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Bolts, screws & studs

Standards in development (217)

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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 2SP 90:2008/Amd 1 Specification for corrosion-resisting steel split cotter pins foraircraft - Inch seriesPublication
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 2342 Aerospace series. Heat and crazing resistant acrylic sheet for aircraft glazing.Accepted
BS EN 2591-227 Aerospace series - Elements of electrical and optical connection - Test methods Part 227: Partial discharges testPublic Comment
BS EN 2714-014 Aerospace series - Cables, electrical, single and multicore for general purpose - Operating temperatures between - 55 °C and 260 °C Part 014: DR family, 5 to 10 cores, taped, screened (braided) and jacketed, UV laser printable - Product standardPublication
BS EN 2811 Aerospace series - Nuts, hexagon, slotted/ castellated in steel cadmiumplated - Classification: 1 100 MPa/235 °CPublication
BS EN 2879 Aerospace series - Nuts, anchor, self-locking, air resistant, sealing, floating, two lug, with counterbore, in corrosion resisting steel, passivated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature) / 235°CPublication
BS EN 2997-002 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak Part 002: Specification of performance and contact arrangementsPublication
BS EN 2997-005 Aerospace series — Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures – 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak — Part 005: Hermetic square flange receptaclePublication
BS EN 2997-007 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak Part 007: Hermetic receptacle with round flange attached by welding or brazing - Product standardPublication
BS EN 2997-014 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak Part 014: Square flange receptacle with integrated accessory - Product standardPublication
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 3155-001 Aerospace series - Electrical contacts used in elements of connection Part 001: Technical SpecificationPublication
BS EN 3155-020 Aerospace Series. Electrical contacts used in elements of connection Size 10 Contact, electrical, triaxial, male 020, type D, crimp, class R, Product StandardAccepted
BS EN 3155-021 Aerospace Series. Electrical contacts used in elements of connection Contacts, electrical, triaxial, size 10 female, type D, crimp, class R - Product StandardAccepted
BS EN 3375-007 Aerospace series - Cable, electrical, for digital data transmission Part 007: Double braid - 77 Ohms - Type WW - Product standardPublication
BS EN 3375-009 Aerospace series - Cable, electrical, for digital data transmission Part 009: Single braid -- CAN Bus -- 120 Ohms -- Type WX - Product standardPublication
BS EN 3572 PTFE flexible hose assembly with convoluted inner tube and titanium 8 degrees 30 mn coupling - Product standardPublication
BS EN 3672 Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated, for 30° swage - Classification: 1 210 MPa (at ambient temperature)/730 °CPublication
BS EN 3745-510 Aerospace series - Fibres and cables, optical, aircraft use - Test methods Part 510: Bending testApproval
BS EN 3745-516 Aerospace series - Fibres and cables, optical, aircraft use - Test methods Part 516: Severe cable bend testApproval
BS EN 3745-517 Aerospace series - Fibres and cables, optical, aircraft use - Test methods Part 517: Cable tie clamping testApproval
BS EN 3875 Aerospace Series - Metallic Materials - Filler metal for brazing - T Technical SpecificationPublication
BS EN 3879 Aerospace series - Metallic materials - Filler metal for welding - Technical SpecificationPublic Comment
BS EN 3902 Washers for rivet assemblies, in aluminium alloy, anodized, metric seriesPublication
BS EN 3903 Washers, laminated, in corrosion resisting steelPublication
BS EN 3908 Aerospace series - Nipples, lubricating, axial type, in corrosionresisting steel, passivatedPublication
BS EN 4056-003 Aerospace series - Cable ties for harnesses Part 003: Plastic cable ties - Operating temperatures -65 °C to 105 °C and -65 °C to 150 °C - Product standardPublication
BS EN 4107 Aerospace series Non-metallic materials Structural adhesive systems Foaming adhesives Technical specificationAccepted
BS EN 4165-001:2015/AC2016 Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature 175 °C continuous Part 001: Technical specificationPublication
BS EN 4165-001:2015/Cor2 Aerospace series - Connectors, electrical, rectangular, modular -Operating temperature 175 °C continuous,, ,, Part 001: Technical specification ,,Publication
BS EN 4165-002:2015/AC:2016 Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature 175 °C continuous Part 002: Specification of performance and contact arrangementsPublication
BS EN 4165-013 Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature 175 °C continuous Part 013: Cable clamp 2 and 4 modules for connectors, series 2 and series 3 - Product standardPublication
BS EN 4165-019 Aerospace series - Connectors, electrical, rectangular, modular, operating temperature 175 degrees C continuous Part 019: Protective cover for plug, for 2 or 4 modules series 2 and 3 - Product standardPublic Comment
BS EN 4178 Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °CPublication
BS EN 4184 Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 45°, welded ends, doublePublic Comment
BS EN 4297 Aerospace series - Nuts, hexagon, self-locking by plastic ring, normal height, normal across flats, in corrosion resisting steel, passivated - Classification: 900 MPa (at ambient temperature) / 120 °CPublication
BS EN 4309 Nuts, hexagon, self-locking by plastic ring, normal height, normqal across flats, in alloy steel, cadmium plated-Classification: 900 MPa (at ambiant temperature) / 120°Publication
BS EN 4400-4 Aerospace series - Aluminium and aluminium- and magnesium- alloys - Technical specification Part 4:Aluminium and aluminium alloy tubePublic Comment
BS EN 4440 Aerospace series Rubber panels and calendered sheets DimensionsAccepted
BS EN 4474 Aluminium pigmented coatings - Coating methodsPublication
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 4531-001 Aerospace series - Connectors, optical, circular, single and multipin, coupled by threaded ring - Flush contacts Part 001 : Technical specificationApproval
BS EN 4534-2 Aerospace series - Bushes, plain in aluminium alloy with self-lubricating liner, elevated load Part 2: Dimensions and loads - Inch seriesPublication
BS EN 4535-2 Aerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load Part 2: Dimensions and loads - Inch seriesPublication
BS EN 4548 Aerospace series - Structural adhesive system - Adhesive film / Anticorrosion primer - Epoxy based - For continuous use up to 120 °CIdea
BS EN 4604-009 Aerospace series - Cable, electrical, for signal transmission Part 009 : Cable, coaxial, light weight, 50 Ohms, 180 °C, type KW (light WN) - Product standardApproval
BS EN 4677-002 Aerospace series - Welded and brazed assemblies for aerospace constructions Electron beam welding machine Part 002 : Qualification specificationsPublic Comment
BS EN 4691-1 Aerospace series - Tie rod with integrated bolts Part 1: Technical specificationPublication
BS EN 4691-2 Aerospace series - Tie rod with integrated bolts Part 2: Overview construction kitPublication
BS EN 4692 Aerospace series - Tie Rod with integrated bolts - Locking clipPublication
BS EN 4693 Aerospace series - Tie rod with integrated bolts - Assembly code A, Band CPublication
BS EN 4694 Aerospace series - Tie rod with integrated bolts - Assembly code D, Eand FPublication
BS EN 4695 Aerospace series - Tie Rod with integrated bolts - Assembly Code G, Hand KPublication
BS EN 4701-002 Aerospace series - Connectors, optical, rectangular, modular, operating temperature 125 °C, for EN 4531-101 contacts Part 002: MaterialApproval
BS EN 4708-101 Aerospace series - Sleeving, heat-shrinkable, for binding, insulation and identification Part 101: Polyolefin sleevingTechnical Review
BS EN 4827 Aerospace series - Hexavalent chromium free anodizing and sealing of aluminium and aluminium alloysApproval
BS EN 6029 Aerospace series - Rod-ends, adjustable, single fork with UNJ threaded shank min. engagement: 1,5 x thread diameter in corrosion resisting steel - Dimensions and loads - Inch seriesApproval
BS EN 6059-307 Aerospace series - Electrical cables, installation - Protection sleeves - Test methods - Part 307: AgeingPublic Comment
BS EN 6080 Aerospace series - Rivet, 100° normal flush head, close tolerance - InchseriesPublication
BS EN 6081 Aerospace series - Rivet, universal head, close tolerance - Inch seriesPublication
BS EN 6090 Aerospace series - Washer, retainingPublication
BS EN 6092 Aerospace series - Receptacle, floating, double lugPublication
BS EN 6094 Aerospace series - Washer, spring, countersunkPublication
BS EN 6101 Aerospace series - Rivet, 100° medium flush head, close tolerance - Inch seriesPublication
BS EN 6105 Aerospace series - Stud with shoulderPublication
BS EN 6129 Aerospace series - Blind bolt, Protruding head, high strengthPublication
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 15872 Aerospace - UNJ threads - GaugingPublic Comment
BS ISO 20894 Aircraft - LED based taxiing light system - General requirementsIdea
BS ISO 20949 Aircraft - Smart Contactor - General RequirementsIdea
BS ISO 2100 Aircraft - Electrical connectors - TestsAccepted
BS ISO 2100-100 Aerospace elements of electrical and optical connection - Test methods Part 100: GeneralAccepted
BS ISO 2100-101 Aerospace elements of electrical and optical connection - Test methods Part 101: Visual examinationAccepted
BS ISO 2100-102 Aerospace elements of electrical and optical connection - Test methods Part 102: Examination of dimensions and massAccepted
BS ISO 2100-201 Aerospace elements of electrical and optical connection - Test methods Part 201: Contact resistance at low levelAccepted
BS ISO 2100-202 Aerospace elements of electrical and optical connection - Test methods Part 202: Contact resistance at rated currentAccepted
BS ISO 2100-203 Aerospace elements of electrical and optical connection - Test methods Part 203: Electrical continuity at microvolt levelAccepted
BS ISO 2100-204 Aerospace elements of electrical and optical connection - Test methods Part 204: Discontinuity of contacts in the microsecond rangeAccepted
BS ISO 2100-205 Aerospace elements of electrical and optical connection - Test methods Part 205: Housing (shell) electrical continuityAccepted
BS ISO 2100-206 Aerospace elements of electrical and optical connection - Test methods Part 206: Measurement of insulation resistanceAccepted
BS ISO 2100-207 Aerospace elements of electrical and optical connection - Test methods Part 207: Voltage proof testAccepted
BS ISO 2100-208 Aerospace elements of electrical and optical connection - Test methods Part 208: Temperature rise due to rated currentAccepted
BS ISO 2100-209 Aerospace elements of electrical and optical connection - Test methods Part 209: Current temperature deratingAccepted
BS ISO 2100-211 Aerospace elements of electrical and optical connection - Test methods Part 211: CapacitanceAccepted
BS ISO 2100-212 Aerospace elements of electrical and optical connection - Test methods Part 212: Surface transfer impedanceAccepted
BS ISO 2100-213 Aerospace elements of electrical and optical connection - Test methods Part 213: Shielding effectiveness from 100 MHz to 1 GHzAccepted
BS ISO 2100-216 Aerospace elements of electrical and optical connection - Test methods Part 216: Engagement depth of contactsAccepted
BS ISO 2100-217 Aerospace elements of electrical and optical connection - Test methods Part 217: Voltage drop under specified current for terminal lugs and in-line splicesAccepted
BS ISO 2100-218 Aerospace elements of electrical and optical connection - Test methods Part 218: Ageing of terminal lugs and in-line splices by temperature and current cyclingAccepted
BS ISO 2100-219 Aerospace elements of electrical and optical connection - Test methods Part 219: Voltage strength for insulated terminal lugs and in-line splicesAccepted
BS ISO 2100-301 Aerospace elements of electrical and optical connection - Test methods Part 301: Endurance at temperatureAccepted
BS ISO 2100-302 Aerospace elements of electrical and optical connection - Test methods Part 302: Climatic sequenceAccepted
BS ISO 2100-303 Aerospace elements of electrical and optical connection - Test methods Part 303: Cold/low pressure and damp heatAccepted
BS ISO 2100-305 Aerospace elements of electrical and optical connection - Test methods Part 305: Rapid change of temperatureAccepted
BS ISO 2100-306 Aerospace elements of electrical and optical connection - Test methods Part 306: Mould growthAccepted
BS ISO 2100-307 Aerospace elements of electrical and optical connection - Test methods Part 307: Salt mistAccepted
BS ISO 2100-308 Aerospace elements of electrical and optical connection - Test methods Part 308: Sand and dustAccepted
BS ISO 2100-309 Aerospace elements of electrical and optical connection - Test methods Part 309: Dry heatAccepted
BS ISO 2100-310 Aerospace elements of electrical and optical connection - Test methods Part 310: ColdAccepted
BS ISO 2100-311 Aerospace elements of electrical and optical connection - Test methods Part 311: Low air pressureAccepted
BS ISO 2100-312 Aerospace elements of electrical and optical connection - Test methods Part 312: Air leakageAccepted
BS ISO 2100-313 Aerospace elements of electrical and optical connection - Test methods Part 313: Artificial rainAccepted
BS ISO 2100-314 Aerospace elements of electrical and optical connection - Test methods Part 314: Immersion at low pressureAccepted
BS ISO 2100-315 Aerospace elements of electrical and optical connection - Test methods Part 315: Fluid resistanceAccepted
BS ISO 2100-317 Aerospace elements of electrical and optical connection - Test methods Part 317: FlammabilityAccepted
BS ISO 2100-318 Aerospace elements of electrical and optical connection - Test methods Part 318: Fire resistanceAccepted
BS ISO 2100-319 Aerospace elements of electrical and optical connection - Test methods Part 319: Gastightness of solderless wrapped connectionsAccepted
BS ISO 2100-321 Aerospace elements of electrical and optical connection - Test methods Part 321: Damp heat, cyclic testAccepted
BS ISO 2100-323 Aerospace elements of electrical and optical connection - Test methods Part 323: Thermal shockAccepted
BS ISO 2100-325 Aerospace elements of electrical and optical connection - Test methods Part 325: Ice resistanceAccepted
BS ISO 2100-401 Aerospace elements of electrical and optical connection - Test methods Part 401: Acceleration, steady stateAccepted
BS ISO 2100-402 Aerospace elements of electrical and optical connection - Test methods Part 402: ShockAccepted
BS ISO 2100-403 Aerospace elements of electrical and optical connection - Test methods Part 403: Sinusoidal and random vibrationAccepted
BS ISO 2100-404 Aerospace elements of electrical and optical connection - Test methods Part 404: Transverse loadAccepted
BS ISO 2100-405 Aerospace elements of electrical and optical connection - Test methods Part 405: Axial loadAccepted
BS ISO 2100-406 Aerospace elements of electrical and optical connection - Test methods Part 406: Mechanical enduranceAccepted
BS ISO 2100-407 Aerospace elements of electrical and optical connection - Test methods Part 407: Durability of contact retention system and seals (Maintenance ageing)Accepted
BS ISO 2100-408 Aerospace elements of electrical and optical connection - Test methods Part 408: Mating and unmating forcesAccepted
BS ISO 2100-409 Aerospace elements of electrical and optical connection - Test methods Part 409: Contact retention in insertAccepted
BS ISO 2100-410 Aerospace elements of electrical and optical connection - Test methods Part 410: Insert retention in housing (axial)Accepted
BS ISO 2100-411 Aerospace elements of electrical and optical connection - Test methods Part 411: Insert retention in housing (torsional)Accepted
BS ISO 2100-412 Aerospace elements of electrical and optical connection - Test methods Part 412: Contact insertion and extraction forces in and out of insertAccepted
BS ISO 2100-413 Aerospace elements of electrical and optical connection - Test methods Part 413: Holding force of grounding spring systemAccepted
BS ISO 2100-414 Aerospace elements of electrical and optical connection - Test methods Part 414: Unmating of layard release connectorsAccepted
BS ISO 2100-415 Aerospace elements of electrical and optical connection - Test methods Part 415: Test probe damage (female contact)Accepted
BS ISO 2100-416 Aerospace elements of electrical and optical connection - Test methods Part 416: Contact bending strengthAccepted
BS ISO 2100-417 Aerospace elements of electrical and optical connection - Test methods Part 417: Tensile strength (crimped connection)Accepted
BS ISO 2100-418 Aerospace elements of electrical and optical connection - Test methods Part 418: Gauge insertion and extraction forces in and out of female contactAccepted
BS ISO 2100-419 Aerospace elements of electrical and optical connection - Test methods Part 419: Stability of male contacts in insertAccepted
BS ISO 2100-420 Aerospace elements of electrical and optical connection - Test methods Part 420: Mechanical strength of rear accessoriesAccepted
BS ISO 2100-421 Aerospace elements of electrical and optical connection - Test methods Part 421: Free fallAccepted
BS ISO 2100-422 Aerospace elements of electrical and optical connection - Test methods Part 422: Locking wire hole strengthAccepted
BS ISO 2100-424 Aerospace elements of electrical and optical connection - Test methods Part 424: Stripping force, solderless wrapped connectionsAccepted
BS ISO 2100-425 Aerospace elements of electrical and optical connection - Test methods Part 425: Unwrapping, solderless wrapped connectionsAccepted
BS ISO 2100-426 Aerospace elements of electrical and optical connection - Test methods Part 426: Contact retention system effectiveness (removable contact walkout)Accepted
BS ISO 2100-427 Aerospace elements of electrical and optical connection - Test methods Part 427: Robustness of protective cover attachmentAccepted
BS ISO 2100-428 Aerospace elements of electrical and optical connection - Test methods Part 428: Sinusoidal vibrations with passage of current for crimped terminal lugsAccepted
BS ISO 2100-501 Aerospace elements of electrical and optical connection - Test methods Part 501: Soft solderabilityAccepted
BS ISO 2100-502 Aerospace elements of electrical and optical connection - Test methods Part 502: Restricted entryAccepted
BS ISO 2100-503 Aerospace elements of electrical and optical connection - Test methods Part 503: Contact deformation after crimpingAccepted
BS ISO 2100-505 Aerospace elements of electrical and optical connection - Test methods Part 505: Contact protection effectiveness (soop proof)Accepted
BS ISO 2100-506 Aerospace elements of electrical and optical connection - Test methods Part 506: Use of toolsAccepted
BS ISO 2100-507 Aerospace elements of electrical and optical connection - Test methods Part 507: Plating porosityAccepted
BS ISO 2100-508 Aerospace elements of electrical and optical connection - Test methods Part 508: Measurement of thickness of coating on contactsAccepted
BS ISO 2100-509 Aerospace elements of electrical and optical connection - Test methods Part 509: Adhesion of coating on contactsAccepted
BS ISO 2100-512 Aerospace elements of electrical and optical connection - Test methods Part 512: Effectiveness of non-removable fixing of hermetically sealed connector shellAccepted
BS ISO 2100-513 Aerospace elements of electrical and optical connection - Test methods Part 513: Magnetic permeabilityAccepted
BS ISO 2100-514 Aerospace elements of electrical and optical connection - Test methods Part 514: Solderability of contacts with self-contained solder and fluxAccepted
BS ISO 2100-601 Aerospace elements of electrical and optical connection - Test methods Part 601: Optical elements - Insertion lossAccepted
BS ISO 2100-602 Aerospace elements of electrical and optical connection - Test methods Part 602: Optical elements - Variation of attenuation and optical discontinuityAccepted
BS ISO 2100-603 Aerospace elements of electrical and optical connection - Test methods Part 603: Change of power distributionAccepted
BS ISO 2100-604 Aerospace elements of electrical and optical connection - Test methods Part 604: Optical elements - Cleaning capability of optical faceAccepted
BS ISO 2100-605 Aerospace elements of electrical and optical connection - Test methods Part 605: Optical elements - Return lossAccepted
BS ISO 2100-606 Aerospace elements of electrical and optical connection - Test methods Part 606: Optical elements - CrosstalkAccepted
BS ISO 2100-607 Aerospace elements of electrical and optical connection - Test methods Part 607: Optical elements - Immunity to ambient light couplingAccepted
BS ISO 2100-609 Aerospace elements of electrical and optical connection - Test methods Part 609: Optical elements - Effectiveness of cable attachment - Cable cycling flexingAccepted
BS ISO 2100-610 Aerospace elements of electrical and optical connection - Test methods Part 610: Optical elements - Effectiveness of cable attachment - Cable pullingAccepted
BS ISO 2100-6101 Aerospace elements of electrical and optical connection - Test methods Part 6101: Optical elements - Visual examinationAccepted
BS ISO 2100-611 Aerospace elements of electrical and optical connection - Test methods Part 611: Optical elements - Effectiveness of cable attachment - Cable torsionAccepted
BS ISO 2100-612 Aerospace elements of electrical and optical connection - Test methods Part 612: Optical elements - Effectiveness of cable attachment - Cable axial compressionAccepted
BS ISO 2100-613 Aerospace elements of electrical and optical connection - Test methods Part 613: Optical elements - Impact testAccepted
BS ISO 2100-614 Aerospace elements of electrical and optical connection - Test methods Part 614: Optical elements - Connector radial compressionAccepted
BS ISO 2100-615 Aerospace elements of electrical and optical connection - Test methods Part 615: Optical elements - Connection integrity at temperatureAccepted
BS ISO 2100-617 Aerospace elements of electrical and optical connection - Test methods Part 617: Optical elements - Temperature cyclingAccepted
BS ISO 2100-6301 Aerospace elements of electrical and optical connection - Test methods Part 6301: Optical elements - Endurance at temperatureAccepted
BS ISO 2100-6303 Aerospace elements of electrical and optical connection - Test methods Part 6303: Optical elements - Cold/low pressure and damp heatAccepted
BS ISO 2100-6305 Aerospace elements of electrical and optical connection - Test methods Part 6305: Optical elements - Rapid change of temperatureAccepted
BS ISO 2100-6306 Aerospace elements of electrical and optical connection - Test methods Part 6306: Optical elements - Mould growthAccepted
BS ISO 2100-6307 Aerospace elements of electrical and optical connection - Test methods Part 6307: Optical elements - salt mistAccepted
BS ISO 2100-6314 Aerospace elements of electrical and optical connection - Test methods Part 6314: Optical elements - Immersion at low pressureAccepted
BS ISO 2100-6315 Aerospace elements of electrical and optical connection - Test methods Part 6315: Optical elements - Fluid resistanceAccepted
BS ISO 2100-6316 Aerospace elements of electrical and optical connection - Test methods Part 6316: Optical elements - Ozone resistanceAccepted
BS ISO 2100-6317 Aerospace elements of electrical and optical connection - Test methods Part 6317: Optical elements - FlammabilityAccepted
BS ISO 2100-6318 Aerospace elements of electrical and optical connection - Test methods Part 6318: Optical elements - Fire resistanceAccepted
BS ISO 2100-6321 Aerospace elements of electrical and optical connection - Test methods Part 6321: Optical elements - Damp heat cyclic testAccepted
BS ISO 2100-6323 Aerospace elements of electrical and optical connection - Test methods Part 6323: Optical elements - Thermal shock (Hermetically sealed devices)Accepted
BS ISO 2100-6324 Aerospace elements of electrical and optical connection - Test methods Part 6324: Optical elements - Interfacial sealingAccepted
BS ISO 2100-6401 Aerospace elements of electrical and optical connection - Test methods Part 6401: Optical elements - Acceleration steady stateAccepted
BS ISO 2100-6402 Aerospace elements of electrical and optical connection - Test methods Part 6402: Optical elements - ShockAccepted
BS ISO 2100-6403 Aerospace elements of electrical and optical connection - Test methods Part 6403: Optical elements - VibrationsAccepted
BS ISO 2100-6404 Aerospace elements of electrical and optical connection - Test methods Part 6404: Optical elements - Transverse loadAccepted
BS ISO 2100-6405 Aerospace elements of electrical and optical connection - Test methods Part 6405: Optical elements - Axial loadAccepted
BS ISO 2100-6406 Aerospace elements of electrical and optical connection - Test methods Part 6406: Optical elements - Mechanical enduranceAccepted
BS ISO 2100-6414 Aerospace elements of electrical and optical connection - Test methods Part 6414: Optical elements - Unmating of lanyard release optical connection elementsAccepted
BS ISO 2100-6415 Aerospace elements of electrical and optical connection - Test methods Part 6415: Optical elements - Test probe damageAccepted
BS ISO 2635:2003/Amdd 1 Aircraft - Conductors for general purpose aircraft electrical cables and aerospace applications - Dimensions and characteristics - Amendmentd 1Public Comment
BS ISO 3203 Aerospace - Bolts, normal bihexagonal head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa - DimensionsPublic Comment
BS ISO 6858 Aircraft - Ground support electrical supplies - General requirementsPublication
BS ISO 7481 Aerospace - Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C - Test methodsPublic Comment
BS ISO 8056-2:1988/Amdd 1 Aircraft - Nickel-chromium and nickel-aluminium thermocouple extension cables Part 2: Terminations - General requirements and tests - Amendmentd 1Publication
BS ISO 8168 Aerospace - Bolts, with MJ threads, made of heat and corrosion resisting steel, strength class 1 100 MPa - Procurement specificationPublication
BS SP 94:1964/Amd 3 Specification for bronze oil-retaining bushes and thrust washers - For aircraftApproval
PD CEN/TR 4541 Instruction for the installation of airframe bearingsPublic Comment
PD CEN/TR 4646 Aerospace series - Fibres and cables of optical contact EN4531 - Aircraft use - TR n°4646null
PD CEN/TR 4653 Aerospace series - Technical specification of plating of connectors Cadmium and hexavalent Chromium replacementnull
PD CEN/TR 4654-001 Aerospace series - Connector, electrical and optical, rectangular, modular, rectangular inserts, EN4644 specific products Part 1 : Technical specificationnull
PD CEN/TR 4654-002 Aerospace series - Connector, electrical and optical, rectangular, modular, rectangular inserts, EN4644 specific products Part 002: Specification of performance and list of technical reportsnull
PD CEN/TR 4654-003 Aerospace series - Connector, electrical and optical, rectangular, modular, rectangular inserts, EN4644 specific products Part 003: Inserts with PC tails electrical contacts -Technical reportnull
PD CEN/TR 4654-010 Aerospace series - Connectors, electrical Part 010: 1Q18 connectors - Technical reportnull
PD CEN/TR 4654-200 Aerospace series - Connectors, electrical Part 200: Size 8 male quadrax contact pc tails – Technical reportnull
PD CEN/TR 4680 Aerospace series - Contacts, electrical, qualification for change of materials and processAccepted
PD CEN/TR 6058 ED 11 Aerospace series: Cable code identification listIdea

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Published standards (266)

Sort by: Reference | Title | Status

Standard referenceNameStatus
BS 3A 174:2012100° Countersunk head, D-slot recess, corrosion-resisting steel bolts (Unified threads), Strength Class 880 MPa, for aircraftCurrent
BS EN 2606:2009Aerospace series. 60° interface for adaptors, threaded, with lockring. Geometric configurationCurrent
BS EN 3444:2006Aerospace series. Bolt, large bihexagonal head, close tolerance normal shank, medium length thread, in heat resisting nickel base alloy, passivated. Classification: 1250 MPa (at ambient temperature) / 650°CCurrent
BS EN 3685:2008Aerospace series. Bolts in heat resisting steel FE-PA2601 (A286). Classification: 1100 MPa/650 °C. Technical specificationCurrent
BS EN 3302:2007Aerospace series. Bolts in heat resisting steel FE-PM1708 (FV535). Classification: 1000 MPa/550°C. Technical specificationCurrent, Work in Hand
BS EN 3323:2009Aerospace series. Bolts with double hexagon head, relieved shank, long thread, in heat resisting steel FE-PM 38 (FV 535). Classification: 1000 MPa/550 °CCurrent
BS EN 3326:2007Aerospace series. Bolts, D-head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-PH2601 (INCO 718). Classification: 1275 MPa/650°C, unplatedCurrent
BS EN 4352:2003Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickel base alloy NI-PH 2601 (Inconel 718), MoS2 coated. Classification: 1550 MPa (at ambient temperature)/425 °CWithdrawn
BS EN 4352:2004Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated. Classification. 1 550 MPa (at ambient temperature) / 425°CCurrent
BS EN 4321:2004Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated. Classification. 1 550 Mpa (at ambient temperature)/650°CCurrent
BS EN 4321:2003Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickelbase alloy NI-PH2601 (Inconel 718), silver plated. Classification: 1550 MPa (at ambient temperature)/650 °CWithdrawn
BS EN 4322:2004Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated. Strength class: 1100 MPa (at ambient temperature)Current
BS EN 4322:2003Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated. Strength class: 1100 MPa (at ambient temperature)Withdrawn
BS EN 4009:2003Aerospace series. Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718). Classification: 1550 MPa (at ambient temperature)/650 °CWithdrawn
BS EN 4009:2004Aerospace series. Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718). Classification: 1550 MPa (at ambient temperature)Current
BS EN 3327:2008Aerospace series. Bolts, double hexagon head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-P100HT (Inconel 718), uncoated. Classification: 1275 MPa/650 °CCurrent
BS EN 3328:2008Aerospace series. Bolts, double hexagon head, close tolerance, medium thread length, in heat resisting steel FE-PM38 (FV535), uncoated. Classification: 1000 MPa/550 °CCurrent
BS EN 3907:2003Aerospace series. Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated. Classification: 1100 MPa (at ambient temperature)/350°CWithdrawn
BS EN 3907:2004Aerospace series. Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated. Classification: 1100MPa (at ambient temperature)/350°CCurrent
BS EN 3832:2003Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718). Classification: 1550 MPa (at ambient temperature) / 650°CWithdrawn
BS EN 3832:2004Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718). Classification: 1550 MPa (at ambient temperature) / 650°CCurrent
BS EN 3686:2008Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated. Classification: 1100 MPa/650°CCurrent
BS EN 3724:2003Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001 MoS2 coated. Classification: 1 100 MPa (at ambient temperature)Withdrawn
BS EN 3324:2007Aerospace series. Bolts, hexagon head, relieved shank, long thread, in heat resisting steel FE-PM1708 (FV535). Classification: 1000 MPa/550°C. UnplatedCurrent
BS EN 4498:2005Aerospace series. Bolts, large bihexagonal head, close tolerance normal shank, medium length thread, in heat resisting nickel base alloy, passivated, with aluminium pigmented coating. Classification: 1 550 MPa (at ambient temperature) / 315 °CCurrent
BS EN 3833:2004Aerospace series. Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), passivated. Classification: 1550 MPa (at ambient temperature) / 650°C. Technical specificationCurrent, Work in Hand
BS EN 3833:2003Aerospace series. Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718). Classification: 1550 MPa (at ambient temperature) / 650°C. Technical specificationsWithdrawn
BS EN 3818:2004Aerospace series. Bolts, MJ threads, in titanium alloy TI-P64001. Strength class: 1100 MPa (at ambient temperature). Technical specificationCurrent
BS EN 4136:2009Aerospace series. Bolts, normal bi-hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated. Classification: 1100 MPa at ambient temperature)/235°CCurrent
BS EN 4135:2009Aerospace series. Bolts, normal bi-hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature)/315°CCurrent
BS EN 4137:2009Aerospace series. Bolts, normal bi-hexagonal head, stepped shank, long thread, in titanium alloy, anodized, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature)/315°CCurrent
BS EN 3687:2010Aerospace series. Bolts, normal hexagon head, relieved shank, long thread, in heat resisting steel FE-PA2601 (A286), silver plated.Classifi cation: 1100 MPa/650 °CCurrent
BS EN 2859:2006Aerospace series. Bolts, normal hexagonal head, close tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification: 1100 MPa (at ambient temperature) / 235°CCurrent
BS EN 3052:2009Aerospace series. Bolts, normal hexagonal head, close tolerance normal shank, short thread, in heat and corrosion resisting steel, passivated. Classification: 1100 MPa (at ambient temperature) / 425 °CCurrent
BS EN 4071:2009Aerospace series. Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated. Classification: 1100 MPa (at ambient temperature) / 425 °CCurrent, Work in Hand
BS EN 4495:2006Aerospace series. Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating, metric series. Classification: 1100 MPa (at ambient temperature) / 315°CCurrent
BS EN 4501:2006Aerospace series. Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating, metric series. Classification: 1100 MPa (at ambient temperature) / 315°CCurrent
BS EN 2549:2006Aerospace series. Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium, anodized, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature) / 315°CCurrent
BS EN 4132:2009Aerospace series. Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated. Classification: 1100 MPa (at ambient temperature)/235°CCurrent
BS EN 4134:2009Aerospace series. Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in heat resisting nickel base alloy, aluminium IVD coated. Classification: 1250 MPa (at ambient temperature)/425°CCurrent
BS EN 4133:2009Aerospace series. Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in titanium alloy, aluminium IVD coated. Classification: 1100 MPa (at ambient temperature) / 425 °CCurrent
BS EN 4129:2009Aerospace series. Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated. Classification: 1100 MPa (at ambient temperature) / 235°CCurrent
BS EN 4131:2009Aerospace series. Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated. Classification: 1250 MPa (at ambient temperature) / 425 °CCurrent
BS EN 4130:2009Aerospace series. Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, aluminium IVD coated. Classification: 1100 MPa (at ambient temperature) / 425 °CCurrent
BS EN 4128:2009Aerospace series. 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 °CWithdrawn
BS EN 4127:2009Aerospace series. Bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated. Classification: 1100 MPa (at ambient temperature)/ 425 °CCurrent
BS EN 4128:2016Aerospace series. Bolts, normal hexagonal head, coarse tolerance shank, short thread, in heat resisting nickel base alloy, aluminium IVD coated. Classification: 1 250 MPa (at ambient temperature) / 425 °CCurrent
BS EN 3613:2009Aerospace series. Bolts, normal hexagonal head, relieved shank, long thread, in heat resisting nickel base alloy NIPH2601 (Inconel 718), silver plated. Classification: 1275 MPa/650 °CCurrent
BS EN 3614:2009Aerospace series. Bolts, normal hexagonal head, relieved shank, long thread, in heat resisting steel FE-PA2601 (A286), silver plated. Classification: 900 MPa/650°CCurrent
BS EN 3725:2003Aerospace series. Bolts, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated. Classification: 1100 MPa (at ambient temperature)Withdrawn
BS EN 3912:2007Aerospace series. Bolts, pan head, six lobe recess, relieved shank, long thread, in heat resisting steel FE-PA2601 (FE-PA92HT, A286), silver plated. Classification: 1100 MPa (at ambient temperature) / 650°CCurrent
BS 3A 117:1962+A2:2016Aerospace Series. Bolts, Pan Head, Slotted Drive, Unified Threads, Corrosion Resisting Steel, Strength Class 880 MPa, for Aircraft. SpecificationCurrent
BS EN 3301:2007Aerospace series. Bolts, T-head, close tolerance medium thread length in heat resisting steel FE-PM1708 (FV535), uncoated. Classification: 1000 MPa/550°CCurrent
BS EN 3294:2008Aerospace series. Bolts, T-head, close tolerance, in heat resisting nickel base alloy NI-P101HT (Waspaloy), uncoated for increased height nuts. Classification: 1210 MPa/730°CCurrent
BS EN 3293:2008Aerospace series. Bolts, T-head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-P100HT (Inconel 718), uncoated. Classification: 1275 MPa/650°CCurrent
BS EN 3325:2007Aerospace series. Bolts, T-head, relieved shank, long thread, in heat resisting steel, FE-PM1708 (FV535). Classification: 1000 MPa/550°C. UnplatedCurrent
BS ISO 16130:2015Aerospace series. Dynamic testing of the locking behaviour of bolted connections under transverse loading conditions (vibration test)Current
BS EN 3389:2009Aerospace series. Fasteners, externally threaded, in heat resisting nickel base alloy NI-PH1302 (Waspaloy). Classification: 1210 MPa/730°C. Manufacturing method optional. Technical specificationCurrent
BS EN 3388:2009Aerospace series. Fasteners, externally threaded, in heat resisting nickel base alloy NI-PH2601 (Inconel 718). Classification 1275 MPa/650°C. Manufacturing method optional. Technical specificationCurrent
BS EN 3706:2012Aerospace series. Headless threaded plugs, cross recess, in aluminium alloy 5086Current
BS EN 3707:2012Aerospace series. Headless threaded plugs. Installation holesCurrent
BS EN 4176:2005Aerospace series. Lockbolts, 100° countersunk normal head or protruding head, tension-/ sheartype, close tolerance, in titanium alloy TI-P64001, anodized or with aluminium pigmented coating. Collars in titanium TI-P99002 or aluminium alloy 2024. Metric series. Technical specificationCurrent
BS EN 4402:2006Aerospace series. Lockbolts, 100° countersunk normal head, sheartype, close tolerance, in titanium alloy TI-P64001,with aluminium pigmented coating, metric series. Classification: 1100 MPa (at ambient temperature) / 315°CCurrent
BS EN 4172:2006Aerospace series. Lockbolts, protruding head, sheartype, close tolerance, in titanium alloy TI-P64001, anodized, metric series. Classification: 1 100 MPa (at ambient temperature) / 315°CCurrent
BS EN 2889:2006Aerospace series. Metric bolts, normal hexagon head, coarse tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification: 900 MPa (at ambient temperature) / 235°CCurrent
BS EN 2888:2006Aerospace series. Metric bolts, normal hexagon head, coarse tolerance normal shank, short thread, in corrosion resisting steel, passivated. Classification: 600 MPa (at ambient temperature) / 425°CCurrent
BS EN 3820:2006Aerospace series. Metric bolts, normal hexagon head, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature)/315°CCurrent, Work in Hand
BS EN 2883:2009Aerospace series. Nuts, hexagonal, self-locking, with counterbore and captive washer, in heat resisting steel, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature)/315°CCurrent
BS EN 3777:2010Aerospace series. Pins, quick release, single and double acting. Technical specificationCurrent
BS EN 4163:2009Aerospace series. Screws 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated. 1100 MPa (at ambient temperature) / 235°CWithdrawn
BS EN 4163:2016Aerospace series. Screws 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated. Classification: 1 100 MPa (at ambient temperature) / 235 °CCurrent
BS EN 4162:2009Aerospace series. Screws 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated. 1100 MPa (at ambient temperature) / 235°C - EN 4162:2009Withdrawn
BS EN 4162:2016Aerospace series. Screws 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated. Classification: 1 100 MPa (at ambient temperature) / 235 °CCurrent
BS EN 4634:2009Aerospace series. Screws, 100° countersunk head, six lobe recess, short thread, in heat resisting steel FE-PA2601 (A286), passivated. Classification: 900 MPa (at ambient temperature)/650°CCurrent
BS EN 4636:2009Aerospace series. Screws, 100° countersunk head, six lobe recess, short thread, in titanium alloy TI-P64001, with aluminium pigmented coating. Classification: 1100 MPa (at ambient temperature) / 315°CCurrent
BS EN 4323:2004Aerospace series. Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated. Classification. 900 MPa (at ambient temperature) / 350°CCurrent
BS EN 4323:2003Aerospace series. Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated. Classification: 900 MPa (at ambient temperature)/350°CWithdrawn
BS EN 4635:2009Aerospace series. Screws, 100° countersunk head, six lobes recess, short thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718). Classification: 1270 MPa (at ambient temperature) / 650 °CCurrent
BS EN 4072:2009Aerospace 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 °CWithdrawn
BS EN 4496:2005Aerospace series. Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating. Classification: 1100 MPa (at ambient temperature) / 315 °CCurrent
BS EN 4072:2016Aerospace series. Screws, 100° countersunk normal head, offset cruciform recess, close tolerance shank, short thread in titanium alloy, aluminium IVD coated. Classification: 1 100 MPa (at ambient temperature) / 425 °CCurrent
BS EN 4499:2009Aerospace series. Screws, 100° countersunk reduced head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating. Classification: 1100 MPa (at ambient temperature) / 315 °CCurrent
BS EN 4073:2016Aerospace series. Screws, pan head, hexalobular recess, coarse tolerance shank, medium length thread, in alloy steel, cadmium plated. Classification: 1 100 MPa (at ambient temperature) / 235 °CCurrent
BS EN 4497:2005Aerospace series. Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating. Classification: 1 100 MPa (at ambient temperature) / 315 °CCurrent
BS EN 4161:2009Aerospace series. Screws, pan head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated. Classification: 1100 MPa (at ambient temperature) / 235 °CCurrent
BS EN 4138:2016Aerospace series. Screws, pan head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated. Classification: 1 100 MPa (at ambient temperature) / 235 °CCurrent
BS EN 4138:2009Aerospace series. 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°CWithdrawn
BS EN 4075:2008Aerospace series. Screws, pan head, offset cruciform recess, threaded to head, in corrosion resisting steel, passivated. Classification: 490 MPa (at ambient temperature) / 425 °CCurrent
BS EN 4073:2009Aerospace series. 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°CWithdrawn
BS EN 4074:2009Aerospace series. Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, aluminium IVD coated. Classification: 1100 MPa (at ambient temperature)/425°CCurrent
BS EN 3725:2004Aerospace series. Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated. Strength class: 1100 MPa (at ambient temperature)Current
BS EN 3636:2008Aerospace series. Screws, reduced pan head, offset cruciform recess, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated. Classification: 900 MPa/650°CCurrent
BS EN 3905:2008Aerospace series. Six lobe recesses for bolts. Technical specificationCurrent
BS EN 4312:2006Aerospace series. Studs, coarse tolerance reduced shank, medium length thread, in heat and corrosion resisting steel, with aluminium pigmented coating. Classification: 1100 MPa (at ambient temperature) / 315°CCurrent
BS EN 4311:2006Aerospace series. Studs, coarse tolerance reduced shank, medium length threads, in heat and corrosion resisting steel, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature) / 315°CCurrent
BS EN 4421:2007Aerospace series. Studs, in titanium alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel. Strength class: 1100 MPa(at ambient temperature)Current
BS EN 4459:2005Aerospace series. Studs, in titanium alloy TI-P64001, with serrated locking ring in corrosion resisting steel. Design standardCurrent
BS EN 4460:2005Aerospace series. Studs, in titanium alloy TI-P64001, with serrated locking ring in corrosion resisting steel. Installation and removal procedureCurrent
BS EN 4458:2005Aerospace series. Studs, MJ threads, in titanium alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel.Strengt h class: 1100 MPa (at ambient temperature). TechnicalspecificationCurrent
BS ISO 3186:2008Aerospace. Bolts, large bihexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes 1250 MPa to 1800 MPa. Dimensions Current
BS ISO 3185:2008Aerospace. Bolts, normal bihexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsCurrent
BS ISO 3193:2008Aerospace. Bolts, normal hexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsCurrent
BS ISO 9255:2008Aerospace. Bolts, normal spline head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsCurrent
BS A 332:1999Aerospace. Bolts, with MJ threads, in titanium alloys, strength class 1 100 MPa. Procurement specificationCurrent
BS ISO 7689:2008Aerospace. Bolts, with MJ threads, made of alloy steel, strength class 1100 MPa. Procurement specificationWithdrawn
BS ISO 5857:2008Aerospace. Bolts, with MJ threads, made of alloy steel, strength class 1250 MPa. Procurement specificationCurrent
BS ISO 8168:2008Aerospace. Bolts, with MJ threads, made of heat and corrosion resisting steel, strength class 1100 MPa. Procurement specificationCurrent, Work in Hand
BS ISO 9154:2016Aerospace. Bolts, with MJ threads, made of heat-resistant nickel-based alloy, strength class 1 550 MPa. Procurement specificationCurrent
BS ISO 14280:2002Aerospace. Drivers, ribbed, for internal cruciform ribbed or unribbed drives. Metric seriesCurrent
BS ISO 14277:2002Aerospace. Drivers, ribbed, for internal offset cruciform ribbed or unribbed drives. Metric seriesCurrent
BS ISO 12256:2002Aerospace. Drives, internal, cruciform, ribbed. Metric seriesCurrent
BS ISO 14279:2002Aerospace. Drives, internal, cruciform. Metric seriesCurrent
BS ISO 14275:2002Aerospace. Drives, internal, offset cruciform, ribbed. Metric seriesCurrent
BS ISO 14276:2002Aerospace. Drives, internal, offset cruciform. Metric seriesCurrent
BS ISO 14281:2002Aerospace. Gauges, for internal cruciform ribbed or unribbed drives. Metric seriesCurrent
BS ISO 14278:2002Aerospace. Gauges, for internal offset cruciform ribbed or unribbed drives. Metric seriesCurrent
BS ISO 12257:2008Aerospace. Internal six-lobe drives. Metric seriesCurrent
BS ISO 5856:2008Aerospace. Screws, 100 degrees normal countersunk head, internal offset cruciform ribbed or unribbed drive, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsCurrent
BS ISO 13921:2008Aerospace. Screws, 100 degrees reduced countersunk head, internal offset cruciform ribbed or unribbed drive, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsCurrent
BS A 311:1997Aerospace. Screws, 100° reduced countersunk head, internal offset cruciform ribbed or unribbed drive, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsWithdrawn
BS ISO 12261:2016Aerospace. 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. DimensionsCurrent
BS ISO 12260:2016Aerospace. 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. DimensionsCurrent
BS A 313:1997Areospace. 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 1100 MPa. DimensionsWithdrawn
BS 2A 266 TO 2A 271:2016Bolt, 100° Countersunk head, Hi-Torque speed drive recess, UNJF thread , split pin hole option, titanium alloy, various finishes, Classification: 80 Tf/in2 (1 100 MPa) at TA/+315 °CCurrent
BS 2A 296:1995Bolts and screws, metric. Tolerances of form and positionCurrent
BS EN 3818:2003Bolts with MJ threads, in titanium alloy TI-P64001. Classification:1100 MPa (at ambient temperature). Technical specificationWithdrawn
BS EN 3379:1996Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), for increased height nuts. Classification: 1210 MPa (at ambient temperature)/730°CCurrent
BS EN 3063:1994Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy). Classification: 1210 MPa (at ambient temperature)/730°CCurrent
BS EN 2928:1996Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plated. Classification: 1275 MPa (at ambient temperature)/650°CCurrent
BS EN 2927:1996Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718). Classification:1275 MPa (at ambient temperature)/650°CCurrent
BS EN 2930:1996Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated. Classification:1210 MPa (at ambient temperature)/730°CCurrent
BS EN 2929:1996Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy). Classification: 1210 MPa (at ambient temperature)/730°CCurrent
BS EN 2925:1994Bolts, double hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A 286). Classification: 900 MPa (at ambient temperature)/650°CCurrent
BS EN 2926:1996Bolts, double hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated. Classification: 900 MPa (at ambient temperature)/650°CCurrent
BS EN 3724:2004Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated. Strength class: 1100 MPa (at ambient temperature)Current
BS EN 3009:1998Bolts, hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plated. Classification. 1275 MPa (at ambient temperature)/650°CCurrent
BS EN 3008:1998Bolts, hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718). Classification:1275 MPa (at ambient temperature)/650°CCurrent
BS EN 3011:1998Bolts, hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated. Classification:1210 MPa (at ambient temperature)/730 °CCurrent
BS EN 3010:1998Bolts, hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy). Classification: 1210 MPa (at ambient temperature)/730°CCurrent
BS EN 3007:1996Bolts, hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated. Classification: 900 MPa (at ambient temperature)/650°CCurrent
BS EN 3006:1994Bolts, hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286). Classification: 900 MPa (at ambient temperature)/650°CCurrent
BS EN 2874:1996Bolts, large bihexagonal head, close tolerance normal shank, medium length thread, in heat resisting nickel base alloy, passivated. Classification: 1550 MPa (at ambient temperature) /315°CCurrent
BS A 310:1995Bolts, large bihexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes 1250 MPa to 1800 MPa. DimensionsWithdrawn
BS A 309:1994Bolts, large hexagonal head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsCurrent
BS EN 2583:1997Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718). Classification: 1275 MPa (at ambient temperature)/650°C. Technical specificationCurrent
BS EN 2870:1996Bolts, normal bihexagonal head, close tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature) /315°CCurrent
BS A 304:1994Bolts, normal bihexagonal head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsCurrent
BS A 303:1994Bolts, normal bihexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsWithdrawn
BS EN 2859:1995Bolts, normal hexagonal head, close tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification: 1100 MPa (at ambient temperature)/235°CWithdrawn
BS EN 3052:1994Bolts, normal hexagonal head, close tolerance normal shank, short thread, in heat and corrosion resisting steel, passivated. Classification: 1100 MPa (at ambient temperature)/425°CWithdrawn
BS EN 2549:1995Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature)/315°CWithdrawn
BS EN 2889:1995Bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification. 900 MPa (at ambient temperature)/235°CWithdrawn
BS EN 2888:1995Bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in corrosion resisting steel, passivated. Classification: 600 MPa (at ambient temperature)/425°CWithdrawn
BS EN 3112:1995Bolts, normal hexagonal head, threaded to head, in alloy steel, cadmium plated. Classification: 900 MPa (at ambient temperature)/235°CCurrent
BS EN 2887:1995Bolts, normal hexagonal head, threaded to head, in corrosion resisting steel, passivated. Classification: 600 MPa (at ambient temperature)/425°CCurrent
BS A 307:1994Bolts, normal spline head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsCurrent
BS A 308:1994Bolts, normal spline head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsWithdrawn
BS A 331:1998Bolts, reduced bihexagonal head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1275 MPa. DimensionsCurrent
BS EN 2413:1995Bolts, shouldered, thin hexagonal head, close tolerance shank, short thread, in alloy steel, cadmium plated. Classification: 1100 MPa (at ambient temperature)/235°CCurrent
BS EN 3740:1997Bolts, shouldered, thin hexagonal head, close tolerance shank, short thread, in titanium alloy, anodized, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature)/315°CCurrent
BS EN 2934:1996Bolts, T-head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plated. Classification:1275 MPa (at ambient temperature)/650°CCurrent
BS EN 2933:1996Bolts, T-head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718). Classification:1275 MPa (at ambient temperature)/650°CCurrent
BS EN 2936:1996Bolts, T-head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated. Classification: 1210 MPa (at ambient temperature)/730°CCurrent
BS EN 2935:1996Bolts, T-head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy). Classification:1210 MPa (at ambient temperature)/730°CCurrent
BS EN 2932:1996Bolts, T-head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated. Classification: 900 MPa (at ambient temperature)/650°CCurrent
BS EN 2931:1993Bolts, T-head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286). Classification: 900 MPa (at ambient temperature)/650°CCurrent
BS A 363:2000Bolts, with MJ threads, made of heat-resistant nickel-based alloy, strength class 1 550 MPa. Procurement specificationWithdrawn
BS A 305:1994Bolts. Test methodsCurrent
BS A 241:1973General requirements for steel protruding-head bolts of tensile strength 1250 MPa (180000 lbf/in2) or greaterWithdrawn
BS 2A 241:2005+A2:2011General requirements for steel protruding-head bolts of tensile strength 1250 MPa (180000 lbf/in2) or greater. SpecificationCurrent
BS EN 3202:1995Holes and traps for T-head bolts. Design standardCurrent
BS EN 2236:1992Pins, headed, close tolerance shank, in alloy steel. Technical specificationCurrent
BS A 301:1989Procurement of corrosion and heat-resisting steel bolts with strength classification 1100 MPa and MJ threadsWithdrawn
BS G 154:1958Screws with captive washers for aircraftCurrent
BS EN 2939:1994Screws, 100° countersunk head, offset cruciform recess, threaded to head in heat resisting steel FE-PA92HT (A286). Classification: 900 MPa (at ambient temperature)/650°CCurrent
BS EN 2940:1996Screws, 100° countersunk head, offset cruciform recess, threaded to head, in heat resisting steel FE-PA92HT (A 286), silver plated. Classification: 900MPa (at ambient temperature)/650°CCurrent
BS EN 3035:1997Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification: 1100 MPa (at ambient temperature)/235°CCurrent
BS EN 3543:1997Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in heat and corrosion resisting steel, passivated. Classification: 1100 MPa (at ambient temperature)/425°CCurrent
BS EN 3381:1997Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in titanium, anodized, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature) /315°CCurrent
BS EN 3760:1997Screws, 100° countersunk normal head, offset cruciform recess, threaded to head, in heat and corrosion resisting steel, passivated. Classification: 1100 MPa (at ambient temperature)/425°CCurrent
BS EN 3306:1996Screws, 100° countersunk normal head, offset cruciform recess, threaded to head, in titanium alloy, anodized, MoS2 lubricated. Classification. 1100 MPa (at ambient temperature)/315°CCurrent
BS EN 4509:2006Screws, 100° countersunk normal head, offset cruciform recess, threaded to head, in titanium alloy, anodized, with aluminium pigmented coating, metric series. Classification: 1100 MPa (at ambient temperature)/315°CCurrent
BS EN 2652:1997Screws, 100° countersunk normal head, slotted, threaded to head, in alloy steel, cadmium plated. Classification: 900 MPa (at ambient temperature)/235°CCurrent
BS EN 2654:1997Screws, 100° countersunk normal head, slotted, threaded to head, in brass, tin plated. Classification: 380 MPa (at ambient temperature)/80°CCurrent
BS EN 2653:1997Screws, 100° countersunk normal head, slotted, threaded to head, in corrosion resisting steel, passivated. Classification: 600 MPa (at ambient temperature) /425°CCurrent
BS EN 3305:1997Screws, 100° countersunk reduced head, offset cruciform recess, close tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification: 1100 MPa (at ambient temperature)/235°CCurrent
BS EN 3304:1997Screws, 100° countersunk reduced head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature)/315°CCurrent
BS EN 3303:1997Screws, cap head, hexagon socket, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated. Classification: 1100 MPa (at ambient temperature)/235°CCurrent
BS EN 2937:1994Screws, hexagon head, threaded to head in heat resisting steel FE-PA92HT (A286) classification: 900 MPa (at ambient temperature)/650°CCurrent
BS EN 2938:1996Screws, hexagon head, threaded to head, in heat resisting steel FE-PA92HT (A 286), silver plated. Classification: 900 MPa (at ambient temperature)/650°CCurrent
BS EN 3308:1996Screws, normal hexagonal head, threaded to head, in titanium alloy, anodized, MoS2 lubricated. Classification. 1100 MPa (at ambient temperature) /315°CCurrent
BS A 312:1997Screws, 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 1100 MPa. DimensionsWithdrawn
BS A 322:1998Screws, pan head, internal offset cruciform ribbed or unribbed drive, threaded to head, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa. DimensionsCurrent
BS EN 2886:1996Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification. 900 MPa (at ambient temperature)/235°CCurrent
BS EN 2897:1996Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification: 1100 MPa (at ambient temperature) /235°CCurrent
BS EN 3038:1997Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in heat and corrosion resisting steel, passivated. Classification: 1100 MPa (at ambient temperature)/425°CCurrent
BS EN 3037:1997Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature)/315°CCurrent
BS EN 2885:1996Screws, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification: 900 MPa (at ambient temperature)/235°CCurrent
BS EN 2884:1996Screws, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in titanium alloy, anodized MoS2 lubricated. Classification: 1100 MPa (at ambient temperature)/315°CCurrent
BS EN 3759:1997Screws, pan head, offset cruciform recess, threaded to head, in heat and corrosion resisting steel, passivated. Classification: 1100 MPa (at ambient temperature)/425°CCurrent
BS EN 3307:1997Screws, pan head, offset cruciform recess, threaded to head, in titanium alloy, anodized, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature)/315°CCurrent
BS EN 2649:1995Screws, pan head, slotted, threaded to head, in alloy steel, cadmium plated. Classification. 900 MPa (at ambient temperature)/235°CCurrent
BS EN 2651:1997Screws, pan head, slotted, threaded to head, in brass, tin plated. Classification: 380 MPa (at ambient temperature)/80°CCurrent
BS EN 2650:1997Screws, pan head, slotted, threaded to head, in corrosion resisting steel, passivated. Classification: 600 MPa (at ambient temperature) /425°CCurrent
BS 2A 175:1962Specification for 100° countersunk head aluminium alloy bolts (Unified threads) for aircraftCurrent
BS 2A 174:1962Specification for 100° countersunk head corrosion-resisting steel bolts (Unified threads) for aircraftWithdrawn
BS A 232:1968Specification for 100° countersunk head steel bolts (160 000 lbf/in2 (110 hbar) with Torq-set recesses)Current
BS A 211:1961Specification for 100° countersunk head steel bolts (Unified threads and cruciform recesses) for aircraftCurrent
BS 2A 173:1962+A7:2012Specification for 100° Countersunk head steel bolts (Unified threads), cadmium plated, for aircraftCurrent
BS 2A 230:1974Specification for 100° countersunk head steel bolts [1100 MPa with Hi-torque speed drive recesses]Current
BS A 266; A 267 [...]:1977Specification for 100° countersunk head titanium alloy bolts 160 000 lbf/in2 (1100 MPa) with Hi-torque speed drive recessesWithdrawn
BS A 120:1954Specification for 90° countersunk head corrosion-resisting steel bolts (UNF threads) for aircraftWithdrawn
BS A 119:1954Specification for 90° countersunk head steel bolts (UNF threads) for aircraftWithdrawn
BS 4A 169:2002Specification for aluminium alloy bolts (Unified hexagons and Unified threads) for aircraftCurrent
BS 3A 169:1962Specification for aluminium alloy bolts (Unified hexagons and Unified threads) for aircraftWithdrawn
BS 2A 61:1962Specification for aluminium alloy hexagonal headed bolts (B.A. and B.S.F. threads) for aircraftCurrent
BS 3A 170:1962Specification for aluminium alloy mushroom head bolts (Unified threads) for aircraftWithdrawn
BS 3A 171:1962Specification for aluminium alloy pan head bolts (Unified threads) for aircraftCurrent
BS 4A 170:1999+A1:2012Specification for aluminium alloy, mushroom-headed, slotted drive, bolts (unified thread)Current
BS A 31-54:1951+A6:2012Specification for British Association (B.A.) low tensile screws and nuts for aeronautical purposesCurrent, Work in Hand
BS 4A 111:1993Specification for cadmium-plated steel bolts (Unified hexagons and Unified threads) with close tolerance shanksCurrent
BS 3A 212:1993Specification for cadmium-plated steel bolts, 55/65 tonf/in2 (Unified hexagons, 3A Unified threads and close tolerance shanks)Withdrawn
BS 2A 59:1962Specification for cadmium-plated steel hexagonal-headed bolts (B.A. and B.S.F. threads) with close tolerance shanks for aircraftCurrent
BS 2A 60:1962Specification for cadmium-plated steel hexagonal-headed shear bolts (B.S.F. threads) for aircraftCurrent
BS 4A 112:1992Specification for cadmium-plated steel shear bolts (Unified hexagons and Unified threads)Current
BS 4A 113:1999+A1:2012Specification for cadmium-plated, mushroom-headed, unified-thread, slotted drive bolts Current
BS 3A 104:1962Specification for corrosion-resisting steel bolts (Unified hexagons and Unified threads) for aircraftWithdrawn
BS 4A 104:2002+A2:2012Specification for corrosion-resisting steel bolts (Unified hexagons and Unified threads), strength class 880 MPa, for aircraftCurrent
BS 2A 26:1962Specification for corrosion-resisting steel hexagonal-headed bolts (B.A and B.S.F. threads) for aircraftCurrent
BS 3A 114:1962Specification for corrosion-resisting steel mushroom head bolts (Unified threads) for aircraftWithdrawn
BS 4A 114:1999+A2:2015Specification for corrosion-resisting steel, mushroom-headed, slotted-drive, bolts, strength class 880 MPaCurrent
BS SP 164:1978Specification for design and performance requirements for turnlock, stud-type panel fasteners (metric series)Current
BS SP 114:1955+A5:2013Specification for Eye bolts (unified threads) for aircraftCurrent
BS 3A 100:1991Specification for general requirements for bolts and free running nuts of tensile strength not exceeding 1249 MPaWithdrawn
BS 4A 100:2003Specification for general requirements for bolts and free running nuts of tensile strength not exceeding 1249 MPaCurrent
BS A 101:1969+A3:2012Specification for general requirements for titanium boltsCurrent
BS A 287; A 288 [...]:1982Specification for hexagon socket head cap screws. Metric seriesWithdrawn
BS 2A 229:1972Specification for hexagonal head steel bolts 160000 lbf/in2 (1100/MPa)Current
BS A 260; A 261 [...]:1976Specification for metric screwsWithdrawn
BS 2A 260-2A 265:2010Specification for pan and 100° countersunk slotted head screws with ISO metric screw threadsCurrent
BS EN 2364:1989Specification for pins, shear headed, close toleranceCurrent
BS A 300:1989Specification for procurement of alloy steel bolts with strength classification 1 100 MPa and MJ threadsCurrent
BS A 274:1981Specification for procurement of alloy steel bolts, metric, with a minimum tensile strength of 1100 MPaCurrent
BS A 299:1989Specification for procurement of alloy steel protruding head bolts with strength classification 1 250 MPa and MJ threadsWithdrawn
BS A 401-420:2015Specification for screws, pan and 100° countersunk head, hexalobular drive recess (unified threads below ¼ inch) in various materialsCurrent
BS 3A 102:1962Specification for steel bolts (Unified hexagons and Unified threads) for aircraftWithdrawn
BS 4A 102:2002+A2:2012Specification for steel bolts (Unified hexagons and Unified threads) for aircraft Current
BS 3A 108:1962Specification for steel bolts (Unified hexagons and Unified threads) with close tolerance shanks for aircraftCurrent
BS 3A 228:1979Specification for steel double hexagon bolts 1250 MPa (180 000 lbf/in2) for aircraftWithdrawn
BS 4A 228:1997Specification for steel double hexagon bolts. 1250 MPa (180,000 lbf/in2) for aircraftCurrent
BS A 226:1965Specification for steel hexagon head bolts (short thread: Class 3A)Current
BS 2A 30:1962Specification for steel hexagonal-headed bolts (B.A. and B.S.F threads) with close tolerance shanks for aircraftWithdrawn
BS 2A 25:1962Specification for steel hexagonal-headed bolts (B.A. and B.S.F. threads) for aircraftCurrent
BS 2A 57:1962Specification for steel hexagonal-headed shear bolts (B.S.F. threads) for aircraftWithdrawn
BS 3A 113:1962Specification for steel mushroom head bolts (Unified threads) for aircraftWithdrawn
BS A 227:1965Specification for steel pan head bolts (short thread: Class 3A)Current
BS 3A 116:1962Specification for steel pan head bolts (Unified threads) for aircraftWithdrawn
BS 3A 109:1985Specification for steel shear bolts (Unified hexagons and Unified threads)Current
BS A 296:1986Specification for tolerances of form and position for bolts and screws. Metric seriesWithdrawn
BS G 203:1967Specification for Unified screws with captive facing and locking washersCurrent
BS A 254; A 255 [...]:1976Specification. Hexagonal head titanium alloy bolts 160 000 lbf/in2 (1100 MPa)Current
BS A 55 AND 56:1951+A3:2012Specifications for grub screws for aeronautical purposesCurrent
BS 2A 204; 2A 206 [...]:1963Specifications for machine screws and nuts (Unified threads) below ¼ inch for aeronautical purposesCurrent, Work in Hand
BS SP 128 to 133:1965Specifications for wood screws for aircraftWithdrawn
BS 4A 116:2012Steel pan head bolts (Unified threads), cadmium plated, for aircraftCurrent
BS ISO 9749:2000Stud-ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loadsCurrent

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