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Standards in development (378)

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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 5306-3 Fire extinguishing installations and equipment on premises Part 3: Commissioning and maintenance of portable fire extinguishers – Code of practiceIdea
BS EN 12312-12 Aircraft ground support equipment - Specific requirements Part 12: Potable water service equipmentTechnical Review
BS EN 12312-13 Aircraft ground support equipment - Specific requirements Part 13: Lavatory service equipmentTechnical Review
BS EN 12312-3 Aircraft ground support equipment - Specific requirements Part 3: Conveyor belt vehiclesApproval
BS EN 12312-6 Aircraft ground support equipment - Specific requirements Part 6: Deicers and deicing/antiicing equipmentTechnical Review
BS EN 12312-8 Aircraft ground support equipment - Specific requirements Part 8: Maintenance stairs and platformsPublic Comment
BS EN 16602-10 Space product assurance - Product assurance managementPublic Comment
BS EN 16602-70 Space product assurance - Materials, mechanical parts and processesPublication
BS EN 16602-70-12 Space product assurance - Design rules for printed circuit boardsPublication
BS EN 16602-70-14 CorrosionPublic Comment
BS EN 16602-70-39 Space product assurance - Welding of metallic materials for flight hardwarePublic Comment
BS EN 16602-70-54 Space product assurance - Ultracleaning of flight hardwarePublic Comment
BS EN 16603-10 Space engineering - System engineering general requirementsApproval
BS EN 16603-10-24 Space engineering - Interface managementPublic Comment
BS EN 16603-20-01 Space engineering - Multipaction, design and testPublication
BS EN 16603-20-20 Space engineering - Interface requirements for electrical powerPublic Comment
BS EN 16603-50-15 prEN 16603-50-15, Space engineering - CANbus extention protocolPublic Comment
BS EN 16603-70-41 Space engineering - Telemetry and telecommand packet utilizationPublic Comment
BS EN 16803-1 Space - Use of geo-positioning services for navigation and localization applications Part 1: Minimum Operational Performances definition methodology for GNSS-based positioning terminals used in road transport applicationsPublication
BS EN 17030 Image processing levelsPublic Comment
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 2285 Bushes, plain, aluminium alloy, with self-lubricating liner - Dimensions and loadsTechnical Review
BS EN 2286 Bushes, flanged aluminium alloy, with self-lubricating liner - Dimensions and loadsTechnical Review
BS EN 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 2714-002 Aerospace series - Cables, electrical, single and multicore for general purpose - Operating temperatures between - 55 °C and 260 °C Part 002: Screened and jacketed - GeneralApproval
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 3-8 Portable fire extinguishers Part 8: Additional requirements to EN 3-7 for the construction, resistance to pressure and mechanical tests for extinguishers with a maximum allowable pressure equal to or lower than 30 barPublic Comment
BS EN 3105 Aerospace series Sealants Test methods Determination of the corrosive effect of sealants on metallic materialsAccepted
BS EN 3110 Aerospace series. Sealants. Method of manufacture of moulded plates.Idea
BS EN 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 3572 PTFE flexible hose assembly with convoluted inner tube and titanium 8 degrees 30 mn coupling - Product standardPublication
BS EN 3646-005 Aerospace series - Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous -Part 005: Receptacle, hermetic, square flange mounting -Product standardApproval
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 testPublication
BS EN 3745-516 Aerospace series - Fibres and cables, optical, aircraft use - Test methods Part 516: Severe cable bend testPublication
BS EN 3745-517 Aerospace series - Fibres and cables, optical, aircraft use - Test methods Part 517: Cable tie clamping testPublication
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 4107 Aerospace series Non-metallic materials Structural adhesive systems Foaming adhesives Technical specificationAccepted
BS EN 4165-001:2015/Cor 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 4165-013 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 4165-024 Aerospace Series - Connector, electrical, rectangular, modular - Operating temperatures 175°C continuous Part 024: Single module Plug - Product standardApproval
BS EN 4165-025 Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature 175 °C continuous Part 025: Module receptacle - Product NormApproval
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 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 4531-001 Aerospace series - Connectors, optical, circular, single and multipin, coupled by threaded ring - Flush contacts Part 001 : Technical specificationPublication
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 standardPublication
BS EN 4604-010 Aerospace series - Cable, electrical, for signal transmission Part 010 : Cable, coaxial, light weight, 50 Ohms, 200 °C, type KX (light WD) - Product standardTechnical Review
BS EN 4644-002 Aerospace series - Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C continuous Part 002: Specification of performance and contact arrangementsApproval
BS EN 4644-142 Aerospace series - Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous Part 142: Size 4 receptacle for rack and panel application - Product standardApproval
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: MaterialPublication
BS EN 4708-101 Aerospace series - Sleeving, heat-shrinkable, for binding, insulation and identification Part 101: Polyolefin sleevingTechnical Review
BS EN 4727 Aerospace series - Standardized passenger seat weight informationApproval
BS EN 4730 Aerospace series - Anthropometric dimensioning of aircraft seatsPublication
BS EN 4801 Aerospace series - Flange couplings - Swivel flange with 3 fastening holes, in heat resisting steel - Inch seriesApproval
BS EN 4802 Aerospace series - Flange couplings - Swivel flange with 3 fastening holes, in nickel alloy - Inch seriesApproval
BS EN 4803 Aerospace series - Flange couplings - Swivel flange with 4 fastening holes, in heat resisting steel - Inch seriesApproval
BS EN 4804 Aerospace series - Flange couplings - Swivel flange with 4 fastening holes, in nickel alloy - Inch seriesApproval
BS EN 4805 Aerospace series - Flange couplings - Weld coupling, Straight, in heat resisting steel - Inch seriesApproval
BS EN 4806 Aerospace series - Flange couplings - Weld coupling, Straight, in nickel alloy - Inch seriesApproval
BS EN 4807 Aerospace series - Flange couplings - Weld coupling, 90° elbow, in heat resisting steel - Inch seriesApproval
BS EN 4808 Aerospace series - Flange couplings - Weld coupling, 90° elbow,in nickel alloy - Inch seriesApproval
BS EN 4809 Aerospace series - Flange couplings - Gasket seal with fluorocarbon seal on aluminium plate with 3 fastening holes, - Inch seriesApproval
BS EN 4810 Aerospace series - Flange couplings - Gasket seal with nickel alloy C seal on heat resisting steel plate with 3 fastening holes, - Inch seriesApproval
BS EN 4811 Aerospace series - Flange couplings - Gasket seal with fluorocarbon seal on aluminium plate with 4 fastening holes - Inch seriesApproval
BS EN 4812 Aerospace series - Flange couplings - Gasket seal with nickel alloy C seal on heat resisting steel plate with 4 fastening holes - Inch seriesApproval
BS EN 4813 Aerospace series - Flange couplings - Cap, in heat resisting steel - Inch seriesApproval
BS EN 4814 Aerospace series - Flange couplings up to 21 000 kPa - Technical specification - Inch seriesApproval
BS EN 4816 Aerospace series - Flange couplings - Gasket seal with nickel alloy C seal - Technical specification - Inch seriesApproval
BS EN 4827 Aerospace series - Hexavalent chromium free anodizing and sealing of aluminium and aluminium alloysPublication
BS EN 6029 Aerospace series - Rod-ends, adjustable, single fork with UNJ threaded shank min. engagement: 1,5 x thread diameter in corrosion resisting steel - Dimensions and loads - Inch seriesPublication
BS EN 6059-202 Aerospace series - Electrical cables, installation - Protection sleeves - Test methods Part 202: Dimensions and massApproval
BS EN 6059-307 Aerospace series - Electrical cables, installation - Protection sleeves - Test methods - Part 307: AgeingPublic Comment
BS EN 6101 Aerospace series - Rivet, 100° medium flush head, close tolerance - Inch seriesPublication
BS EN 6105 Aerospace series - Stud with shoulderPublication
BS EN 61347-1:2015+A1 Lamp controlgear - Part 1: General and safety requirementsPublic Comment
BS EN 61347-2-11:2002/A1 Lamp Controlgear - Part 2-11: Particular requirements for miscellaneous electronic circuits used with luminairesPublic Comment
BS EN 61347-2-13:2014/A1 Lamp controlgear - Part 2-13: Particular requirements for d.c. or a.c. supplied electronic controlgear for LED modulesPublication
BS EN 61347-2-14 Lamp controlgear - Part 2-14: Particular requirements for d.c. and/or a.c. supplied electronic controlgear for fluorescent induction lampsPublic Comment
BS EN 61347-2-3:2011+A1 Lamp control gear - Part 2-3: Particular requirements for a.c. and/or d.c. supplied electronic control gear for fluorescent lampsPublication
BS EN 61347-2-7:2012/A1 Lamp controlgear - Part 2-7: Particular requirements for battery supplied electronic controlgear for emergency lighting (self-contained)Accepted
BS EN 61347-2-9 Ed 2.0/A1 Lamp controlgear – Part 2-9: Particular requirements for electromagnetic controlgear for discharge lamps(excluding fluorescent lamps)Idea
BS EN 6138 Aerospace series - Cap, protective, non metallic for fitting ends ? 3 000 PSI hydraulic systemsTechnical Review
BS EN 62384 Ed 2.0 DC or AC supplied electronic control gear for LED modules - PerformancerequirementsAccepted
BS EN 62386-102 Ed 2.0/A1 Digital addressable lighting interface – Part 102: General requirements – Control gearAccepted
BS EN 62386-103 Ed 1.0/A1 Digital addressable lighting interface – Part 103: General requirements – Control devicesAccepted
BS EN 62386-207 Digital addressable lighting interface - Part 207: Particular requirements for control gear - LED modules (device type 6)Accepted
BS EN 62386-216 Digital addressable lighting interface - Part 216: Particular requirements for control gear - Load referencing (device type 15)Public Comment
BS EN 62386-217 Digital addressable lighting interface - Part 217: Particular requirements for control gear - Thermal gear protection (device type 16)Accepted
BS EN 62386-218 Digital addressable lighting interface - Part 218: Particular requirements for control gear - Dimming Curve Selection (device type 17)Accepted
BS EN 62386-220 Digital addressable lighting interface - Part 220: Particular requirements for control gear - Centrally Supplied DC Emergency Operation (device type 19)Accepted
BS EN 62386-221 Digital addressable lighting interface - Part 221: Particular requirements for control gear - Load Shedding (device type 20)Public Comment
BS EN 62386-222 Digital addressable lighting interface - Part 222: Particular requirements for control gear - Thermal lamp protection (device type 21)Accepted
BS EN 62386-224 Digital addressable lighting interface - Part 224: Particular requirements for control gear - Integrated light source (device type 23)Accepted
BS EN 62386-301 Digital addressable lighting interface - Part 301: General requirements - Input devices - Push buttons and binary inputsPublic Comment
BS EN 62386-302 Digital addressable lighting interface - Part 302: Particular requirements - Input devices - Absolute input devicesPublic Comment
BS EN 62386-303 Digital addressable lighting interface - Part 303: Particular requirements - Input devices - Occupancy sensorPublic Comment
BS EN 62386-304 Digital addressable lighting interface - Part 304: Particular requirements - Input devices - Light sensorPublic Comment
BS EN 62386-333 Digital addressable lighting interface - Part 333: Particular requirements for control devices - Manual Configuration (feature type 33)Public Comment
BS EN 62442-1 Ed1.0/A1 Energy performance of lamp controlgear – Part 1: Controlgear for fluorescent lamps – Method of measurement to determine the total input power of controlgear circuits and the efficiency of the controlgearPublic Comment
BS EN 62442-1:2011/A11 Energy performance of lamp controlgear - ,, Part 1: Controlgear for fluorescent lamps - Method of measurement to determine the total input power of controlgear circuits and the efficiency of the controlgearIdea
BS EN 62442-2 Ed1.0/A1 Energy performance of lamp controlgear – Part 2: Controlgear for high intensity discharge lamps (excluding fluorescent lamps) - Method of measurement to determine the efficiency of the controlgearPublic Comment
BS EN 62442-2:014/A11 Energy performance of lamp controlgear - ,, Part 2: Controlgear for high intensity discharge lamps (excluding fluorescent lamps) - Method of measurement to determine the efficiency of the controlgear ,,Idea
BS EN 62442-3 Ed1.0/A1 Energy performance of lamp controlgear – Part 3: Controlgear for halogen lamps and LED modules - Method of measurement to determine the efficiency of the controlgearPublic Comment
BS EN 62442-3:2014/AA Energy performance of lamp controlgear - Part 3: Controlgear for halogen lamps and LED modules - Method of measurement to determine the efficiency of the controlgearIdea
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 9100 Quality Management Systems – Requirements for Aviation, Space and andDefence OrganizationsPublic Comment
BS EN 9101 Quality management systems - Audit requirements for aviation, space and defense organizationsPublic Comment
BS EN 9104-003 Aerospace series - Quality management systems Part 003: Requirements for Aviation, Space, and Defense Auditor Training Development, Competence, and AuthenticationPublic Comment
BS EN 9107 Aerospace series - Quality systems - Direct Delivery Authorization - Guidance for Aerospace CompaniesPublic Comment
BS EN 9110 Aerospace series - Quality Management Systems – Requirements for Aviation Maintenance OrganizationsPublic Comment
BS EN 9115 Quality Management Systems - Requirements for Aviation, Space and Defence Organizations - Deliverable SoftwarePublic Comment
BS EN 9117 Aerospace Series - Delegated Product Release VerificationPublic Comment
BS EN 9120 Aerospace series - Quality Management Systems – Requirements for Aviation, Space and Defense DistributorsPublic Comment
BS EN 9130 Quality systems - Record retentionPublication
BS EN 9132 Aerospace series - Data Matrix Quality Requirements for Parts MarkingTechnical Review
BS EN 9132 Aerospace series - Quality management systems - Data Matrix Quality Requirements for Parts MarkingApproval
BS EN 9133 Aerospace Series – Qualification Procedure for Aerospace StandardProductsPublic Comment
BS EN 9136 Aerospace Series – Root Cause Analysis and Problem Solving (9S Methodology)Public Comment
BS EN 9138 Aerospace Series – Quality Management Systems - Statistical ProductAcceptance RequirementsPublic Comment
BS EN 9139 Aerospace Series - Quality Management Systems - Development of Process-Based Bodies of KnowledgePublic Comment
BS EN 9145 Aerospace Series – Requirements for Advanced Product Quality Planning and Production Part Approval ProcessPublic Comment
BS EN 9146 Aerospace series - Foreign Object Debris/Damage (FOD) Prevention Program - Requirements for Aviation, Space and Defense OrganizationsAccepted
BS EN 9162 Aerospace Operator Self-Verification ProgramsPublic Comment
BS EN 9223-100 Programme Management — Configuration Management — Part 100: A guide for the application of the principles of configuration managementPublication
BS EN 9223-101 Programme Management — Configuration Management — Part 101: Configuration identificationPublication
BS EN 9223-102 Programme Management — Configuration Management — Part 102: Configuration status accountingPublication
BS EN 9223-103 Programme Management — Configuration Management — Part 103: Configuration Verifications, Reviews and AuditsPublication
BS EN 9223-104 Programme Management — Configuration Management — Part 104: Configuration ControlPublication
BS EN 9223-105 Programme Management — Configuration Management — Part 105: GlossaryPublication
BS EN 9250 organisations - GeneralrequirementsAccepted
BS EN 9251 Organisations QualificationStandardAccepted
BS EN 9252 management and approvalAccepted
BS EN 9253 Aerospace series - Surveillance of Design SuppliersPublic Comment
BS EN 9300-002 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 002: RequirementsPublic Comment
BS EN 9300-005 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 005: Authentication and VerificationPublic Comment
BS EN 9300-007 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 007: Terms and ReferencesPublic Comment
BS EN 9300-015 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 115: explicit CAD assembly structurePublic Comment
BS EN 9300-100 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 100: Common concepts for Long term archiving and retrieval of CAD 3D mechanical informationPublic Comment
BS EN 9300-110 LOng Term Archiving and Retrieval of digital technical product documenta tion such as 3D, CAD and PDM data. PART 110: CAD mechanical 3D Explicit geometry informationPublic Comment
BS EN 9300-120 Aerospace series - LOTAR - LOng Term Archiving and Retrieval of digital technical product documentation such as 3D, CAD and PDM data Part 120: CAD 3D explicit geometry with product and manufacturing informationPublic Comment
BS EN 9300-200 LOng Term Archiving and Retrieval of digital technical productdocumentation such as 3D-CAD and PDM data Part 200: Common Concepts for Long term Archiving and Retrieval of Product Structure InformationPublic Comment
BS ENISO 17666 Space systems - Risk managementApproval
BS IEC 62386-101 Ed2.0 Amd 1 Digital addressable lighting interface – Part 101: General requirements - System componentsPublic Comment
BS IEC 62386-332 Ed1.0 Digital addressable lighting interface - Part 332: Particular requirements - Input control devices - FeedbackPublic Comment
BS ISO 11231 Space systems - Probabilistic risk assessment (PRA)Accepted
Opens a new windowBS ISO 11532 Aircraft ground equipment - Graphical symbolsPublic Comment
BS ISO 14624-4 Space systems - Safety and compatibility of materials Part 4: Determination of upward flammability of materials in pressurized gaseous oxygen or oxygen-enriched environmentsAccepted
BS ISO 1464 Aerospace - Tripod jacks - Clearance dimensionsPublic Comment
BS ISO 15872 Aerospace - UNJ threads - GaugingPublic Comment
BS ISO 16049-2 Air cargo equipment - Restraint straps Part 2: Utilization guidelines and lashing calculationsAccepted
BS ISO 21494 Space systems - Magnetic testingIdea
BS ISO 21886 Space systems - Configuration managementIdea
BS ISO 43 Aircraft - Jacking padsPublication
BS ISO 8267-2 Aircraft - Tow bar attachment fittings interface requirements Part 2: Regional aircraftPublic Comment
BS ISO 9667 Aircraft ground support equipment - Tow barsPublic Comment
BS ISO 10537 Space data and information transfer systems - Encapsulation servicePublic Comment
BS ISO 10842 Aircraft - Ground service connections - Locations and typesPublic Comment
BS ISO 11601 Fire fighting - Wheeled fire extinguishers - Performance and constructionPublic Comment
BS ISO 12604-1 Aircraft ground handling - Checked baggage - Mass and dimensions Part 1: Title missingPublic Comment
BS ISO 16004 Aircraft ground equipment - Passenger boarding bridge or transfer vehicle - Requirements for interface with aircraft doorsApproval
BS ISO 16157 Human-Life Activity Support Systems and Equipment Integration in Space Flight - Techno-Medical Requirements for Space Vehicle Human Habitation EnvironmentsAccepted
BS ISO 16192 Space systems - Experience gained in space projects (Lessons learned) - Principles and guidelinesPublic Comment
BS ISO 16709 Realtime solar activity and space environment information for spacecraft operationPublic Comment
BS ISO 16726 Human-Life Activity Support Systems and Equipment Integration in Space Flight - Techno-Medical Requirements for Space Vehicle Human Habitation Environments - Requirements for the air quality affected by harmful chemical contaminantsAccepted
BS ISO 17355 Space data and information transfer systems - CCSDS file delivery protocolAccepted
BS ISO 17540 Space systems - Liquid rocket engines and test stands - Terms and definitionsPublication
BS ISO 17763 Space systems - Human-life activity support systems and equipment integration in space flightAccepted
BS ISO 17770 Space systems - Cube satellites (CubeSats)Approval
BS ISO 18257 Space systems - Semiconductor integrated circuits for space applications - Design requirementsApproval
BS ISO 18322 accreditation of space test centers and laboratoriesPublic Comment
BS ISO 18440 Space data and information transfer systems - Space link extension - Internet protocol for transfer servicesApproval
BS ISO 18441 Space data and information transfer systems - Space link extension - Application program interface for transfer services - Core specificationApproval
BS ISO 18442 Space data and information transfer systems - Space link extension - Application program interface for return all frames serviceApproval
BS ISO 18443 Space data and information transfer systems - Space link extension - Application program interface for return channel frames serviceApproval
BS ISO 18444 Space data and information transfer systems - Space link extension - Application program interface for return operational control fields serviceApproval
BS ISO 18445 Space data and information transfer systems - Space link extension - Application program interface for the forward CLTU serviceApproval
BS ISO 18446 Space data and information transfer systems - Space link extension - Application program interface for the forward space packet serviceApproval
BS ISO 18667 Space Systems - Requirements for the management of capability-based Safety, Dependability, and Quality Assurance (SD&QA) programmeAccepted
BS ISO 18676 Space Systems - Guidelines for the management of systems engineering processesAccepted
Opens a new windowBS ISO 19683 Space systems - Design qualification and acceptance tests of small-scale satellite and units seeking low-cost and fast-deliveryPublic Comment
BS ISO 19826 Space systems - Programme management --Management of product characteristicsPublic Comment
BS ISO 19923 Space environment (natural and artificial) - Spacecraft potential estimation in worst case environmentPublic Comment
BS ISO 19924 Space systems - Acoustic testingAccepted
BS ISO 19971 Space systems - Spacecraft and launch vehicle Combined Operation Plan (COP) at launch site - General formatAccepted
BS ISO 20188 Space systems - Product assurance requirements for commercial satellitesAccepted
BS ISO 20584 Space environment (natural and artificial) - Spacecraft charging - Earth orbitIdea
BS ISO 20780 Space systems - Fiber optic components - Design and verification requirementsAccepted
BS ISO 20892 Space systems - Launch complex - Modernization process: General requirementsAccepted
BS ISO 20893 Space systems - Prevention of break-up of orbital launch stagesIdea
BS ISO 20894 Aircraft - LED based taxiing light system - General requirementsIdea
BS ISO 20930 Space systems - Calibration requirements for satellite-based passive microwave sensorsIdea
BS ISO 20949 Aircraft - Smart Contactor - General RequirementsIdea
BS ISO 20991 Space systems - Requirements for small spacecraftAccepted
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 21095 Space systems - Procedure for limiting risk of re-entering spacecraft and launch vehicle orbital stagesIdea
BS ISO 21100 Air cargo unit load devices - Performance requirements and test parametersPublic Comment
BS ISO 21323 Space data and information transfer systems - CCSDS Bundle protocol specificationApproval
BS ISO 21324 Space data and information transfer systems - Space data link security protocolApproval
BS ISO 21442 Space systems - General requirements for control engineeringIdea
BS ISO 22645 Space data and information transfer systems - TM (telemetry) space data link protocolApproval
BS ISO 22664 Space data and information transfer systems - TC (telecommand) space data link protocolApproval
BS ISO 22666 Space data and information transfer systems - AOS (advanced orbiting systems) space data link protocolApproval
BS ISO 23038 Space systems - Space solar cells - Electron and proton irradiation test methodsAccepted
BS ISO 24917 Space systems - General test requirements for launch vehiclesAccepted
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 7165 Fire fighting - Portable fire extinguishers - Performance and constructionPublic 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 7718-1 Aircraft - Passenger doors interface requirements for connection of passenger boarding bridge or passenger transfer vehicles Part 1: Main deck doorsApproval
BS ISO 7718-2 Aircraft - Passenger doors interface requirements for connection of passenger boarding bridge or passenger transfer vehicles Part 2: Upper deck doorsApproval
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 8267-2:2015/Amdd 1 Aircraft - Tow bar attachment fittings interface requirements Part 2: Regional aircraft - Amendmentd 1Public Comment
BS ISO 9788 Air cargo equipment - Cast components of double stud fitting assembly with a load capacity of 22 250 N (5 000 lbf), for aircraft cargo restraintPublic Comment
BS SP 94:1964/Amd 3 Specification for bronze oil-retaining bushes and thrust washers - For aircraftApproval
BSEN 9300-010 Aerospace series - LOTAR - LOng Term Archiving and Retrieval of digital technical product documentation such as 3D, CAD and PDM data. PART 010: Overview Data FlowPublication
BSEN9300-1 Long Term Archiving and Retrieval of digital technical productdocumentat ion such as 3D, CAD and PDM data within the aerospaceindustry Part 1 StructurePublic Comment
BSEN9300-2 Long Term Archiving and Retrieval of digital technical productdocumentat ion such as 3D, CAD and PDM data within the aerospaceindustry Part 2 RequirementsPublic Comment
BSEN9300-4 Long Term Archiving and Retrieval of digital technical productdocumentat ion such as 3D, CAD and PDM data within the aerospaceindustry Part 4 Description MethodsPublic Comment
PD CEN/TR 4541 Instruction for the installation of airframe bearingsPublic Comment
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
PD ISO/TR 21891 Aerospace electrical requirements - Insulating, heat shrink, sleeves and moulded shapses - Specification for aircraft useAccepted
PD ISO/TR 20590 Space systems - Debris mitigation design and operation manual for launch vehicle orbital stagesAccepted
PD ISO/TR 20891 Space systems - Space batteries - Guidelines for easing in-flight health assessmentIdea
PD ISO/TS 18667 Space Systems - Requirements for the management of capability-based Safety, Dependability, and Quality Assurance (SD&QA) programmeAccepted

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Published standards (119)

Sort by: Reference | Title | Status

Standard referenceNameStatus
BS EN 3375-009:2016Aerospace series. Cable, electrical, for digital data transmission - Single braid. CAN Bus. 120 ohms. Type WX. Product standardCurrent
BS EN 3375-012:2013Aerospace series. Cable, electrical, for digital data transmission - Single braid. Star Quad 100 ohms. 260°C. Type KH. Product standardCurrent
BS EN 3375-011:2015Aerospace series. Cable, electrical, for digital data transmission - Single braid. Star Quad 100 ohms. Light weight. Type KL. Product standardCurrent
BS EN 3375-007:2016Aerospace series. Cable, electrical, for digital data transmission - Double braid. 77 Ohms. Type WW. Product standardCurrent
BS EN 4641-100:2015Aerospace series. Cables, optical 125 µm diameter cladding - Tight structure 62,5/125 µm core GI fibre 1,8 mm outside diameter. Product standardCurrent
BS EN 4641-101:2015Aerospace series. Cables, optical 125 µm diameter cladding - Tight structure 62,5 µm core GI fibre 0,9 mm outside diameter. Product standardCurrent
BS EN 4644-014:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Receptacle, size 1, with ground block, class B and F. Product standardCurrent
BS EN 4644-011:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Plug, size 1, without mounting holes, class A, C and E. Product standardCurrent
BS EN 4644-001:2012Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Technical specificationCurrent, Work in Hand
BS EN 4644-133:2011Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Size 3 receptacle for rack and panel application. Product standardWithdrawn
BS EN 4644-131:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Size 3 plug for rack and panel applications, class C and D. Product standardCurrent
BS EN 4644-013:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Plug, size 1, with ground block, without mounting holes, class B and F. Product standardCurrent
BS EN 4644-141:2016Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Size 4 plug for rack and panel applications, class C and D. Product standardCurrent
BS EN 4644-131:2011Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Size 3 plug for rack and panel applications. Product standard Withdrawn
BS EN 4644-003:2011Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Rectangular inserts. Product standard Withdrawn
BS EN 4644-133:2016Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Size 3 receptacle for rack and panel application, class C and D. Product StandardCurrent
BS EN 4644-201:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Locking and polarizing hardware. Product standardCurrent
BS EN 4644-012:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Receptacle, size 1, class A, C and E. Product standardCurrent
BS EN 4644-003:2016Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Rectangular inserts. Product standardCurrent
BS EN 4644-024:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Receptacle size 2, class A, C and E. Product standardCurrent
BS EN 4644-026:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Receptacle size 2 with ground block, class B and F. Product standardCurrent
BS EN 4644-025:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Receptacle, size 2, with flange, class A, C and E. Product standardCurrent
BS EN 4644-141:2011Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Size 4 plug for rack and panel applications. Product standardWithdrawn
BS EN 4644-002:2012Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Specification of performance and contact arrangementsCurrent, Work in Hand
BS EN 4644-023:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175°C (or 125°C) continuous - Plug, size 2, with ground block, class B and F. Product standardCurrent
BS EN 4644-022:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175°C (or 125°C) continuous - Plug, size 2, with mounting holes, class A, C and E. Product standardCurrent
BS EN 4644-021:2015Aerospace series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175°C (or 125°C) continuous - Plug, size 2, without mounting holes, class A, C and E. Product standardCurrent
BS EN 4644-142:2012Aerospace series. Connector, electrical and optical, rectangular,modular, rectangular inserts, operating temperature 175°C (or 125°C) continuous - Size 4 receptacle for rack and panel application. Product standardCurrent, Work in Hand
BS EN 4645-001:2010Aerospace series. Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder - Technical specificationCurrent
BS EN 4531-201:2016Aerospace series. Connectors, optical, circular, single and multipin, coupled by triple start threaded ring. Flush contacts - Optical contact for EN 4641 singlemode cable -55 °C to 125 °C. Product standardCurrent
BS EN 4701-002:2013Aerospace series. Connectors, optical, rectangular, modular, operating temperature 125 °C, for EN 4531-101 contacts - MaterialCurrent, Work in Hand
BS EN 4701-001:2014Aerospace series. Connectors, optical, rectangular, modular, operating temperature 125 °C, for EN 4531-101 contacts - Technical specificationCurrent
BS EN 4830-001:2015Aerospace series. Connectors, optical, rectangular, modular, operating temperature 125 °C, for EN 4639-10X contacts - Technical specificationCurrent
BS EN 4830-002:2015Aerospace series. Connectors, optical, rectangular, modular, operating temperature 125 °C, for EN 4639-10X contacts - Specification of performanceCurrent
BS EN 4701-001:2013Aerospace series. Connectors, optical, rectangular, modular, operating temperature 125°C, for EN 4531-101 contacts - Technical specificationWithdrawn
BS EN 4701-003:2013Aerospace series. Connectors, optical, rectangular, modular,operating temperature 125°C, for EN 4531-101 contacts - Module series 2. Product standardCurrent
BS EN 3716-004:2014Aerospace series. Connectors, single-way with triaxial interface for transmission of digital data - Solder plug and terminator. Product standardCurrent
BS EN 3197:2010Aerospace series. Design and installation of aircraft electrical and optical interconnection systemsCurrent, Work in Hand
BS EN 2591-227:2015Aerospace series. Elements of electrical and optical connection. Test methods - Partial discharges testCurrent
BS EN 2591-315:2015Aerospace series. Elements of electrical and optical connection. Test methods - Fluid resistanceCurrent
BS EN 2591-307:2012Aerospace series. Elements of electrical and optical connection. Test methods - Salt mistCurrent
BS EN 2591-402:2012Aerospace series. Elements of electrical and optical connection. Test methods - ShockCurrent
BS EN 3745-515:2012Aerospace series. Fibres and cables, optical, aircraft use. Test methods - Buffer insertion force Current
BS EN 3745-516:2012Aerospace series. Fibres and cables, optical, aircraft use. Test methods - Severe cable bend test Current, Work in Hand
BS EN 3745-517:2012Aerospace series. Fibres and cables, optical, aircraft use. Test methods - Cable tie clamping test Current, Work in Hand
BS EN 4660-003:2011Aerospace series. Modular and open avionics architectures - Communications/NetworkCurrent, Work in Hand
BS EN 4660-004:2011Aerospace series. Modular and open avionics architectures - PackagingCurrent, Work in Hand
BS EN 4660-005:2011Aerospace series. Modular and open avionics architectures - SoftwareCurrent, Work in Hand
BS EN 4660-002:2011Aerospace series. Modular and open avionics architectures - Common functional modulesCurrent
BS EN 4660-001:2011Aerospace series. Modular and open avionics architectures - ArchitectureCurrent
BS M 90:1997Aircraft ground support equipment. Self-propelled passenger stairs for large capacity aircraft. Functional requirementsCurrent
BS 4N 100-5:1999Aircraft oxygen systems and equipment - Guide to fire and explosion hazards associated with oxygenWithdrawn
BS 4N 100-4:1999Aircraft oxygen systems and equipment - Guide to the physiological factorsCurrent
BS 4N 100-3:1999Aircraft oxygen systems and equipment - Testing of equipment and systemsCurrent
BS 4N 100-1:1999Aircraft oxygen systems and equipment - Design and installation Current
BS 4N 100-6:1999Aircraft oxygen systems and equipment - Guidance and recommendations on the selection of materials for use with oxygenCurrent
BS 4N 100-7:1999Aircraft oxygen systems and equipment - Guide to cleaning labelling and packagingWithdrawn
BS 5N 100-5:2006Aircraft oxygen systems and equipment - Guide to fire and explosion hazards associated with oxygen, including handling, storage and replenishmentCurrent
BS 4N 100-2:1999Aircraft oxygen systems and equipment. Tests for the compatibility of materials in the presence of oxygenCurrent
BS 3N 3:2000Breathing oxygen for airborne applicationsCurrent
BS 185-14:1972Glossary of aeronautical and astronautical terms - Radiocommunication and radiolocationCurrent
BS F 140:1991Glossary of parachute termsCurrent
BS EN 61347-2-6:2001Lamp controlgear - Particular requirements for d.c. supplied electronic ballasts for aircraft lightingWithdrawn
BS 2G 215-1:1985Nickel-chromium and nickel-aluminium thermocouple extension cables for aircraft - Specification for conductorsCurrent
BS EN 16603-50-04:2014Space engineering. Space data links. Telecommand protocols, synchronization and channel codingCurrent
BS EN 16602-70-20:2014Space product assurance. Determination of the susceptibility of silver-plated copper wire and cable to "red-plague" corrosionCurrent
BS EN 16602-70-18:2014Space product assurance. Preparation, assembly and mounting of RF coaxial cablesCurrent
BS G 152:1956Specification for a.c. electrically-operated artificial horizons for aircraftCurrent
BS N 6:1998Specification for aeromedical portable oxygen concentrator systems. General requirementsCurrent
BS 2G 112:1956Specification for air-driven directional gyroscopes for aircraftCurrent
BS G 118:1949Specification for aircraft magnetic compass, direct-readingCurrent
BS G 122:1949Specification for aircraft magnetic compass, remote-reading (gyro-stabilized)Current
BS G 123:1949Specification for aircraft magnetic compass, remote-reading (non-stabilized)Current
BS G 190:1964Specification for cabin altimeters for aircraftCurrent
BS G 201:1967Specification for counter and pointer pressure altimetersWithdrawn
BS 2G 201:1996Specification for counter and pointer pressure altimetersCurrent
BS G 226:1979Specification for counter and pointer, servo type, pressure altimeter systemsCurrent
BS N 5:1992Specification for crew portable protective breathing equipment for use during aircraft emergenciesCurrent
BS 2G 114:1953Specification for direct current ratiometer indicators for aircraftCurrent
BS 2G 135:1967Specification for electrically-heated pitot and pitotstatic pressure headsCurrent
BS N 4:1974Specification for full face mask assemblies for use in contaminated atmospheresWithdrawn
BS 2N 3:1990Specification for gaseous breathing oxygen supplied for airborne applicationWithdrawn
BS 3N 100:1985Specification for general design requirements for aircraft oxygen systems and equipmentWithdrawn
BS 3G 148:1981Specification for general purpose platinum temperature sensors for aircraftCurrent
BS G 217:1975Specification for general requirements for cockpit lighting controllersCurrent
BS 2N 2:1989Specification for general requirements for construction and performance of airborne chemical oxygen generatorsWithdrawn
BS 3G 100-0:1980Specification for general requirements for electrical equipment and indicating instruments for aircraft - IntroductionWithdrawn
BS 3G 100-1:1973Specification for general requirements for equipment for use in aircraft - Identification and declarationsWithdrawn
BS 3G 100-2.1:1973Specification for general requirements for equipment for use in aircraft. All equipment - ConstructionWithdrawn
BS 3G 100-2.3.12:1986Specification for general requirements for equipment for use in aircraft. All equipment - Fluid contaminationWithdrawn
BS 3G 100-2.2:1972Specification for general requirements for equipment for use in aircraft. All equipment - Magnetic influenceCurrent
BS 3G 100-2.3.10:1974Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Impact icingCurrent
BS 3G 100-2.3.9:1972Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Ice formationCurrent
BS 3G 100-2.3.2:1970Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Temperature-pressure requirementsCurrent
BS 3G 100-2.3.8:1972Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Salt mistCurrent
BS 3G 100-2.3.6:1972Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Acceleration requirementsCurrent
BS 3G 100-2.3.5:1972Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Explosion-proofnessCurrent
BS 3G 100-2.3.7:1972Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Tropical exposureCurrent
BS 3G 100-2.3.4:1972Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Differential pressure requirementsCurrent
BS 3G 100-2.3.3:1972Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Mould growthCurrent
BS 3G 100-2.3.12:1991Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Fluid contaminationCurrent
BS 3G 100-2.3.15:1978Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Change of temperatureWithdrawn
BS 3G 100-2.3.0:1972Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Standard test requirementsCurrent
BS 3G 100-2.3.11:1973Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Water-proofnessCurrent
BS 3G 100-2.3.14:1973Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Acoustic vibrationCurrent
BS 3G 100-2.3.1:1969Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - VibrationCurrent
BS 3G 100-2.3.13:1973Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions - Resistance to fire in designated fire zonesCurrent
BS 3G 101:1987Specification for general requirements for mechanical and electromechanical aircraft indicatorsCurrent
BS G 183:1963Specification for interconnections in analogue data transmission systems in aircraftCurrent
BS 2G 113:1956Specification for manifold pressure gauges for aircraftCurrent
BS 2N 1:1990Specification for oro-nasal oxygen mask assemblies for use in demand systemsWithdrawn
BS 7867:1997Specification for portable fire extinguishers for use in aircraftCurrent
BS G 240:1988Specification for pressure transducers for use on aircraftCurrent
BS 2G 117:1975Specification for pressure-driven airspeed indicatorsCurrent
BS 2G 182:1975Specification for pressure-driven machmeters for aircraftCurrent
BS 2G 111:1955Specification for rate of climb indicators for aircraftCurrent
BS G 234:1984Specification for self-aligning air flow angle transmitters for use on aircraftCurrent
BS 2G 115:1956Specification for sensitive altimeters for aircraftCurrent
BS G 125:1950Specification for turn and slip indicators for aircraft purposesCurrent

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