. Extruded T-section, in aluminium alloys. DimensionsCurrent
BS EN 2131:2002Aerospace series. Plates in aluminium alloys. Thickness 6 mm < a = 160 mm. DimensionsCurrent
BS EN 2044:2001Aerospace series. Round bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Diameter 4 mm = D = 63 mm. DimensionsCurrent
BS EN 2134:2002Aerospace series. Round bars, extruded in aluminium and aluminium alloys. Diameter 10 mm = D = 220 mm. DimensionsCurrent
BS EN 2071:2002Aerospace series. Sheets in aluminium and aluminium alloys. Thickness 0,25 mm = a = 6 mm. DimensionsCurrent
BS EN 2045:2001Aerospace series. Square bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Thickness 6 mm = a = 50 mm. DimensionsCurrent
BS EN 2599:2001Aerospace series. Strips in aluminium and aluminium alloys. Thickness 0,25 mm = a = 3.2 mm. DimensionsCurrent
BS EN 2072:1994Aluminium alloy AL-P1050A-H14. Sheet and strip 0,4 mm = a = 6 mmWithdrawn
BS EN 2089:2005Aluminium alloy AL-P2014A T6 or T62. Sheet and strip. 0,4 mm = a = 6 mmCurrent
BS EN 2395:1994Aluminium alloy AL-P2014A-T4 or T42. Sheet and strip 0,4 mm = a = 6 mmWithdrawn
BS EN 2100:1992Aluminium alloy AL-P2014A-T4511. Extruded bars and sections a or D = 200 mmCurrent
BS EN 2089:1994Aluminium alloy AL-P2014A-T6 or T62. Sheet and strip 0,4 mm = a = 6 mmWithdrawn
BS EN 2384:1992Aluminium alloy AL-P2014A-T6511. Extruded bars and sections a or D = 150 mmCurrent
BS EN 2318:1992Aluminium alloy AL-P2024-T3511. Extruded bars and sections 1,2 mm = a or D = 150 mmCurrent
BS EN 2633:1994Aluminium alloy AL-P2024-T3511. Extruded bars and sections 1,2 mm = a or D = 150 mm with peripheral coarse grain controlCurrent, Work in Hand
BS EN 2422:2005Aluminium alloy AL-P2124-T351. Plate. 25 mm < a = 120 mmCurrent
BS EN 3341:2005Aluminium alloy AL-P6061-T4 or T42. Sheet and strip. 0,4 mm = a = 6 mmCurrent
BS EN 2326:1992Aluminium alloy AL-P6082-T6. Extruded bars and sections a or D = 200 mmCurrent
BS EN 2636:1994Aluminium alloy AL-P6082-T6. Extruded bars and sections a or D = 200 mm with peripheral coarse grain controlCurrent
BS EN 2094:1992Aluminium alloy AL-P7009-T74. Die forgings 3 mm = a = 150 mmCurrent
BS EN 2093:1992Aluminium alloy AL-P7009-T74. Hand forgings 20 mm = a = 150 mmCurrent
BS EN 2385:1992Aluminium alloy AL-P7009-T74511. Extruded bars and sections a or D = 125 mmCurrent
BS EN 2630:1994Aluminium alloy AL-P7009-T74511. Extruded bars and sections a or D = 125 mm with peripheral coarse grain controlCurrent
BS EN 2381:1992Aluminium alloy AL-P7009-T7452. Hand forgings 40 mm = a = 150 mmCurrent
BS EN 4449:2005Aluminium alloy AL-P7050. T76. Sheet. 0,8 mm = a = 6 mmCurrent
BS EN 2092:1994Aluminium alloy AL-P7075-T6 or T62. Clad sheet and strip 0,4 mm = a = 6 mmWithdrawn
BS EN 2126:1992Aluminium alloy AL-P7075-T651. Plate 6 mm < a = 80 mmCurrent
BS EN 2128:1992Aluminium alloy AL-P7075-T7351. Drawn bars 6 mm = a or D = 75 mmCurrent
BS EN 2511:2005Aluminium alloy AL-P7075-T7351. Plate. 6 mm < a = 100 mmCurrent
BS EN 2127:1992Aluminium alloy AL-P7075-T73511. Extruded bars and sections a or D = 100 mmCurrent
BS EN 2632:1994Aluminium alloy AL-P7075-T73511. Extruded bars and sections a or D = 100 mm with peripheral coarse grain controlWithdrawn
BS EN 3335:2005Aluminium alloy AL-P7475-O2. Sheet for superplastic forming (SPF). 0,8 mm = a = 6 mmCurrent
BS EN 2802:2005Aluminium alloy AL-P7475-T761. Sheet and strip. 0,6 mm = a = 6 mmCurrent
BS EN 3333:2005Aluminium alloy AL-P7475-T762. Sheet and strip. 0,6 mm = a = 6 mmCurrent
BS EN 2693:1994Aluminium alloy. AL-P5086-H111. Sheet and strip 0,3 mm = a = 6 mmWithdrawn
BS EN 2694:1994Aluminium alloy. AL-P6061-T6 or T62. Sheet and strip 0,4 mm = a = 6 mmWithdrawn
BS EN 2695:1994Aluminium alloy. AL-P6081-T6. Sheet and strip 0,3 mm = a = 6 mmWithdrawn
BS EN 2696:1994Aluminium alloy. AL-P7075-T6 or T62. Sheet and strip 0,4 mm = a = 6 mmWithdrawn
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 EN 2046:2001Hexagonal bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Width across flats 7 mm = a = 50 mm. DimensionsCurrent
BS 2L 169:2002Ingots (as cast) and castings (solution treated and artificially aged) of aluminium-silicon-magnesium alloy (Si 7, Mg 0.6)Current
BS 4L 101:1990Procedure for inspection, testing and acceptance of aluminium-base and magnesium-base ingots and castingsWithdrawn
BS 5L 101:2011Procedure for inspection, testing and acceptance of aluminium-base and magnesium-base ingots and castingsCurrent
BS 5L 100:2011+A1:2013Procedure for inspection, testing and acceptance of wrought aluminium and aluminium alloysCurrent
BS 4L 100:1993Procedure for inspection, testing and acceptance of wrought aluminium and aluminium alloysWithdrawn
BS EN 2082-1:1991Specification for aluminium alloy forging stock and forgings. Technical specification - General requirementsCurrent
BS EN 2082-2:1991Specification for aluminium alloy forging stock and forgings. Technical specification - Forging stockCurrent
BS EN 2082-3:1991Specification for aluminium alloy forging stock and forgings. Technical specification - Pre-production and production forgingsCurrent, Work in Hand
BS EN 2070-4:1991Specification for aluminium and aluminium alloy wrought products. Technical specification - Tube for structuresCurrent
BS EN 2070-5:1991Specification for aluminium and aluminium alloy wrought products. Technical specification - Tube used under pressureCurrent
BS EN 2070-6:1991Specification for aluminium and aluminium alloy wrought products. Technical specification - Rivet wireCurrent, Work in Hand
BS EN 2070-7:1991Specification for aluminium and aluminium alloy wrought products. Technical specification - Wrought forging stockCurrent
BS EN 2070-3:1991Specification for aluminium and aluminium alloy wrought products. Technical specification - Bar and sectionCurrent
BS EN 2070-1:1991Specification for aluminium and aluminium alloy wrought products. Technical specification - General requirementsCurrent
BS EN 2070-2:1991Specification for aluminium and aluminium alloy wrought products. Technical specification - Sheet, strip formed profiles and plateCurrent
BS 2L 88:1971Specification for aluminium-alloy-coated sheet and strip of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and precipitation treated) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15)Withdrawn
BS L 109:1971Specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 1.5, Mn 0.6)Withdrawn
BS L 110:1971Specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-manganese alloy (supplied for solution treatment by the user) (Cu 4.4, Mg 1.5, Mn 0.6)Withdrawn
BS L 102:1971Specification for bars and extruded sections of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (not exceeding 200 mm diameter or minor sectional dimension) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)Current
BS L 168:1978Specification for bars and extruded sections of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (not exceeding 200 mm diameter or minor sectional dimension) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)Current
BS 2L 84:1971Specification for bars and extruded sections of aluminium-copper-silicon-magnesium alloy (solution treated and aged at room temperature) (not exceeding 200 mm diameter or minor sectional dimension) (Cu 1.5, Si 1, Mg 0.8)Withdrawn
BS L 111:1971Specification for bars and extruded sections of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)Current
BS L 173:1991Specification for castings of aluminium-silicon-magnesium alloy, chill cast (solution treated and precipitation treated to an overaged (T7) condition)Current
BS L 174:1991Specification for castings of aluminium-silicon-magnesium alloy, sand cast (solution treated and precipitation treated to an overaged (T7) condition)Current
BS EN 2101:1991Specification for chromic acid anodizing of aluminium and wrought aluminium alloysCurrent
BS L 166:1978Specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)Withdrawn
BS L 167:1978Specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)Withdrawn
BS L 158:1978Specification for close toleranced sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)Withdrawn
BS L 159:1978Specification for close toleranced sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)Withdrawn
BS L 170:1989Specification for extruded bars and sections of aluminium-zinc-copper-chromium alloy (solution treated, controlled stretched and artificially aged) (not exceeding 150 mm diameter or minor sectional dimension) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.23) (7075)Current
BS L 172:1989Specification for extruded, rolled or cast forging stock of aluminium-zinc-magnesium-manganese-copper alloy (for manufacture of forgings to BS L 171) (Zn 5.7, Mg 2.7, Mn 0.5, Cu 0.5) (7014)Current
BS L 171:1990Specification for forging of aluminium-zinc-magnesium-manganese-copper alloy (supplied as-forged or annealed for subsequent heat treatment) (not exceeding 150 mm diameter or minor sectional dimension) (Zn 5.7, Mg 2.7, Mn 0.5, Cu 0.5) (7014)Current
BS L 103:1971Specification for forging stock and forgings of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)Withdrawn
BS 2L 77:1971Specification for forging stock and forgings of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)Current
BS L 112:1971Specification for forging stock and forgings of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)Current
BS 5L 34:1985Specification for forging stock, bars, extruded sections and forgings of 99% aluminiumCurrent
BS 5L 44:1985Specification for forging stock, bars, extruded sections and forgings of aluminium-2¼% magnesium alloyWithdrawn
BS 2L 83:1971Specification for forging stock, bars, extruded sections and forgings of aluminium-copper-nickel-magnesium-iron-silicon alloy (solution treated and precipitation treated) (Cu 2, Ni 1, Mg 1, Si 0.9, Fe 0.9)Withdrawn
BS 2L 85:1971Specification for forging stock, bars, extruded sections and forgings of aluminium-copper-silicon-magnesium alloy (solution treated and precipitation treated) (Cu 1.5, Si 1, Mg 0.8)Withdrawn
BS 2L 87:1971Specification for hexagonal bars for nuts, couplings and hollow machined parts of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (free from peripheral and asymmetric coarse grain) (not less than 14 mm nor more than 36 mm across flats) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)Withdrawn
BS L 119:1975Specification for ingots and castings of aluminium-copper-nickel-manganese-titanium-zirconium-cobalt-antimony alloy (solution treated and artificially aged) (Cu 5.0, Ni 1.5, Mn 0.25, Ti 0.2, Zr 0.2, Co 0.2, Sb 0.2)Current
BS L 154:1977Specification for ingots and castings of aluminium-copper-silicon alloy (solution treated and aged at room temperature) (Cu 4, Si 1)Current
BS L 155:1977Specification for ingots and castings of aluminium-copper-silicon alloy (solution treated and artificially aged) (Cu 4, Si 1)Current
BS 3L 51:1970Specification for ingots and castings of aluminium-silicon-copper-iron-nickel-magnesium alloy (precipitation treated) (Si 2.5, Cu 1.2, Fe 1, Ni 1, Mg 0.1)Withdrawn
BS 3L 78:1970Specification for ingots and castings of aluminium-silicon-copper-magnesium alloy (solution treated and precipitation treated) (Si 5, Cu 1.2, Mg 0.5)Withdrawn
BS L 169:1986Specification for ingots and castings of aluminium-silicon-magnesium alloy (solution treated and artificially aged) (Si 7, Mg 0.6)Withdrawn
BS 2L 99:1972Specification for ingots and castings of aluminium-silicon-magnesium alloy (solution treated and precipitation treated) (Si 7, Mg 0.3)Current
BS 2L 98:1971Specification for plate of aluminium-copper-magnesium-manganese alloy (solution treated and aged at room temperature: not controlled stretched) (Cu 4.4, Mg 1.5, Mn 0.6)Withdrawn
BS 2L 97:1971Specification for plate of aluminium-copper-magnesium-manganese alloy (solution treated, controlled stretched and aged at room temperature) (Cu 4.4, Mg 1.5, Mn 0.6)Withdrawn
BS 2L 93:1971Specification for plate of aluminium-copper-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)Current
BS L 115:1971Specification for plate of aluminium-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (not exceeding 25 mm thickness) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)Withdrawn
BS 2L 95:1971Specification for plate of aluminium-zinc-magnesium-copper-chromium alloy (solution treated, controlled stretched and precipitation treated) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15)Current
BS 6L 16:1985Specification for sheet and strip of 99% aluminium (temper designation H14 or H24)Current
BS 6L 17:1985Specification for sheet and strip of 99% aluminium (temper designation-O)Current
BS 3L 81:1985Specification for sheet and strip of aluminium-2¼% magnesium alloy (temper designation H16 or H26)Current
BS 3L 80:1985Specification for sheet and strip of aluminium-2¼% magnesium alloy (temper designation-O)Current
BS L 164:1978Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)Current
BS L 165:1978Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)Current
BS L 163:1978Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated, cold worked for flattening and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)Withdrawn
BS L 156:1978Specification for sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)Withdrawn
BS L 157:1978Specification for sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)Withdrawn
BS L 113:1971Specification for sheet and strip of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)Withdrawn
BS 4L 60:1985Specification for sheet and strip of aluminium-manganese alloy (temper designation H12 or H22)Withdrawn
BS 4L 59:1985Specification for sheet and strip of aluminium-manganese alloy (temper designation H16 or H26)Withdrawn
BS 4L 61:1985Specification for sheet and strip of aluminium-manganese alloy (temper designation-O)Withdrawn
BS EN 2284:1991Specification for sulfuric acid anodizing of aluminium and wrought aluminium alloysCurrent, Work in Hand
BS L 105:1971Specification for tube of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (not exceeding 10 mm wall thickness) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)Current
BS 3L 63:1971Specification for tube of aluminium-copper-mangesium-silicon-manganese alloy (solution treated and precipitation treated) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)Current
BS 7L 37:1989Specification for wire for solid cold-forged rivets of aluminium-copper-magnesium-silicon-manganese alloy (for use in the solution treated and naturally aged condition) (not exceeding 10 mm diameter) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8) (2014A)Current
BS 5L 36:1985Specification for wire for solid, cold-forged rivets of 99.5% aluminium (not exceeding 10 mm diameter)Current
BS 3L 58:1971Specification for wire for solid, cold-forged rivets of aluminium-5% magnesium alloy (not exceeding 10 mm diameter)Withdrawn
BS 3L 86:1971Specification for wire for solid, cold-forged rivets of aluminium-copper-magnesium alloy (not exceeding 10 mm diameter) (Cu 2.5, Mg 0.3)Withdrawn
BS L 160:1976Specification. Bars and extruded sections of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)Current
BS L 162:1976Specification. Cold compressed hand forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)Withdrawn
BS L 161:1976Specification. Hand and die forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)Withdrawn
BS EN 2004-1:1993Test methods for aluminium and aluminium alloy products - Determination of electrical conductivity of wrought aluminium alloysCurrent
BS EN 2004-5:1993Test methods for aluminium and aluminium alloy products - Determination of cladding thickness and copper diffusion of clad semi-finished productsCurrent

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