STD-EN 4XXXX

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• EN 4000:2001 Aerospace series – Metallic materials – Rules for the drafting and presentation of dimensional standards for metallic semi-finished products
• EN 4001:2007 Aerospace series – Aluminium alloy AL-P2024-T351 – Clad sheet and strip with improved chemical milling capability 1,6 mm = a = 6 mm
• EN 4002:2007 Aerospace series – Aluminium alloy AL-P2219-T81 – Sheet and strip 0,5 mm = a = 6 mm
• EN 4003:2006 Aerospace series – Aluminium alloy AL-P2219-T87 – Sheet and strip 0,5 mm = a = 6 mm
• EN 4004:2007 Aerospace series – Aluminium alloy AL-P3103-H16 – Sheet and strip 0,4 mm = a = 6 mm
• EN 4005:2007 Aerospace series – Aluminium alloy AL-P5052-O – Sheet and strip 0,3 mm = a = 6 mm
• EN 4006:2007 Aerospace series – Aluminium alloy AL-P6082-T4 or T42 – Sheet and strip 0,4 mm = a = 6 mm
• EN 4007:2005 Aerospace series – Aluminium alloy AL-P6082-T6 or T62 – Sheet and strip – 0,4 mm<="" td="">
• EN 4008-001:2006 Aerospace series – Elements of electrical and optical connection – Crimping tools and associated accessories – Part 001: Technical specification
• EN 4008-002:2006 Aerospace series – Elements of electrical and optical connection – Crimping tools and associated accessories – Part 002: List of product standards
• EN 4008-005:2006 Aerospace series – Elements of electrical and optical connection – Crimping tools and associated accessories – Part 005: Positioner for crimping tool M22520/2-01 – Product standard
• EN 4008-006:2006 Aerospace series – Elements of electrical and optical connection – Crimping tools and associated accessories – Part 006: Positioner for crimping tool M22520/7 – Product standard
• EN 4008-007:2011 Aerospace series – Elements of electrical and optical connection – Crimping tools and associated accessories – Part 007: Positioner for crimping tool M22520/2-01 – Product standard
• EN 4008-008:2011 Aerospace series – Elements of electrical and optical connection – Crimping tools and associated accessories – Part 008: Positioner for crimping tool M22520/7-01 – Product standard
• EN 4008-011:2006 Aerospace series – Elements of electrical and optical connection – Crimping tools and associated accessories – Part 011: Positioner for crimping tool M22520/2-01 – Product standard
• EN 4008-012:2006 Aerospace series – Elements of electrical and optical connection – Crimping tools and associated accessories – Part 012: Positioner for crimping tool M22520/2-01 – Product standard
• EN 4008-013:2006 Aerospace series – Elements of electrical and optical connection – Crimping tools and associated accessories – Part 013: Positioner for crimping tool M22520/2-01 – Product standard
• EN 4008-014:2006 Aerospace series – Elements of electrical and optical connection – Crimping tools and associated accessories – Part 014: Turret for crimping tool M22520/31-01 – Product standard
• EN 4008-015:2007 Aerospace series – Elements of electrical and optical connection – Crimping tool and associated accessories – Part 015: Positioner for crimping tool M22520/2-01 – Product standard
• EN 4008-017:2006 Aerospace series – Elements of electrical and optical connection – Crimping tools and associated accessories – Part 017: Head for crimping tool M22520/4-01 – Product standard
• EN 4009:2004 Aerospace series – Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) – Classification: 1 550 MPa (at ambient temperature) / 650 °C
• EN 40-1:1991 Lighting columns – Part 1: Definitions and terms
• EN 4011:2004 Aerospace series – Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated – Classification: 1 550 MPa (at ambient temperature) / 600 °C
• EN 4012:2004 Aerospace series – Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated – Classification: 1 550 MPa (at ambient temperature) / 425 °C
• EN 4013:2004 Aerospace series – Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated – Classification: 1 550 MPa (at ambient temperature) / 600 °C
• EN 4014:2004 Aerospace series – Inserts, thickwall, self-locking – Design standard
• EN 4015:2004 Aerospace series – Inserts, thickwall, self-locking – Installation and removal procedure
• EN 4017:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 90°
• EN 4018:2009 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 90° with thrust wire nut
• EN 4019:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 90° welded end
• EN 402:2003 Respiratory protective devices – Lung governed demand self-contained open-circuit compressed air breathing apparatus with full face mask or mouthpiece assembly for escape – Requirements, testing, marking
• EN 40-2:2004 Lighting columns – Part 2: General requirements and dimensions
• EN 4020:2009 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 90°, welded end with thrust wire nut
• EN 4021:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 90°, bulkhead
• EN 4022:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 90° bulkhead, welded end
• EN 4023:2010 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 45°
• EN 4024:2009 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 45° welded end with thrust wire nut
• EN 4025:2010 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 45°, bulkhead
• EN 4026:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees
• EN 4027:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees branch with thrust wire nut
• EN 4028:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees with thrust wire nut on run
• EN 4029:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees bulkhead branch
• EN 403:2004 Respiratory protective devices for self-rescue – Filtering devices with hood for escape from fire – Requirements, testing, marking
• EN 4030:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees bulkhead on run
• EN 4031:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Nut for welded ferrule
• EN 40-3-1:2013 Lighting columns – Part 3-1: Design and verification – Specification for characteristic loads
• EN 4032:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Thrust wire
• EN 4032:2001/AC:2003 Aerospace series – Pipe couplings 8°30′ in titanium alloy – Thrust wire
• EN 40-3-2:2013 Lighting columns – Part 3-2: Design and verification – Verification by testing
• EN 4033:2007 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in corrosion resisting steel – Diameter series 8 and 9, reduced internal radial clearance – Dimensions and loads
• EN 40-3-3:2013 Lighting columns – Part 3-3: Design and verification – Verification by calculation
• EN 4034:2007 Aerospace series – Bearings, airframe rolling – Double row self-aligning ball bearings with flanged outer ring in corrosion resisting steel, reduced internal radial clearance – Dimensions and loads
• EN 4035:2006 Aerospace series – Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy – Dimensions and loads
• EN 4036:2006 Aerospace series – Rod ends, adjustable with self-aligning double row ball bearing and threaded shank in corrosion resisting steel, reduced internal radial clearance – Dimensions and loads
• EN 40-4:2005 Lighting columns – Part 4: Requirements for reinforced and prestressed concrete lighting columns
• EN 404:2005 Respiratory protective devices for self-rescue – Filter self-rescuer from carbon monoxide with mouthpiece assembly
• EN 40-4:2005/AC:2006 Lighting columns – Part 4: Requirements for reinforced and prestressed concrete lighting columns
• EN 4040:2006 Aerospace series – Bearings, spherical plain in corrosion resisting steel with self-lubricating liner with wide inner ring – Elevated loads at ambient temperature – Dimensions and loads
• EN 4041:2006 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in corrosion resisting steel, with extended inner ring and flanged alignment bush – Dimensions and loads
• EN 4045:2001 Aerospace series – Capillary tubes, seamless in heat resisting alloys – Diameter 0,6 mm <= D <= 2 mm - Dimensions
• EN 4047:2004 Aerospace series – Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated – Classification: 1 550 MPa (at ambient temperature) / 600 °C – Technical specification
• EN 4048:2004 Aerospace series – Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated – Classification: 1 550 MPa (at ambient temperature) / 425 °C – Technical specification
• EN 4049-001:2006 Aerospace series – Thermocouple extension cable – Operating tempera-tures between – 65 °C to 260 °C – Part 001: Technical specification
• EN 4049-002:2005 Aerospace series – Thermocouple extension cable – Operating temperatures between – 65 °C to 260 °C – Part 002: General
• EN 4049-003:2006 Aerospace series – Thermocouple extension cable – Operating tempera-tures between – 65 °C to 260 °C – Part 003: Single core nickel chro-mium/nickel aluminium – Product standard
• EN 4049-004:2006 Aerospace series – Thermocouple extension cable – Operating tempera-tures between – 65 °C to 260 °C – Part 004: Two core nickel chro-mium/nickel aluminium shielded and jacketed – Product standard
• EN 405:2001+A1:2009 Respiratory protective devices – Valved filtering half masks to protect against gases or gases and particles – Requirements, testing, marking
• EN 40-5:2002 Lighting columns – Part 5: Requirements for steel lighting columns
• EN 4050-1:2012 Aerospace series – Test method for metallic materials – Ultrasonic inspection of bars, plates, forging stock and forgings – Part 1: General requirements
• EN 4050-2:2012 Aerospace series – Test method for metallic materials – Ultrasonic inspection of bars, plates, forging stock and forgings – Part 2: Performance of test
• EN 4050-3:2012 Aerospace series – Test method for metallic materials – Ultrasonic inspection of bars, plates, forging stock and forgings – Part 3: Reference blocks
• EN 4050-4:2012 Aerospace series – Test method for metallic materials – Ultrasonic inspection of bars, plates, forging stock and forgings – Part 4: Acceptance criteria
• EN 4051:2002 Aerospace series – Pipe couplings, 60°, spherical, in titanium alloy – Port connection
• EN 4054:2004 Aerospace series – Pipe couplings, loose flanges and seals – Seals in fluorocarbon rubber and armature in aluminium alloy – Technical specification
• EN 4056-001:2006 Aerospace series – Cable ties for harnesses – Part 001: Technical specification
• EN 4057-100:2006 Aerospace series – Cable ties for harnesses – Test methods – Part 100: General
• EN 4057-201:2005 Aerospace series – Cable ties for harnesses – Test methods – Part 201: Visual examination
• EN 4057-202:2005 Aerospace series – Cable ties for harnesses – Test methods – Part 202: Examination of mass and dimensions
• EN 4057-301:2005 Aerospace series – Cable ties for harnesses – Test methods – Part 301: Salt mist test
• EN 4057-302:2006 Aerospace series – Cable ties for harnesses – Test methods – Part 302: Flammability
• EN 4057-303:2005 Aerospace series – Cable ties for harnesses – Test methods – Part 303: Resistance to fluids
• EN 4057-304:2006 Aerospace series – Cable ties for harnesses – Test methods – Part 304: Loop tensile strength at maximum working temperature
• EN 4057-305:2005 Aerospace series – Cable ties for harnesses – Test methods – Part 305: Colour fastness
• EN 4057-306:2006 Aerospace series – Cable ties for harnesses – Test methods – Part 306: Heat ageing test
• EN 4057-307:2006 Aerospace series – Cable ties for harnesses – Test methods – Part 307: Resistance to ultra violet radiation
• EN 4057-401:2006 Aerospace series – Cable ties for harnesses – Test methods – Part 401: Loop tensile strength
• EN 4057-402:2006 Aerospace series – Cable ties for harnesses – Test methods – Part 402: Life cycle
• EN 4057-404:2006 Aerospace series – Cable ties for harnesses – Test methods – Part 404: Low temperature installation
• EN 4057-405:2005 Aerospace series – Cable ties for harnesses – Test methods – Part 405: Compass safe distance
• EN 4057-406:2006 Aerospace series – Cable ties for harnesses – Test methods – Part 406: Locking device retention
• EN 4057-407:2005 Aerospace series – Cable ties for harnesses – Test methods – Part 407: Verification of application tool settings
• EN 4058:2001 Aerospace series – Filler rods and filler wires for welding in titanium and titanium alloys – Diameter 0,5 mm < = D < = 5,0 mm - Dimensions
• EN 4059:2001 Aerospace series – Filler rods and filler wires for welding in steel – Diameter 0,5 mm < D < 5,0 mm - Dimensions
• EN 40-6:2002 Lighting columns – Part 6: Requirements for aluminium lighting columns
• EN 4060:2001 Aerospace series – Filler rods and filler wires for welding in heat resisting alloys – Diameter 0,5 mm < = D < = 5,0 mm - Dimensions
• EN 4069:1996 Aerospace series – Nuts, hexagon, plain, reduced height, reduced across flats, in heat resisting steel, passivated – Classification: 600 MPa (at ambient temperature)/650°C
• EN 40-7:2002 Lighting columns – Part 7: Requirements for fibre reinforced polymer composite lighting columns
• EN 407:2004 Protective gloves against thermal risks (heat and/or fire)
• EN 4071:2009 Aerospace series – Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 4072:2009 Aerospace series – Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 4073:2009 Aerospace series – Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated – Classification 1 100 MPa (at ambient temperature) / 235 °C
• EN 4074:2009 Aerospace series – Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, aluminium IVD coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 4075:2008 Aerospace series – Screws, pan head, offset cruciform recess, threaded to head, in corrosion resisting steel, passivated – Classification: 490 MPa (at ambient temperature) / 425 °C
• EN 4078:2009 Aerospace series – Inserts, threaded, thin wall, locked and self-locking, in heat resisting steel, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature) / 315 °C
• EN 408:2010+A1:2012 Timber structures – Structural timber and glued laminated timber – Determination of some physical and mechanical properties
• EN 4084:2009 Aerospace series – Nuts, anchor, self-locking, fixed, two lug, with counterbore, in alloy steel, cadmium plated, MoS2 lubricated – Classification: 1 100 MPA (at ambient temperature) / 235 °C
• EN 4085:2001 Aerospace series – Nickel base alloy NI-B40002 (NiSi4B2) – Filler metal for brazing – Amorphous foil
• EN 409:2009 Timber structures – Test methods – Determination of the yield moment of dowel type fasteners
• EN 4098:2007 Aerospace series – Steel FE-PL1507 (40CrMoV12) – Remelted, hardened and tempered, forgings De = 50 mm, 1 250 MPa = Rm = 1 400 MPa
• EN 4099:2005 Aerospace series – Aluminium alloy AL-P2219-T6 or T62 – Clad sheet and strip – 0,5 mm<="" td="">
• EN 410:2011 Glass in building – Determination of luminous and solar characteristics of glazing
• EN 4100:2005 Aerospace series – Aluminium alloy AL-P2219-T6 or T62 – Sheet and strip – 0,5 mm<="" td="">
• EN 4101:2005 Aerospace series – Aluminium alloy AL-P2024-T4 – Sheet and strip with improved stretch forming capability – 0,4 mm<="" td="">
• EN 4102:2005 Aerospace series – Aluminium alloy AL-P2219-T81 – Clad sheet and strip – 0,5 mm<="" td="">
• EN 4103:2001 Aerospace series – Nickel base alloy NI-B40002 (NiSi4B2) – Filler metal for brazing – Borided foil
• EN 4104:2001 Aerospace series – Nickel base alloy NI-B40002 – Filler metal for brazing – Powder or paste
• EN 4105:1998 Aerospace series – Nickel base alloy NI-B40002 (NiSi4B2) – Filler metal for brazing – Tape
• EN 4106:2013 Aerospace series – Non-metallic materials – Structural adhesive systems – Paste adhesive – Technical specification
• EN 4108:2006 Aerospace series – Wrenches, crow foot, attachment socket, socket drive
• EN 4109:2006 Aerospace series – Wrenches, face spanner
• EN 4110:2006 Aerospace series – Wrenches, open end, box
• EN 4111:2006 Aerospace series – Wrenches, splined, socket for pipe fittings – Technical specification
• EN 4113:2009 Aerospace series – Clamps, loop (”P” type) in corrosion resisting steel, passivated with rubber cushioning – Dimensions, masses
• EN 4114:2009 Aerospace series – Clamps, loop (”P” type) in aluminium alloy with rubber cushioning – Dimensions, masses
• EN 4115:2010 Aerospace series – Cushion, rubber for clamps – Dimensions, masses
• EN 4116:2004 Aerospace series – Nuts, hexagonal, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 4117:2004 Aerospace series – Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread – Classification: 1 550 MPa (at ambient temperature) / 600 °C
• EN 4118:2004 Aerospace series – Nuts, bihexagonal, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread – Classification: 1 100 MPa (at ambient temperature) / 650 °C
• EN 4119:2004 Aerospace series – Nuts, bihexagonal, self-locking, deep counterbore, in heat resisting steel FE-PA2601 (A286), silver plated on thread – Classification: 1 100 MPa (at ambient temperature) / 650 °C
• EN 4120:2004 Aerospace series – Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated on thread – Classification: 1 210 MPa (at ambient temperature) / 730 °C
• EN 4121:2004 Aerospace series – Shank nuts, serrated, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread – Classification: 1 100 MPa (at ambient temperature) / 650 °C
• EN 4122:2004 Aerospace series – Shank nuts, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread – Classification: 1 100 MPa (at ambient temperature) / 650 °C
• EN 4123:2004 Aerospace series – Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread – Classification: 1 550 MPa (at ambient temperature) / 600 °C
• EN 4124:2004 Aerospace series – Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated on thread, for 60° swage – Classification: 1 210 MPa (at ambient temperature) / 730 °C
• EN 4125:2010 Aerospace series – Nuts, anchor, self-locking, fixed, two lug, reduced series, with incremental counterbore, in heat resisting steel, MoS2 lubricated – Classification: 900 MPa (at ambient temperature) / 315 °C
• EN 4126:2010 Aerospace series – Nuts, anchor, self-locking, floating, two lug, reduced series, with incremental counterbore, in heat resisting steel, MoS2 lubricated – Classification: 900 MPa (at ambient temperature) / 315 °C
• EN 4127:2009 Aerospace series – Bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 4128:2009 Aerospace series – Bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in heat resisting nickel base alloy, aluminium IVD coated – Classification: 1 250 MPa (at ambient temperature) / 425 °C
• EN 4129:2009 Aerospace series – Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated – Classification: 1 100 MPa (at ambient temperature) / 235 °C
• EN 4129:2009/AC:2010 Aerospace series – Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated – Classification: 1 100 MPa (at ambient temperature) / 235 °C
• EN 4130:2009 Aerospace series – Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, aluminium IVD coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 4130:2009/AC:2010 Aerospace series – Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, aluminium IVD coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 4131:2009 Aerospace series – Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated – Classification: 1 250 MPa (at ambient temperature) / 425 °C
• EN 4131:2009/AC:2010 Aerospace series – Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated – Classification: 1 250 MPa (at ambient temperature) / 425 °C
• EN 413-1:2011 Masonry cement – Part 1: Composition, specifications and conformity criteria
• EN 413-2:2005 Masonry cement – Part 2: Test methods
• EN 4132:2009 Aerospace series – Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated – Classification: 1 100 MPa (at ambient temperature) / 235 °C
• EN 4133:2009 Aerospace series – Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in titanium alloy, aluminium IVD coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 4134:2009 Aerospace series – Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in heat resisting nickel base alloy, aluminium IVD coated – Classification: 1 250 MPa (at ambient temperature) / 425°C
• EN 4135:2009 Aerospace series – Bolts, normal bi-hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature) / 315 °C
• EN 4136:2009 Aerospace series – Bolts, normal bi-hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated – Classification: 1 100 MPa (at ambient temperature) / 235 °C
• EN 4136:2009/AC:2010 Aerospace series – Bolts, normal bi-hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated – Classification: 1 100 MPa (at ambient temperature) / 235 °C
• EN 4137:2009 Aerospace series – Bolts, normal bi-hexagonal head, stepped shank, long thread, in titanium alloy, anodized, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature) / 315 °C
• EN 4138:2009 Aerospace 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 °C
• EN 415-1:2000+A1:2009 Packaging machines safety – Part 1: Terminology and classification of packaging machines and associated equipment
• EN 415-2:1999 Packaging machines safety – Part 2: Pre-formed rigid container packaging machines
• EN 415-3:1999+A1:2009 Safety of packaging machines – Part 3: Form, fill and seal machines
• EN 415-4:1997 Safety of packaging machines – Part 4: Palletisers and depalletisers
• EN 415-4:1997/AC:2002 Safety of packaging machines – Part 4: Palletisers and depalletisers
• EN 415-5:2006+A1:2009 Safety of packaging machines – Part 5: Wrapping machines
• EN 415-6:2013 Safety of packaging machines – Part 6: Pallet wrapping machines
• EN 415-7:2006+A1:2008 Safety of packaging machines – Part 7: Group and secondary packaging machines
• EN 4158:2006 Aerospace series – Paints and varnishes – Test method for measurement of electrical surface resistance of conductive layers
• EN 415-8:2008 Safety of packaging machines – Part 8: Strapping machines
• EN 415-9:2009 Safety of packaging machines – Part 9: Noise measurement methods for packaging machines, packaging lines and associated equipment, grade of accuracy 2 and 3
• EN 4159:2011 Aerospace series – Paints and varnishes – Determination of resistance to microbial growth
• EN 4160:2011 Aerospace series – Paints and varnishes – Determination of the effect of thermal exposure
• EN 4161:2009 Aerospace series – Screws, pan head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated – Classification : 1 100 PMa (at ambient temperature) / 235 °C
• EN 416-1:2009 Single burner gas-fired overhead radiant tube heaters for non-domestic use – Part 1: Safety
• EN 4161:2009/AC:2010 Aerospace series – Screws, pan head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated – Classification: 1 100 MPa (at ambient temperature) / 235 °C
• EN 416-2:2006 Single burner gas-fired overhead radiant tube heaters for non-domestic use – Part 2: Rational use of energy
• EN 4162:2009 Aerospace series – Screws 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated – 1 100 MPa (at ambient temperature) / 235 °C
• EN 4163:2009 Aerospace series – Screws 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated – 1 100 MPa (at ambient temperature) / 235 °C
• EN 4165-001:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 001: Technical specification
• EN 4165-002:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 002: Specification of performance and contact arrangements
• EN 4165-003:2008 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 003: Modules series 2 and series 3 – Product standard
• EN 4165-004:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175°C continuous – Part 004: Stackable mounting receptacle 2 and 4 modules, series 2 – Product standard
• EN 4165-005:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 005: Stackable mounting receptacle 2 and 4 modules, series 3 – Product standard
• EN 4165-006:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 006: Plug for 2 and 4 modules, series 2 – Product standard
• EN 4165-007:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 007: Plug for 2 and 4 modules, series 3 – Product standard
• EN 4165-008:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 008: Rack and panel plug for 2 and 4 modules, series 2 – Product standard
• EN 4165-009:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 009: Rack and panel plug for 2 and 4 modules, series 3 – Product standard
• EN 4165-010:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 010: Rack and panel rear mounted plug for 2 and 4 modules, series 2 – Product standard
• EN 4165-011:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 011: Flange mounting receptacle 2 and 4 modules, series 2 – Product standard
• EN 4165-012:2005 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 012: Flange mounting receptacle 2 and 4 modules, series 3 – Product standard
• EN 4165-013:2005 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 standard
• EN 4165-014:2005 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 014: Shielded accessory body, 2 and 4 modules for connectors, series 2 and series 3 – Product standard
• EN 4165-015:2005 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 015: Round chimney for accessory (1 per module cavity) – Product standard
• EN 4165-016:2005 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 016: Double oval chimney for accessory (1 per 2 modules) – Product standard
• EN 4165-017:2005 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 017: Blank chimney for accessory (1 per module cavity) – Product standard
• EN 4165-018:2007 Aerospace series – Connectors, electrical, rectangular, modular Operating temperature 175 °C continuous Part 018: Protective cover for receptacle 2 and 4 modules, series 2 and series 3 Product standard
• EN 4165-020:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 020: Coupling system keyway for receptacle – Product standard
• EN 4165-021:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 021: Coupling system keyway for plug – Product standard
• EN 4165-022:2005 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 022: Insertion/extraction tool for removal of modules – Product standard
• EN 4165-023:2007 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 023: Tooling for assembly of receptacle coding component – Product standard
• EN 4165-024:2011 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 024: Single module plug – Product standard
• EN 4165-025:2011 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 025: Module receptacle – Product Standard
• EN 4165-026:2011 Aerospace series – Connectors, electrical, rectangular, modular – Operating temperature 175 °C continuous – Part 026: Accessories for single modules – Product standard
• EN 4166:2004 Aerospace series – Clips, spring tension, three parts – PTFE bushes
• EN 4167:2004 Aerospace series – Clips, spring tension, three parts – Inner clips in heat resisting steel FE-PA2601 (A286)
• EN 4168:2004 Aerospace series – Clips, spring tension, three parts – Outer clips in heat resisting steel FE-PA2601 (A286)
• EN 417:2012 Non-refillable metallic gas cartridges for liquefied petroleum gases, with or without a valve, for use with portable appliances – Construction, inspection, testing and marking
• EN 4170:2007 Aerospace series – Paints and varnishes – Test method for measurement of resistance to cold crack temperature cycle
• EN 4171:2011 Aerospace series – Paints and varnishes – Test method for determination of phosphoric acid index
• EN 4172:2006 Aerospace series – Lockbolts, protruding head, sheartype, close tolerance, in titanium alloy TI-P64001, anodized, metric series – Classification: 1 100 MPa (at ambient temperature) / 315 °C
• EN 4173:2006 Aerospace series – Lockbolts, 100° countersunk normal head, sheartype, close tolerance, in titanium alloy TI-P64001, anodized, metric series – Classification: 1 100 MPa (at ambient temperature) / 315 °C
• EN 4174:2006 Aerospace series – Collars, swage locking, sheartype, in aluminium alloy 2024, anodized or chromated, metric series
• EN 4175:2005 Aerospace series – Collars, flanged swage locking, sheartype, in titanium TI-P99002, metric series
• EN 4176:2005 Aerospace 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 specification
• EN 4178:2009 Aerospace series – Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated – 1 100 MPa (at ambient temperature) / 315 °C
• EN 4179:2009 Aerospace series – Qualification and approval of personnel for non-destructive testing
• EN 4180:2001 Aerospace series – Circular tubes, for fluids in titanium and titanium alloys – Wide tolerances – Diameter 4 mm < D < 40 mm – Dimensions
• EN 4182:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees, reduced
• EN 4183:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 90° welded ends
• EN 4184:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 45° double, welded ends
• EN 4185:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees bulkhead on run long
• EN 4186:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, cross
• EN 4187:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 90° bulkhead, long
• EN 4188:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Elbows 90° bulkhead, long, welded end
• EN 4189:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees, bulkhead branch long
• EN 4190:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees, reduced with thrust wire nut on run
• EN 4191:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees, reduced, bulkhead branch, long
• EN 419-1:2009 Non-domestic gas-fired overhead luminous radiant heaters – Part 1: Safety
• EN 4192:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees, reduced bulkhead branch
• EN 419-2:2006 Non-domestic gas-fired overhead luminous radiant heaters – Part 2: Rational use of energy
• EN 419211-2:2013 Protection profiles for secure signature creation device – Part 2: Device with key generation
• EN 419211-3:2013 Protection profiles for secure signature creation device – Part 3: Device with key import
• EN 419251-1:2013 Security requirements for device for authentication – Part 1: Protection profile for core functionality
• EN 419251-2:2013 Security requirements for device for authentication – Part 2: Protection profile for extension for trusted channel to certificate generation application
• EN 419251-3:2013 Security requirements for device for authentication – Part 3: Additional functionality for security targets
• EN 4193:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees, reduced bulkhead on run long
• EN 4194:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees, reduced, bulkhead
• EN 4195:2011 Aerospace series – Paints and varnishes – Test method for determination of chromate leaching
• EN 4198:2006 Aerospace series – Rod-ends, adjustable self-aligning plain bearing with self-lubricating liner and threaded shank in corrosion resisting steel – Dimensions and loads
• EN 4199-001:2013 Aerospace series – Bonding straps for aircraft – Part 001: Technical specification
• EN 4199-002:2006 Aerospace series – Bonding straps for aircraft – Part 002: Index of product standard
• EN 4199-003:2009 Aerospace series – Bonding straps for aircraft – Part 003: Bonding strap assemblies with flat braided conductor copper, tin plated – 65 °C up to 150 °C and copper, nickel plated – 65 °C up to 260 °C – Product standard
• EN 4199-004:2009 Aerospace series – Bonding straps for aircraft – Part 004: Round bonding straps, copper, tin plated – 65 °C up to 150 °C and nickel plated – 65 °C up to 260 °C – Product standard
• EN 4199-005:2009 Aerospace series – Bonding straps for aircraft – Part 005: Flat braid conductors copper, tin plated -65 °C up to 150 °C and copper, nickel plated, -65 °C up to 260 °C – Product standard
• EN 4199-006:2006 Aerospace series – Bonding straps for aircraft – Part 006: Round braid copper conductors for bonding straps, tin plated up to 150 °C or nickel plated up to 260 °C – Product standard
• EN 438-7:2005 High-pressure decorative laminates (HPL) – Sheets based on thermosetting resins (Usually called Laminates) – Part 7: Compact laminate and HPL composite panels for internal and external wall and ceiling finishes
• EN 438-8:2009 High-pressure decorative laminates (HPL) – Sheets based on thermosetting resins (Usually called Laminates) – Part 8: Classification and specifications for design laminates
• EN 438-9:2010+A1:2013 High-pressure decorative laminates (HPL) – Sheets based on thermosetting resins (Usually called Laminates) – Part 9: Classification and specifications for alternative core laminates
• EN 4500-001:2012 Aerospace series – Metallic materials – Rules for drafting and presentation of material standards – Part 001: General rules
• EN 4500-003:2012 Aerospace series – Metallic materials – Rules for drafting and presentation of material standards – Part 003: Specific rules for heat resisting alloys
• EN 4500-004:2012 Aerospace series – Metallic materials – Rules for drafting and presentation of material standards – Part 004: Specific rules for titanium and titanium alloys
• EN 4500-005:2012 Aerospace series – Metallic materials – Rules for drafting and presentation of material standards – Part 005: Specific rules for steels
• EN 4501:2006 Aerospace series – Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating, metric series – Classification: 1 100 MPa (at ambient temperature) / 315 °C
• EN 450-1:2012 Fly ash for concrete – Part 1: Definition, specifications and conformity criteria
• EN 450-2:2005 Fly ash for concrete – Part 2: Conformity evaluation
• EN 45020:2006 Standardization and related activities – General vocabulary (ISO/IEC Guide 2:2004)
• EN 4503:2013 Aerospace series – Non-metallic materials – Textiles – Test method – Determination of water soluble chloride and sulfate of aqueous extracts
• EN 4504:2013 Aerospace series – Non-metallic materials, Textiles – Test method – Determination of flexibility of narrow fabrics
• EN 4505:2013 Aerospace series – Non-metallic materials – Textiles – Test method – Determination of dimensional stability
• EN 4507:2013 Aerospace series – Non-metallic materials – Textiles – Test method – Determination of water extractable matter
• EN 4508:2006 Aerospace series – Paints and varnishes – Test method for anti slip coatings – Determination of the sliding friction behaviour
• EN 4509:2006 Aerospace series – Screws, 100 countersunk normal head, offset cruciform recess, threaded to head, in titanium alloy, anodized, with aluminium pigmented coating, metric series – Classification: 1 100 MPa (at ambient temperature) / 315 °C
• EN 451-1:2003 Method of testing fly ash – Part 1: Determination of free calcium oxide content
• EN 451-2:1994 Method of testing fly ash – Part 2: Determination of fineness by wet sieving
• EN 452:1995 Swap bodies – Swap bodies of Class A – Dimensions and general requirements
• EN 4526:2013 Aerospace series – Metallic materials – Test methods – Sharp edge-notch tensile testing for sheet and strip
• EN 4528:2009 Aerospace series – Steel FE-PA3903 (X10CrNi18-8) – Cold rolled – Strip for springs – a = 3 mm – 1 250 MPa = Rm = 1 640 MPa
• EN 4529-001:2006 Aerospace series – Elements of electrical and optical connection – Sealing plugs – Part 001: Technical specification
• EN 4529-002:2006 Aerospace series – Elements of electrical and optical connection – Sealing plugs – Part 002: Index of product standards
• EN 4529-003:2006 Aerospace series – Elements of electrical and optical connection – Sealing plugs – Part 003: Class T – Product standard
• EN 453:2000+A1:2009 Food processing machinery – Dough mixers – Safety and hygiene requirements
• EN 4530-001:2006 Aerospace series – Sealing sleeves used in elements of connection – Part 001: Technical specification
• EN 4530-002:2006 Aerospace series – Sealing sleeves used in elements of connection – Part 002: List and utilization of sealing sleeves
• EN 4530-005:2006 Aerospace series – Sealing sleeves used in elements of connection – Part 005: Sealing sleeves for external diameter cable 3 mm to 4,1 mm – Product standard
• EN 4530-006:2006 Aerospace series – Sealing sleeves used in elements of connection – Part 006: Sealing sleeves for external diameter cable 4,68 mm to 5,05 mm – Product standard
• EN 4531-001:2012 Aerospace series – Connectors, optical, circular, single and multipin, coupled by triple start threaded ring – Flush contacts – Part 001: Technical specification
• EN 4531-002:2012 Aerospace series – Connectors, optical, circular, single and multipin, coupled by triple start threaded ring – Flush contacts – Part 002: Specification of performance and contact arrangements
• EN 4531-003:2012 Aerospace series – Connectors, optical, circular, single and multipin, coupled by triple start threaded ring – Flush contacts – Part 003: Square flange receptacle – Product standard
• EN 4531-004:2012 Aerospace series – Connectors, optical, circular, single and multipin, coupled by triple start threaded ring – Flush contacts – Part 004: Jam nut receptacle – Product standard
• EN 4531-005:2012 Aerospace series – Connectors, optical, circular, single and multipin, coupled by triple start threaded ring – Flush contacts – Part 005: Plug – Product standard
• EN 4531-101:2012 Aerospace series – Connectors, optical, circular, single and multipin, coupled by triple start threaded ring – Flush contacts – Part 101: Optical contact for EN 4641-100 cable – 55 °C to 125 °C – Product standard
• EN 4531-901:2012 Aerospace series – Connectors, optical, circular, single and multipin, coupled by triple start threaded ring – Flush contacts – Part 901: Filler plugs – Product standard
• EN 4532:2009 Aerospace series – Cables, optical, single core 200 µm/280 µm fibre, 2,5 mm outer jacket – Technical specification
• EN 4533-001:2006 Aerospace series – Fibre optic systems – Handbook – Part 001: Termination methods and tools
• EN 4533-002:2006 Aerospace series – Fibre optic systems – Handbook – Part 002: Test and measurement
• EN 4533-003:2006 Aerospace series – Fibre optic systems – Handbook – Part 003: Looming and installation practices
• EN 4533-004:2006 Aerospace series – Fibre optic systems – Handbook – Part 004: Repair, maintenance and inspection
• EN 4534-2:2009 Aerospace series – Bushes, plain in aluminium alloy with self-lubricating liner, elevated load – Part 2: Dimensions and loads – Inch series
• EN 4535-2:2009 Aerospace series – Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load – Part 2: Dimensions and loads – Inch series
• EN 4536-2:2009 Aerospace series – Bushes, plain in corrosion resisting steel with self-lubricating liner, elevated load – Part 2: Dimensions and loads – Inch series
• EN 4537-2:2009 Aerospace series – Bushes, flanged in corrosion-resisting steel with self-lubricating liner, elevated load – Part 2: Dimensions and loads – Inch series
• EN 4538-003:2010 Aerospace series – Bearings, spherical plain, in corrosion resisting steel with self-lubricating liner elevated load under low oscillations – Narrow series – Dimensions and loads – Part 003: Inch series with low friction coefficient
• EN 4539-003:2010 Aerospace series – Bearings, spherical plain, in corrosion resisting steel with self-lubricating liner elevated load under low oscillations – Wide series – Dimensions and loads – Part 003: Inch series with low friction coefficient
• EN 454:2000+A1:2009 Food processing machinery – Planetary mixers – Safety and hygiene requirements
• EN 4540:2011 Aerospace series – Bearings, spherical plain, in corrosion resisting steel with self-lubricating liner elevated load under low oscillations – Technical specification
• EN 4549:2003 Aerospace series – Pipe coupling, in heat resisting steel or in heat resisting nickel alloy – Coupling end, welded – Design configuration – Inch series
• EN 45501:1992 Metrological aspects of non-automatic weighing instruments
• EN 45501:1992/AC:1993 Metrological aspects of non-automatic weighing instruments
• EN 4550-1:2003 Aerospace series – Pipe coupling, 37° – Design configuration – Inch series – Part 1: Male sealing ends, spherical
• EN 4550-2:2003 Aerospace series – Pipe coupling, 37° – Design configuration – Inch series – Part 2: Port ends
• EN 45502-1:1997 Active implantable medical devices – Part 1: General requirements for safety, marking and information to be provided by the manufacturer
• EN 45502-2-1:2004 Active implantable medical devices – Part 2-1: Particular requirements for active implantable medical devices intended to treat bradyarrhythmia (cardiac pacemakers)
• EN 45502-2-3:2010 Active implantable medical devices – Part 2-3: Particular requirements for cochlear and auditory brainstem implant systems
• EN 4550-3:2003 Aerospace series – Pipe coupling, 37° – Design configuration – Inch series – Part 3: Port connections
• EN 4550-4:2003 Aerospace series – Pipe coupling, 37° – Design configuration – Inch series – Part 4: Female sealing ends
• EN 455-1:2000 Medical gloves for single use – Part 1: Requirements and testing for freedom from holes
• EN 4551:2003 Aerospace series – Pipe coupling 37°, in heat resisting steel – Swivel nuts – Inch series
• EN 45510-1:1997 Guide for procurement of power station equipment – Part 1: Common clauses
• EN 45510-2-2:1999 Guide for procurement of power station equipment – Part 2-2: Electrical equipment – Uninterruptible power supplies
• EN 45510-2-3:2000 Guide for procurement of power station equipment – Part 2-4: Electrical equipment – Stationary batteries and chargers
• EN 45510-2-4:2000 Guide for procurement of power station equipment – Part 2-4: Electrical equipment – High power static convertors
• EN 45510-2-5:2002 Guide for procurement of power station equipment – Part 2-5: Electrical equipment – Motors
• EN 45510-2-6:2000 Guide for procurement of power station equipment – Part 2-6: Electrical equipment – Generators
• EN 45510-2-7:2002 Guide for procurement of power station equipment – Part 2-7: Electrical equipment – Switchgear and controlgear
• EN 45510-2-8:2004 Guide for procurement of power station equipment – Part 2-8: Electrical equipment – Power cables
• EN 45510-3-1:1999 Guide for procurement of power station equipment – Part 3-1: Boilers – Water tube boilers
• EN 45510-3-2:1999 Guide for procurement of power station equipment – Part 3-2: Boilers – Shell boilers
• EN 45510-3-3:1999 Guide for procurement of power station equipment – Part 3-3: Boilers – Boilers with fluidized bed firing
• EN 45510-4-1:1999 Guide for procurement of power station equipment – Part 4: Boiler auxiliaries – Section 1: Equipment for reduction of dust emissions
• EN 45510-4-10:1999 Guide for procurement of power station equipment – Part 4-10: Boiler auxiliaries – Flue gas denitrification (De-NOx) plant
• EN 45510-4-2:1999 Guide for procurement of power station equipment – Part 4: Boiler auxiliaries – Section 2: Gas-air, steam-air and gas-gas heaters
• EN 45510-4-3:1999 Guide for procurement of power station equipment – Part 4: Boiler auxiliaries – Section 3: Draught plant
• EN 45510-4-4:2002 Guide for procurement of power station equipment – Part 4-4: Boiler auxiliaries – Fuel preparation equipment
• EN 45510-4-5:2002 Guide for procurement of power station equipment – Part 4-5: Boiler auxiliaries – Coal handling and bulk storage plant
• EN 45510-4-6:1999 Guide for procurement of power station equipment – Part 4: Boiler auxiliaries – Section 6: Flue gas desulphurization (De-SOx) plant
• EN 45510-4-7:1999 Guide for procurement of power station equipment – Part 4: Boiler auxiliaries – Section 7: Ash handling plant
• EN 45510-4-8:1999 Guide for procurement of power station equipment – Part 4-8: Boiler auxiliaries – Dust handling plant
• EN 45510-4-9:1999 Guide for procurement of power station equipment – Part 4-9: Boiler auxiliaries – Sootblowers
• EN 45510-5-1:1998 Guide for procurement of power station equipment – Part 5-1: Steam turbines
• EN 45510-5-2:1998 Guide for procurement of power station equipment – Part 5-2: Gas turbines
• EN 45510-5-3:1998 Guide for procurement of power station equipment – Part 5-3: Wind turbines
• EN 45510-5-4:1998 Guide for procurement of power station equipment – Part 5-4: Hydraulic turbines, storage pumps and pump-turbines
• EN 45510-6-1:1998 Guide for procurement of power station equipment – Part 6-1: Turbine auxiliaries – Deaerators
• EN 45510-6-2:1998 Guide for procurement of power station equipment – Part 6-2: Turbine auxiliaries – Feedwater heaters
• EN 45510-6-3:1998 Guide for procurement of power station equipment – Part 6-3: Turbine auxiliaries – Condenser plant
• EN 45510-6-4:1999 Guide for procurement of power station equipment – Part 6-4: Turbine auxiliaries – Pumps
• EN 45510-6-5:1999 Guide for procurement of power station equipment – Part 6-5: Turbine auxiliaries – Dry cooling systems
• EN 45510-6-6:1999 Guide for procurement of power station equipment – Part 6-6: Turbine auxiliaries – Wet and wet/dry cooling towers
• EN 45510-6-7:1998 Guide for procurement of power station equipment – Part 6-7: Turbine auxiliaries – Moisture separator reheaters
• EN 45510-6-8:1999 Guide for procurement of power station equipment – Part 6-8: Turbine auxiliaries – Cranes
• EN 45510-6-9:1999 Guide for procurement of power station equipment – Part 6-9: Turbine auxiliaries – Cooling water systems
• EN 45510-7-1:1999 Guide for procurement of power station plant, equipment, and systems – Part 7-1: Pipework and valves – High pressure piping systems
• EN 45510-7-2:1999 Guide for procurement of power station plant, equipment, and systems – Part 7-2: Pipework and valves – Boiler and high pressure piping valves
• EN 45510-8-1:1998 Guide for procurement of power station equipment – Part 8-1: Control and instrumentation
• EN 4552:2003 Aerospace series – Pipe coupling 37°, spherical, in heat resisting steel – Straight nipples, welded end – Inch series
• EN 455-2:2009+A2:2013 Medical gloves for single use – Part 2: Requirements and testing for physical properties
• EN 4553:2003 Aerospace series – Pipe coupling 37°, spherical, in heat resisting steel – Elbow 90° nipples, welded end – Inch series
• EN 455-3:2006 Medical gloves for single use – Part 3: Requirements and testing for biological evaluation
• EN 4554:2003 Aerospace series – Pipe coupling 37°, spherical, in heat resisting steel – Straight unions, threaded – Inch series
• EN 455-4:2009 Medical gloves for single use – Part 4: Requirements and testing for shelf life determination
• EN 45544-1:1999 Workplace atmospheres – Electrical apparatus used for the direct detection and direct concentration measurement of toxic gases and vapours – Part 1: General requirements and test methods
• EN 45544-2:1999 Workplace atmospheres – Electrical apparatus used for the direct detection and direct concentration measurement of toxic gases and vapours – Part 2: Performance requirements for apparatus used for measuring concentrations in the region of limit values
• EN 45544-3:1999 Workplace atmospheres – Electrical apparatus used for the direct detection and direct concentration measurement of toxic gases and vapours – Part 3: Performance requirements for apparatus used for measuring concentrations well above limit values
• EN 45544-4:1999 Workplace atmospheres – Electrical apparatus used for the direct detection and direct concentration measurement of toxic gases and vapours – Part 4: Guide for selection, installation, use and maintenance
• EN 45545-1:2013 Railway applications – Fire protection on railway vehicles – Part 1: General
• EN 45545-2:2013 Railway applications – Fire protection on railway vehicles – Part 2: Requirements for fire behavior of materials and components
• EN 45545-3:2013 Railway applications – Fire protection on railway vehicles – Part 3: Fire resistance requirements for fire barriers
• EN 45545-4:2013 Railway applications – Fire protection on railway vehicles – Part 4: Fire safety requirements for rolling stock design
• EN 45545-5:2013 Railway applications – Fire protection on railway vehicles – Part 5: Fire safety requirements for electrical equipment including that of trolley buses, track guided buses and magnetic levitation vehicles
• EN 45545-6:2013 Railway applications – Fire protection on railway vehicles – Part 6: Fire control and management systems
• EN 45545-7:2013 Railway applications – Fire protection on railway vehicles – Part 7: Fire safety requirements for flammable liquid and flammable gas installations
• EN 4555:2003 Aerospace series – Pipe coupling 37°, in heat resisting steel – Ferrules, welded end – Inch series
• EN 4556:2003 Aerospace series – Pipe coupling 37°, in heat resisting steel – Cap assemblies- Inch series
• EN 4557:2003 Aerospace series – Pipe coupling 37°, spherical, in heat resisting steel – Tees nipples, welded end – Inch series
• EN 4560:2003 Aerospace series – Pipe coupling 37°, spherical, up to 21000 kPa – Inch series – Technical specification
• EN 4561:2003 Aerospace series – Pipe coupling, welded, in heat resisting steel – Elbow 90° – Inch series
• EN 4562:2003 Aerospace series – Pipe coupling, welded, in heat resisting steel – Reductors – Inch series
• EN 4563:2003 Aerospace series – Pipe coupling, welded, in heat resisting steel – Tees – Inch series
• EN 458:2004 Hearing protectors – Recommendations for selection, use, care and maintenance – Guidance document
• EN 4585:2003 Aerospace series – Clips, spring tension – Technical specification
• EN 4588:2007 Aerospace series – Paints and varnishes – Two component, cold curing polyurethane paint, anti slip
• EN 4590:2005 Aerospace series – Retainers, spring, sheet metal, for self-locking barrel nuts, in corrosion resisting steel, passivated
• EN 4591:2005 Aerospace series – Nuts, barrel, self-locking, floating, self-aligning, in heat resisting nickel base alloy, MoS2 lubricated – Classification: 1 550 MPa (at ambient temperature) / 315 °C
• EN 459-1:2010 Building lime – Part 1: Definitions, specifications and conformity criteria
• EN 4592:2006 Aerospace series – Paints and varnishes – Test method for determination of infrared reflectance
• EN 459-2:2010 Building lime – Part 2: Test methods
• EN 4593:2011 Aerospace series – Paints and varnishes – Determination of solar absorptance
• EN 459-3:2011 Building lime – Part 3: Conformity evaluation
• EN 4594:2013 Aerospace series – Paints and varnishes – Two component cold curing polyurethane finish – Supersonic erosion resistance
• EN 4595:2013 Aerospace series – Paints and varnishes – Two component cold curing polyurethane finish – Subsonic erosion resistance
• EN 460:1994 Durability of wood and wood-based products – Natural durability of solid wood – Guide to the durability requirements for wood to be used in hazard classes
• EN 4604-001:2009 Aerospace series – Cable, electrical, for signal transmission – Part 001: Technical specification
• EN 4604-002:2009 Aerospace series – Cable, electrical, for signal transmission – Part 002 : General
• EN 4604-003:2009 Aerospace series – Cable, electrical, for signal transmission – Part 003: Cable, coaxial, 50 ohm, 200 °C, type WZ – Product standard
• EN 4604-004:2007 Aerospace series – Cable, electrical, for signal transmission – Part 004: Cable, microcoaxial, high immunity, 50 Ohms, 200 °C, type WS – Product standard
• EN 4604-006:2009 Aerospace series – Cable, electrical, for signal transmission – Part 006: Cable, coaxial, 50 ohm, 200 °C, type WM – Product standard
• EN 4604-007:2007 Aerospace series – Cable, electrical, for signal transmission – Part 007: Cable, coaxial 50 ?, 200 °C, type WN – Product standard
• EN 4604-008:2009 Aerospace series – Cable, electrical, for signal transmission – Part 008: Cable, coaxial, 50 ohms, 200°C., Type WD – Product standard
• EN 4604-009:2011 Aerospace series – Cable, electrical, for signal transmission – Part 009: Cable, coaxial, light weight, 50 ohms, 180 °C, type KW (light WN) – Product standard
• EN 4604-010:2011 Aerospace series – Cable, electrical, for signal transmission – Part 010: Cable, coaxial, light weight, 50 Ohms, 200 °C, type KX (light WD) – Product standard
• EN 4608-001:2006 Aerospace series – Cable, electrical, fire resistant – Single and twisted multicore assembly, screened (braided) and jacketed – Operating temperatures between – 65 °C and 260 °C – Part 001: Technical specification
• EN 4608-002:2006 Aerospace series – Cable, electrical, fire resistant – Single and twisted multicore assembly, screened (braided) and jacketed – Operating temperatures between – 65 °C and 260 °C – Part 002: General
• EN 4608-003:2012 Aerospace series – Cable, electrical, fire resistant – Single and twisted multicore assembly, screened (braided) and jacketed – Operating temperatures between -65 °C and 260 °C – Part 003: DN family – Lightweight – UV Laser printable – Product standard
• EN 4608-005:2012 Aerospace series – Cable, electrical, fire resistant – Single and twisted multicore assembly, screened (braided) and jacketed – Operating temperatures between -65 °C and 260 °C – Part 005: DW family – Lightweight two-core gauge 24 for data transmission – UV laser printable – Product standard
• EN 461:1999 Specification for dedicated liquefied petroleum gas appliances – Flueless non-domestic space heaters not exceeding 10 kW
• EN 461:1999/A1:2004 Specification for dedicated liquefied petroleum gas appliances – Flueless non-domestic space heaters not exceeding 10 kW
• EN 46-1:2009 Wood preservatives – Determination of the preventive action against recently hatched larvae of Hylotrupes bajulus (Linnaeus) – Part 1: Application by surface treatment (laboratory method)
• EN 4610:2005 Aerospace series – Pipe coupling 8° 30′ in titanium alloy – Elbows 45°, with thrust wire nut
• EN 4611-002:2012 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Part 002: General
• EN 4611-003:2012 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Part 003: Tin plated copper – Operating temperatures, between -65 °C and 135 °C – Single extruded wall for enclosed applications – UV laser printable – Product standard
• EN 4611-004:2012 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Part 004: Tin plated copper – Operating temperatures, between –65 °C and 135 °C – Dual extruded wall for open applications – UV laser printable – Product standard
• EN 4611-005:2012 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Part 005: Silver plated copper — Operating temperatures, between –65 °C and 150 °C – Single extruded wall for enclosed applications – UV laser printable – Product standard
• EN 4611-006:2012 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Part 006: Silver plated copper – Operating temperatures, between –65 °C and 150 °C – Dual extruded wall for open applications – UV laser printable – Product standard
• EN 4611-007:2012 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Part 007: Nickel plated copper – Operating temperatures, between –65 °C and 150 °C – Dual extruded wall for open applications – UV laser printable – Product standard
• EN 4611-008:2012 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Part 008: BP – Nickel plated copper – Operating temperatures, between –65 °C and 150 °C – Dual extruded wall for open applications with additional protection in areas of high vibration, cable flexing and fluid contamination – UV laser printable – Product standard
• EN 4611-009:2012 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Part 009: BJ – Nickel plated copper – Operating temperatures, between –65 °C and 150 °C – Single extruded wall for use as cable cores or within equipment in areas of high vibration, cable flexing and fluid contamination – UV laser printable – Product standard
• EN 4612-002:2011 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Jacketed or screened and jacketed – Part 002: General
• EN 4612-003:2011 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – jacketed or screened and jacketed – Part 003: Tin plated copper – Operating temperatures, between – 65 °C and 135 °C – Single extruded wall for open applications, with jacket without screen – UV laser printable – Product standard
• EN 4612-004:2011 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Jacketed or screened and jacketed – Part 004: Tin plated copper – Operating temperatures, between – 65 °C and 135 °C – Single extruded wall for open applications, with jacket and screen (braid) – UV laser printable – Product standard
• EN 4612-005:2011 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly XLETFE Family jacketed or screened and jacketed – Part 005: Tin plated copper – Operating temperatures, between – 65 °C and 135 °C – Dual extruded wall for open applications, with jacket without screen – UV laser printable – Product standard
• EN 4612-006:2011 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Jacketed or screened and jacketed – Part 006: Tin plated copper – Operating temperatures, between – 65 °C and 135 °C – Dual extruded wall for open applications, with jacket and screen (braid) – UV laser printable – Product standard
• EN 4612-007:2011 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly XLETFE Family jacketed or screened and jacketed – Part 007: Silver plated copper – Operating temperatures, between – 65 °C and 150 °C – Single extruded wall for open applications, with jacket without screen – UV laser printable – Product standard
• EN 4612-008:2011 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly XLETFE Family jacketed or screened and jacketed – Part 008: Silver plated copper – Operating temperatures, between – 65 °C and 150 °C – single extruded wall for open applications, with jacket and screen (braid) – UV laser printable – Product standard
• EN 4612-009:2011 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Jacketed or screened and jacketed – Part 009: Silver plated copper – Operating temperatures, between – 65 °C and 150 °C – Dual extruded wall for open applications, with jacket without screen – UV laser printable – Product standard
• EN 4612-010:2011 Aerospace series – Cables, electrical, for general Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Jacketed or screened and jacketed – Part 010: Silver plated copper – Operating temperatures, between – 65 °C and 150 °C – Dual extruded wall for open applications, with jacket and screen (braid) – UV laser printable – Product standard
• EN 4612-011:2011 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Jacketed or screened and jacketed – Part 011: Nickel plated copper – Operating temperatures, between – 65 °C and 150 °C – Dual extruded wall for open applications, with jacket without screen – UV laser printable – Product standard
• EN 4612-012:2011 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Jacketed or screened and jacketed – Part 012: Nickel plated copper – Operating temperatures, between – 65 °C and 150 °C – Dual extruded wall for open applications, with jacket and screen (braid) – UV laser printable – Product standard
• EN 4612-013:2011 Aerospace series – Cables, electrical, for general purpose, single and multicore assembly – XLETFE Family – Jacketed or screened and jacketed – Part 013: SX, TC and UC – Nickel plated copper – Operating temperatures, between – 65 °C and 150 °C – Single extruded wall for equipment only, with jacket and screen (spiral) – UV laser printable – Product standard
• EN 4613:2009 Aerospace series – Spherical plain bearings in corrosion resisting steel with self-lubricating liner, narrow series – Dimensions and loads – Inch series
• EN 4614:2009 Aerospace series – Spherical plain bearings in corrosion resisting steel with self-lubricating liner, wide series – Dimensions and loads – Inch series
• EN 4615:2005 Aerospace series – Magnesium alloy MG-C18002 – T4 – Sand casting
• EN 4616:2005 Aerospace series – Magnesium alloy MG-C18002 – T4 – Chill casting
• EN 4617:2006 Aerospace series – Recommended practices for standardising company standards
• EN 4618:2009 Aerospace series – Aircraft internal air quality standards, criteria and determination methods
• EN 4619:2010 Aerospace series – Inserts, MJ threads, self-locking, with self-broaching keys – Installation and removal procedure
• EN 46-2:2009 Wood preservatives – Determination of the preventive action against recently hatched larvae of Hylotrupes bajulus (Linnaeus) – Part 2: Ovicidal effect (laboratory method)
• EN 4620:2010 Aerospace series – Inserts, MJ threads, self-locking, with self-broaching keys – Design standard
• EN 4621:2010 Aerospace series – Inserts, MJ threads, self-locking, self-broaching keys – Technical specification
• EN 4622:2010 Aerospace series – Inserts, MJ threads, self-locking, with self-broaching keys, in heat resisting steel FE-PA2601 (A286), MoS2 coated
• EN 4623:2010 Aerospace series – Inserts, MJ threads, self-locking, with self-broaching keys, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated
• EN 4624:2010 Aerospace series – Inserts, MJ threads, self-locking, with self-broaching keys, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plate
• EN 4626-001:2008 Aerospace series – Connectors, optical, rectangular, multicontact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule – Operating temperatures -65 °C to 125 °C (cable dependent) – Flush contacts – Part 001: Technical specification
• EN 4626-002:2008 Aerospace series – Connectors, optical, rectangular, multicontact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule – Operating temperatures – 65 °C to 125 °C (cable dependent) – Flush contacts – Part 002: Specification of performance and contact arrangements
• EN 4626-003:2008 Aerospace series – Connectors, optical, rectangular, multicontact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule – Operating temperatures – 65 °C to 125 °C (cable dependent) – Flush contacts – Part 003: Adaptor for plug
• EN 4626-004:2008 Aerospace series – Connectors, optical, rectangular, multicontact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule – Operating temperatures – 65 °C to 125 °C (cable dependent) – Flush contacts – Part 004: Adaptor for receptacle
• EN 4626-101:2008 Aerospace series – Connectors, optical, rectangular, multicontact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule – Operating temperatures – 65 °C to 125 °C (cable dependent) – Flush contacts – Part 101: Optical contact (sub-assembly) for plug – Product standard
• EN 4626-201:2009 Aerospace series – Connectors, optical, rectangular, multicontact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule – Operating temperatures – 65 °C to 125 °C (cable dependent) – Flush contacts – Part 201: Optical contact (sub-assembly) for receptacle – Product standard
• EN 4626-202:2009 Aerospace series – Connectors, optical, rectangular, multicontact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule – Operating temperatures – 65 °C to 125 °C (cable dependent) – Flush contacts – Part 202: Optical contact assembly for 900 µm buffered fibre receptacle – Product standard
• EN 4627:2007 Aerospace series – Steel FE-PM 3504 (X4CrNiMo16-5-1) – Air melted – Hardened and tempered – Forgings – De = 150 mm – 1 100 MPa = Rm = 1 300 MPa
• EN 4628:2013 Aerospace series – Steel X4CrNiMo16-5-1 (1.4418) – Air melted – Hardened and tempered – Bar – De = 200 mm — 1 150 MPa = Rm = 1 300 MPa
• EN 4629:2013 Aerospace series – Steel X4CrNiMo16-5-1 (1.4418) – Air melted – Softened – Forging stock – De = 300 mm
• EN 4630:2007 Aerospace series – Steel FE-PM 3504 (X4CrNiMo16-5-1) – Air melted – Hardened and tempered – Forgings – De = 200 mm – 900 MPa = Rm = 1 050 MPa
• EN 4631:2013 Aerospace series – Steel X4CrNiMo16-5-1 (1.4418) – Air melted – Hardened and tempered – Bar – De = 200 mm – 900 MPa = Rm = 1 050 MPa
• EN 4632-001:2008 Aerospace series – Welded and brazed assemblies for aerospace constructions – Weldability and brazeability of materials – Part 001: General requirements
• EN 4632-002:2008 Aerospace series – Welded and brazed assemblies for aerospace constructions – Weldability and brazeability of materials – Part 002: Homogeneous assemblies aluminium and aluminium alloys
• EN 4632-003:2010 Aerospace series – Weldability and brazeability of materials in aerospace constructions – Part 003: Welding and brazing of homogeneous assemblies of unalloyed and low alloy steels
• EN 4632-004:2012 Aerospace series – Weldability and brazeability of materials in aerospace constructions – Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels
• EN 4632-005:2009 Aerospace series – Weldability and brazeability of materials in aerospace constructions – Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys
• EN 4632-006:2013 Aerospace series – Weldability and brazeability of materials in aerospace constructions – Part 006: Homogeneous assemblies of titanium alloys
• EN 4634:2009 Aerospace 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 °C
• EN 4635:2009 Aerospace series – Screws, 100° countersunk head, six lobes recess, short thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) – Classification: 1 270 MPa (at ambient temperature) / 650 °C
• EN 4636:2009 Aerospace series – Screws, 100° countersunk head, six lobe recess, short thread, in titanium alloy TI-P64001, with aluminium pigmented coating – Classification: 1 100 MPa (at ambient temperature) / 315 °C
• EN 4637:2010 Aerospace series – Blast media – White corundum
• EN 4638:2010 Aerospace series – Blast media – Brown corundum, without iron
• EN 4639-001:2007 Aerospace series – Connectors, optical, rectangular, modular, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder – Part 001: Technical specification
• EN 4639-002:2007 Aerospace series – Connectors, optical, rectangular, modular, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder – Part 002: List of product standards
• EN 4639-003:2007 Aerospace series – Connectors, optical, rectangular, modular, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder – Part 003: Male optical module – Product standard
• EN 4639-004:2007 Aerospace series – Connectors, optical, rectangular, modular, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder – Part 004: Female optical module – Product standard
• EN 4639-005:2007 Aerospace series – Connectors, optical, rectangular, modular, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder – Part 005: Removable alignment sleeve holder – Product standard
• EN 4639-101:2007 Aerospace series – Connectors, optical, rectangular, modular, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder – Part 101: Optical contact for cable EN 4641-100 – Operating temperatures between – 65 °C and 125 °C – Product standard
• EN 4639-102:2007 Aerospace series – Connectors, optical, rectangular, modular, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder – Part 102: Optical contact for cable EN 4641-102 – Operating temperatures between – 55 °C and 100 °C – Product standard
• EN 464:1994 Protective clothing – Protection against liquid and gaseous chemicals, including aerosols and solid particles – Test method: Determination of leak-tightness of gas-tight suits (Internal pressure test)
• EN 4640-001:2009 Aerospace series – Connectors, optical, rectangular, rack and panel, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder – Part 001: Technical specification
• EN 4640-002:2009 Aerospace series – Connectors, optical, rectangular, rack and panel, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder – Part 002: List of product standards
• EN 4640-003:2008 Aerospace series – Connectors, optical, rectangular, rack and panel, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder – Part 003: Plug optical connector – Product standard
• EN 4640-004:2008 Aerospace series – Connectors, optical, rectangular, rack and panel, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder – Part 004: Receptacle optical connector – Product standard
• EN 4641-001:2009 Aerospace series – Cables, optical, 125 µm diameter cladding – Part 001: Technical specification
• EN 4641-102:2009 Aerospace series – Cables, optical 125 µm outside diameter cladding – Part 102: Semi-loose 62,5/125 µm GI fibre nominal 1,8 mm outside diameter – Product standard
• EN 4641-103:2010 Aerospace series – Cables, optical 125 µm diameter cladding – Part 103: Semi-loose, ruggedized simplex construction 62,5/125 µm GI fibre nominal 2,74 mm, outside diameter – Product standard
• EN 4641-104:2010 Aerospace series – Cables, optical 125 µm diameter cladding – Part 104: Semi-loose, ruggedized duplex construction 62,5/125 µm GI fibre nominal, 4,95 mm outside diameter – Product standard
• EN 4641-105:2010 Aerospace series – Cables, optical 125 µm diameter cladding – Part 105: Semi-loose, ruggedized quadraxial construction 62,5/125 µm GI fibre nominal, 5,72 mm outside diameter – Product standard
• EN 4641-301:2011 Aerospace series – Cables, optical 125 µm diameter cladding – Part 301: Tight structure 50/125 µm GI fibre nominal 1,8 mm outside diameter – Product standard
• EN 4642:2009 Aerospace series – Steel FE-PM 3504 (X4CrNiMo16-5-1) – Air melted – Hardened and tempered – Sheet and plate – 0,6 mm = a = 50 mm – 900 MPa = Rm = 1 050 MPa
• EN 4644-001:2012 Aerospace series – Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous – Part 001: Technical specification
• EN 4644-002:2012 Aerospace series – Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous – Part 002: Specification of performance and contact arrangements
• EN 4644-003:2011 Aerospace series – Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous – Part 003: Rectangular inserts – Product standard
• EN 4644-131:2011 Aerospace series – Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous – Part 131: Size 3 plug for rack and panel applications – Product standard
• EN 4644-133:2011 Aerospace series – Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous – Part 133: Size 3 receptacle for rack and panel application – Product standard
• EN 4644-141:2011 Aerospace series – Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous – Part 141: Size 4 plug for rack and panel applications – Product standard
• EN 4644-142:2012 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 standard
• EN 4645-001:2010 Aerospace series – Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder – Part 001: Technical specification
• EN 4645-002:2009 Aerospace series – Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder – Part 002: Specification of performance and contact arrangements
• EN 4645-003:2009 Aerospace series – Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder – Part 003: Square flange receptacle – Product standard
• EN 4645-004:2009 Aerospace series – Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder – Part 004: Jam nut receptacle – Product standard
• EN 4645-005:2009 Aerospace series – Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder – Part 005: Plug – Product standard
• EN 4649:2009 Aerospace series – Handheld fire extinguishers with synthesis gases, for aircraft use – Technical specification and qualification conditions
• EN 4650:2010 Aerospace series – Wire and cable marking process, UV Laser
• EN 4655:2010 Aerospace series – Steel FE-PM1506 (X1CrNiMoAlTi12-10-2) – Vacuum induction melted and consumable electrode remelted – Solution treated and precipitation treated – Bars – a or D = 200 mm – Rm = 1 400 MPa
• EN 4656:2010 Aerospace series – Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) – Vacuum induction melted and consumable electrode remelted – Solution treated and precipitation treated – Bars – a or D = 200 mm – Rm = 1520 MPa
• EN 4657:2010 Aerospace series – Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) – Vacuum induction melted and consumable electrode remelted – Solution treated and precipitation treated – Bars – a or D = 200 mm – Rm = 1 650 MPa
• EN 4658:2010 Aerospace series – Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) – Vacuum induction melted and consumable electrode remelted – Solution treated and precipitation treated – Forgings – a or D = 200 mm – Rm = 1 520 MPa
• EN 4659:2010 Aerospace series – Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) – Vacuum induction melted and consumable electrode remelted – Solution treated and precipitation treated – Forgings – a or D = 200 mm – Rm = 1 650 MPa
• EN 4660-001:2011 Aerospace series – Modular and Open Avionics Architectures – Part 001: Architecture
• EN 4660-002:2011 Aerospace series – Modular and Open Avionics Architectures – Part 002: Common Functional Modules
• EN 4660-003:2011 Aerospace series – Modular and Open Avionics Architectures – Part 003: Communications/Network
• EN 4660-004:2011 Aerospace series – Modular and Open Avionics Architectures – Part 004: Packaging
• EN 4660-005:2011 Aerospace series – Modular and Open Avionics Architectures – Part 005: Software
• EN 4662:2010 Aerospace series – Test specification for vibration control components
• EN 4670:2010 Aerospace series – Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) – Vacuum induction melted and consumable electrode remelted – Softened – Forging stock – a or D = 300 mm
• EN 4671:2010 Aerospace series – Steel FE-PM1506 (X1CrNiMoAlTi12-10-2) – Vacuum induction melted and consumable electrode remelted – Solution treated and precipitation treated – Forgings – a or D = 200 mm – Rm = 1400 MPa
• EN 4672:2011 Aerospace series – Steel FE-PM1504 (X1CrNiMoAlTi12-10-2) – Vacuum induction melted and consumable electrode remelted – Softened – Forging stock – a or D = 300 mm
• EN 4673-001:2010 Aerospace series – Inserts, UNJ threads, self-locking, with self-broaching keys – Part 001: Installation and removal procedure
• EN 4673-002:2010 Aerospace series – Inserts, UNJ threads, self-locking, with self-broaching keys – Part 002: Design standard
• EN 4673-003:2010 Aerospace series – Inserts, UNJ threads, self-locking, with self-broaching keys – Part 003: Technical specification
• EN 4673-004:2010 Aerospace series – Inserts, UNJ threads, self-locking, with self-broaching keys – Part 004: In heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plating
• EN 4673-005:2010 Aerospace series – Inserts, UNJ threads, self-locking, with self-broaching keys – Part 005: In heat resisting nickel base alloy NI-P101HT (WASPALOY), silver plating
• EN 4673-006:2010 Aerospace series – Inserts, UNJ threads, self-locking, with self-broaching keys – Part 006: In heat resisting steel FE-PA2601 (A286), MoS2 coated
• EN 4675:2011 Aerospace series – Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe) – Rm = 1 300 MPa – Bars – De < 110 mm
• EN 4677-001:2012 Aerospace series – Welded and brazed assemblies for aerospace construction – Joints of metallic materials by electron beam welding – Part 001: Quality of welded assemblies
• EN 4678:2011 Aerospace series – Weldments and brazements for aerospace structures – Joints of metallic materials by laser beam welding – Quality of weldments
• EN 4681-001:2012 Aerospace series – Cables, electric, general purpose, with conductors in aluminium or copper-clad aluminium – Part 001: Technical specification
• EN 4681-002:2012 Aerospace series – Cables, electric, general purpose, with conductors in aluminium or copper-clad aluminium – Part 002: General
• EN 4683:2011 Aerospace series – Steel FE-WM 3504 (X4CrNiMo16-5-1) – Air melted – Filler metal for welding – Wire and rod
• EN 4685:2011 Aerospace series – Titanium Ti10V2Fe3Al – Bars – D < 110 mm – Rm = 1 240 MPa
• EN 4687:2012 Aerospace series – Paints and varnishes – Chromate free non corrosion inhibiting two components cold curing primer for military application
• EN 4688:2012 Aerospace series – Paints and varnishes – Corrosion inhibiting two components cold curing primer for military application
• EN 4689:2012 Aerospace series – Paints and varnishes – Two components cold curing polyurethane finish – High flexibility and chemical agent resistance for military application
• EN 469:2005 Protective clothing for firefighters – Performance requirements for protective clothing for firefighting
• EN 469:2005/A1:2006 Protective clothing for firefighters – Performance requirements for protective clothing for firefighting
• EN 469:2005/AC:2006 Protective clothing for firefighters – Performance requirements for protective clothing for firefighting
• EN 4697:2012 Aerospace series – General and installation requirements for passenger seat fittings
• EN 47:2005 Wood preservatives – Determination of the toxic values against larvae of Hylotrupes bajulus (Linnaeus) – (Laboratory method)
• EN 47:2005/AC:2007 Wood preservatives – Determination of the toxic values against larvae of Hylotrupes bajulus (Linnaeus) – (Laboratory method)
• EN 4700-001:2010 Aerospace series – Steel and heat resisting alloys – Wrought products – Technical specification – Part 001: Plate, sheet and strip
• EN 4700-002:2010 Aerospace series – Steel and heat resisting alloys – Wrought products – Technical specification – Part 002: Bar and section
• EN 4700-003:2010 Aerospace series – Steel and heat resisting alloys – Wrought products – Technical specification – Part 003: Tube
• EN 4700-004:2010 Aerospace series – Steel and heat resisting alloys – Wrought products – Technical specification – Part 004: Wire
• EN 4700-005:2010 Aerospace series – Steel and heat resisting alloys – Wrought products – Technical specification – Part 005: Forging stock
• EN 4700-006:2010 Aerospace series – Steel and heat resisting alloys – Wrought products – Technical specification – Part 006: Pre-production and production forgings
• EN 4700-007:2010 Aerospace series – Steel and heat resisting alloys – Wrought products – Technical specification – Part 007: Remelting stock
• EN 4701-001:2013 Aerospace series – Connectors, optical, rectangular, modular, operating temperature 125 °C, for EN 4531-101 contacts – Part 001: Technical specification
• EN 4701-002:2013 Aerospace series – Connectors, optical, rectangular, modular, operating temperature 125 °C, for EN 4531-101 contacts – Part 002: Material
• EN 4701-003:2013 Aerospace series – Connectors, optical, rectangular, modular, operating temperature 125 °C, for EN 4531-101 contacts – Part 003: Module series 2 – Product standard
• EN 4704:2012 Aerospace series – Tartaric-Sulphuric-Acid anodizing of aluminium and aluminium wrought alloys for corrosion protection and paint pre-treatment (TSA)
• EN 472:1994 Pressure gauges – Vocabulary
• EN 474-1:2006+A3:2013 Earth-moving machinery – Safety – Part 1: General requirements
• EN 474-1:2006+A4:2013 Earth-moving machinery – Safety – Part 1: General requirements
• EN 474-10:2006+A1:2009 Earth-moving machinery – Safety – Part 10: Requirements for trenchers
• EN 474-11:2006+A1:2008 Earth-moving machinery – Safety – Part 11: Requirements for earth and landfill compactors
• EN 474-12:2006+A1:2008 Earth-moving machinery – Safety – Part 12: Requirements for cable excavators
• EN 474-2:2006+A1:2008 Earth-moving machinery – Safety – Part 2: Requirements for tractor-dozers
• EN 474-3:2006+A1:2009 Earth-moving machinery – Safety – Part 3: Requirements for loaders
• EN 474-4:2006+A2:2012 Earth-moving machinery – Safety – Part 4: Requirements for backhoe loaders
• EN 474-5:2006+A3:2013 Earth-moving machinery – Safety – Part 5: Requirements for hydraulic excavators
• EN 474-6:2006+A1:2009 Earth-moving machinery – Safety – Part 6: Requirements for dumpers
• EN 474-7:2006+A1:2009 Earth-moving machinery – Safety – Part 7: Requirements for scrapers
• EN 474-8:2006+A1:2009 Earth-moving machinery – Safety – Part 8: Requirements for graders
• EN 474-9:2006+A1:2009 Earth-moving machinery – Safety – Part 9: Requirements for pipelayers
• EN 476:2011 General requirements for components used in drains and sewers
• EN 477:1995 Unplasticized polyvinylchloride (PVC-U) profiles for the fabrication of windows and doors – Determination of the resistance to impact of main profiles by falling mass
• EN 478:1995 Unplasticized polyvinylchloride (PVC-U) profiles for the fabrication of windows and doors – Appearance after exposure at 150 °C – Test method
• EN 479:1995 Unplasticized polyvinylchloride (PVC-U) profiles for the fabrication of windows and doors – Determination of heat reversion
• EN 48:2005 Wood preservatives – Determination of eradicant action against larvae of Anobium punctatum (De Geer) (laboratory method)
• EN 4800-001:2010 Aerospace series – Titanium and titanium alloys – Technical specification – Part 001: Plate, sheet and strip
• EN 4800-002:2010 Aerospace series – Titanium and titanium alloys – Technical specification – Part 002: Bar and section
• EN 4800-003:2010 Aerospace series – Titanium and titanium alloys – Technical specification – Part 003: Tube
• EN 4800-004:2010 Aerospace series – Titanium and titanium alloys – Technical specification – Part 004: Wire
• EN 4800-005:2010 Aerospace series – Titanium and titanium alloys – Technical specification – Part 005: Forging stock
• EN 4800-006:2010 Aerospace series – Titanium and titanium alloys – Technical specification – Part 006: Pre-production and production forgings
• EN 4800-007:2010 Aerospace series – Titanium and titanium alloys – Technical specification – Part 007: Remelting stock
• EN 4800-008:2010 Aerospace series – Titanium and titanium alloys – Technical specification – Part 008: Pre-production and production castings
• EN 480-1:2006+A1:2011 Admixtures for concrete, mortar and grout – Test methods – Part 1: Reference concrete and reference mortar for testing
• EN 480-10:2009 Admixtures for concrete, mortar and grout – Test methods – Part 10: Determination of water soluble chloride content
• EN 480-11:2005 Admixtures for concrete, mortar and grout – Test methods – Part 11: Determination of air void characteristics in hardened concrete
• EN 480-12:2005 Admixtures for concrete, mortar and grout – Test methods – Part 12: Determination of the alkali content of admixtures
• EN 480-13:2009+A1:2011 Admixtures for concrete, mortar and grout – Test methods – Part 13: Reference masonry mortar for testing mortar admixtures
• EN 480-14:2006 Admixtures for concrete, mortar and grout – Test methods – Part 14: Determination of the effect on corrosion susceptibility of reinforcing steel by potentiostatic electro-chemical test
• EN 480-15:2013 Admixtures for concrete, mortar and grout – Test methods – Part 15: Reference concrete and method for testing viscosity modifying admixtures
• EN 480-2:2006 Admixtures for concrete, mortar and grout – Test methods – Part 2: Determination of setting time
• EN 480-4:2005 Admixtures for concrete, mortar and grout – Test methods – Part 4: Determination of bleeding of concrete
• EN 480-5:2005 Admixtures for concrete, mortar and grout – Test methods – Part 5: Determination of capillary absorption
• EN 480-6:2005 Admixtures for concrete, mortar and grout – Test methods – Part 6: Infrared analysis
• EN 480-8:2012 Admixtures for concrete, mortar and grout – Test methods – Part 8: Determination of the conventional dry material content
• EN 481:1993 Workplace atmospheres – Size fraction definitions for measurement of airborne particles
• EN 4817:2012 Aerospace series – Passive UHF RFID tags intended for aircraft use
• EN 4818:2012 Aerospace series – Passive HF RFID tags intended for aircraft use
• EN 4819:2012 Aerospace series – Contact Memory Button (CMB) tags intended for aircraft use
• EN 482:2012 Workplace exposure – General requirements for the performance of procedures for the measurement of chemical agents
• EN 484:1997 Specification for dedicated liquefied petroleum gas appliances – Independent hotplates, including those incorporating a grill for outdoor use
• EN 485-1:2008+A1:2009 Aluminium and aluminium alloys – Sheet, strip and plate – Part 1: Technical conditions for inspection and delivery
• EN 485-2:2013 Aluminium and aluminium alloys – Sheet, strip and plate – Part 2: Mechanical properties
• EN 485-3:2003 Aluminium and aluminium alloys – Sheet, strip and plate – Part 3: Tolerances on dimensions and form for hot-rolled products
• EN 485-4:1993 Aluminium and aluminium alloys – Sheet, strip and plate – Part 4: Tolerances on shape and dimensions for cold-rolled products
• EN 486:2009 Aluminium and aluminium alloys – Extrusion ingots – Specifications
• EN 487:2009 Aluminium and aluminium alloys – Rolling ingots – Specifications
• EN 488:2011 District heating pipes – Preinsulated bonded pipe systems for directly buried hot water networks – Steel valve assembly for steel service pipes, polyurethane thermal insulation and outer casing of polyethylene
• EN 489:2009 District heating pipes – Preinsulated bonded pipe systems for directly buried hot water networks – Joint assembly for steel service pipes, polyurethane thermal insulation and outer casing of polyethylene
• EN 490:2011 Concrete roofing tiles and fittings for roof covering and wall cladding – Product specifications
• EN 49-1:2005 Wood preservatives – Determination of the protective effectiveness against Anobium punctatum (De Geer) by egg-laying and larval survival – Part 1: Application by surface treatment (Laboratory method)
• EN 491:2011 Concrete roofing tiles and fittings for roof covering and wall cladding – Test methods
• EN 49-2:2005 Wood preservatives – Determination of the protective effectiveness against Anobium punctatum (De Geer) by egg-laying and larval survival – Part 2: Application by impregnation (Laboratory method)
• EN 492:2012 Fibre-cement slates and fittings – Product specification and test methods
• EN 494:2012 Fibre-cement profiled sheets and fittings – Product specification and test methods
• EN 495-5:2013 Flexible sheets for waterproofing – Determination of foldability at low temperature – Part 5: Plastic and rubber sheets for roof waterproofing
• EN 497:1997 Specification for dedicated liquefied petroleum gas appliances – Multi purpose boiling burners for outdoor use
• EN 498:2012 Specification for dedicated liquefied petroleum gas appliances – Barbecues for outdoor use contact grills included

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