STD-EN 3XXXX

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• EN 300:2006 Oriented Strand Boards (OSB) – Definitions, classification and specifications
• EN 3004:1997 Aerospace series – Nuts, self-locking, MJ threads, in heat resisting steel FE-PA2601 (A286) – Classification: 1 100 MPa (at ambient temperature)/650°C – Technical specification
• EN 3005:2004 Aerospace series – Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated or uncoated – Classification: 1 210 MPa (at ambient temperature) / 730 °C – Technical specification
• EN 3006:1994 Aerospace series – Bolts, hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286) – Classification: 900 MPa (at ambient temperature) / 650 °C
• EN 3007:1996 Aerospace series – Bolts, hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated – Classification: 900 MPa (at ambient temperature)/650°C
• EN 3008:1998 Aerospace series – Bolts, hexagon head, relieved shank, long thread, in heat resisting base alloy NI-P100HT (Inconel 718) – Classification: 1 275 MPa (at ambient temperature)/650 °C
• EN 3009:1998 Aerospace series – Bolts, hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plated – Classification: 1 275 MPa (at ambient temperature)/650 °C
• EN 301:2013 Adhesives, phenolic and aminoplastic, for load-bearing timber structures – Classification and performance requirements
• EN 3010:1998 Aerospace series – Bolts, hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy) – Classification: 1 210 MPa (at ambient temperature)/730 °C
• EN 3011:1998 Aerospace series – Bolts, hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated – Classification: 1 210 MPa (at ambient temperature)/730 °C
• EN 30-1-1:2008+A3:2013 Domestic cooking appliances burning gas – Part 1-1: Safety – General
• EN 3012:1995 Aerospace series – Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy) – Classification: 1 210 MPa (at ambient temperature) / 730 °C
• EN 30-1-2:2012 Domestic cooking appliances burning gas – Safety – Part 1-2: Appliances having forced-convection ovens and/or grills
• EN 3013:1995 Aerospace series – Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated – Classification: 1 210 MPa (at ambient temperature) / 730 °C
• EN 30-1-3:2003+A1:2006 Domestic cooking appliances burning gas – Part 1-3: Safety – Appliances having a glass ceramic hotplate
• EN 3014:2001 Aerospace series – Shank nuts, self-locking, serrated, in heat resisting steel FE-PA2601 (A286) – Classification: 1100 MPa (at ambient temperature)/650°C
• EN 30-1-4:2012 Domestic cooking appliances burning gas – Safety – Part 1-4: Appliances having one or more burners with an automatic burner control system
• EN 3015:2001 Aerospace series – Shank nuts, self-locking, serrated, in heat resisting steel FE-PA2601 (A286), silver plated – Classification: 1 100 MPa (at ambient temperature) / 650 °C
• EN 3016:2008 Aerospace series – Washers countersunk, load spreading – Heat resisting steel
• EN 3017:2008 Aerospace series – Washers, facing/packing – Heat resisting steel
• EN 3019:2008 Aerospace series – Self-locking plate nuts, floating, two-lug, in heat resisting steel FE-PA92HT (A286) – Classification: 1 100 MPa (at ambient temperature)/650 °C
• EN 3020:2008 Aerospace series – Self-locking plate nuts, floating, two-lug, in heat resisting steel FE-PA92HT (A286), silver plated – Classification: 1 100 MPa (at ambient temperature)/650 °C
• EN 30-2-1:1998 Domestic cooking appliances burning gas – Part 2-1: Rational use of energy – General
• EN 30-2-1:1998/A1:2003 Domestic cooking appliances burning gas – Part 2-1: Rational use of energy – General
• EN 30-2-1:1998/A1:2003/AC:2004 Domestic cooking appliances burning gas – Part 2-1: Rational use of energy – General
• EN 30-2-1:1998/A2:2005 Domestic cooking appliances burning gas – Part: 2-1: Rational use of energy – General
• EN 302-1:2013 Adhesives for load-bearing timber structures – Test methods – Part 1: Determination of longitudinal tensile shear strength
• EN 30-2-2:1999 Domestic cooking appliances burning gas – Part 2-2: Rational use of energy – Appliances having forced-convection ovens and/or grills
• EN 302-2:2013 Adhesives for load-bearing timber structures – Test methods – Part 2: Determination of resistance to delamination
• EN 302-3:2013 Adhesives for load-bearing timber structures – Test methods – Part 3: Determination of the effect of acid damage to wood fibres by temperature and humidity cycling on the transverse tensile strength
• EN 302-4:2013 Adhesives for load-bearing timber structures – Test methods – Part 4: Determination of the effects of wood shrinkage on the shear strength
• EN 302-5:2013 Adhesives for load-bearing timber structures – Test methods – Part 5: Determination of maximum assembly time under referenced conditions
• EN 3026:1994 Aerospace series – Test method for dry film lubricants – Corrosion test on steels specimens
• EN 302-6:2013 Adhesives for load-bearing timber structures – Test methods – Part 6: Determination of the minimum pressing time under referenced conditions
• EN 3027:1994 Aerospace series – Test method for dry film lubricants – Salt spray test
• EN 302-7:2013 Adhesives for load-bearing timber structures – Test methods – Part 7: Determination of the working life under referenced conditions
• EN 3030:1994 Aerospace series – Test method for dry film lubricants – Solids content
• EN 303-1:1999 Heating boilers – Part 1: Heating boilers with forced draught burners – Terminology, general requirements, testing and marking
• EN 303-1:1999/A1:2003 Heating boilers – Part 1: Heating boilers with forced draught burners – Terminology, general requirements, testing and marking
• EN 3032:1994 Aerospace series – Test method for dry film lubricants – Thickness measurement
• EN 303-2:1998 Heating boilers – Part 2: Heating boilers with forced draught burners – Special requirements for boilers with atomizing oil burners
• EN 303-2:1998/A1:2003 Heating boilers – Part 2: Heating boilers with forced draught burners – Special requirements for boilers with atomizing oil burners
• EN 30326-1:1994 Mechanical vibration – Laboratory method for evaluating vehicle seat vibration – Part 1: Basic requirements (ISO 10326-1:1992)
• EN 30326-1:1994/A1:2007 Mechanical vibration – Laboratory method for evaluating vehicle seat vibration – Part 1: Basic requirements – Amendment 1 (ISO 10326-1:1992/Amd 1:2007)
• EN 30326-1:1994/A2:2011 Mechanical vibration – Laboratory method for evaluating vehicle seat vibration – Part 1: Basic requirements – Amendment 2 (ISO 10326-1:1992/Amd 2:2011)
• EN 303-3:1998 Heating boilers – Part 3: Gas-fired central heating boilers – Assembly comprising a boiler body and a forced draught burner
• EN 303-3:1998/A2:2004 Heating Boilers – Part 3 : Gas-fired heating boilers – Assembly comprising a boiler body and a forced draught burner
• EN 303-3:1998/AC:2006 Heating boilers – Part 3: Gas-fired central heating boilers – Assembly comprising a boiler body and a forced draught burner
• EN 3033:2008 Aerospace series – Nuts, self-locking, hexagonal with captive washer, in heat resisting steel FE-PA2601 (A286), uncoated – Classification : 1 100 MPa/425 °C
• EN 303-4:1999 Heating boilers – Part 4: Heating boilers with forced draught burners – Special requirements for boilers with forced draught oil burners with outputs up to 70 kW and a maximum operating pressure of 3 bar – Terminology, special requirements, testing and marking
• EN 3034:2009 Aerospace series – Nuts, self-locking, hexagonal with captive washer – In heat resisting steel FE-PA92HT (A286), silver coated Classification: 1100 MPa/425 °C
• EN 3034:2009/AC:2011 Aerospace series – Nuts, self-locking, hexagonal with captive washer – In heat resisting steel FE-PA92HT (A286), silver coated Classification: 1100 MPa/425 °C
• EN 3035:1996 Aerospace series – Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in alloy steel, cadmium plated – Classification: 1 100 MPa (at ambient temperature)/235 °C
• EN 303-5:2012 Heating boilers – Part 5: Heating boilers for solid fuels, manually and automatically stoked, nominal heat output of up to 500 kW – Terminology, requirements, testing and marking
• EN 303-6:2000 Heating boilers – Part 6: Heating boilers with forced draught burners – Specific requirements for the domestic hot water operation of combination boilers with atomizing oil burners of nominal heat input not exceeding 70 kW
• EN 3037:1996 Aerospace series – Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315 °C
• EN 303-7:2006 Heating boilers – Part 7: Gas-fired central heating boilers equipped with a forced draught burner of nominal heat output not exceeding 1 000 kW
• EN 3038:1996 Aerospace series – Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in heat and corrosion resisting steel, passivated – Classification: 1 100 MPa (at ambient temperature)/425 °C
• EN 304:1992 Heating boilers – Test code for heating boilers for atomizing oil burners
• EN 304:1992/A1:1998 Heating boilers – Test code for heating boilers for atomizing oil burners
• EN 304:1992/A2:2003 Heating boilers – Test code for heating boilers for atomizing oil burners
• EN 3043:2008 Aerospace series – Fasteners, externally threaded, in heat resisting steel FE PA92HT (A286) – Classification: 900 MPa/650 °C, manufacturing method optional – Technical specification
• EN 3044:1998 Aerospace series – Installation holes for inserts, screw thread, helical coil, self-locking – Design standard
• EN 3045:1993 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in steel – Diameter series 0 and 2 – Reduced clearance category – Dimensions and loads
• EN 3046:1993 Aerospace series – Bearings, airframe rolling – Rigid single row bearings in steel, cadmium plated – Diameter series 0 and 2 – Reduced clearance category – Dimensions and loads
• EN 3047:1993 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in corrosion resisting steel – Diameter series 0 and 2 – Reduced clearance category – Dimensions and loads
• EN 3048:2001 Aerospace series – Bearings, spherical plain in corrosion resisting steel with self-lubricating liner – Light series – Elevated load at ambient temperature – Dimensions and loads
• EN 3049:1998 Aerospace series – O-rings, in fluorocarbon rubber (FKM), low compression set – Hardness 80 IRHD
• EN 305:1997 Heat exchangers – Definitions of performance of heat exchangers and the general test procedure for establishing performance of all heat exchangers
• EN 3050:1998 Aerospace series – O-rings, in fluorocarbon rubber (FKM), low compression set – Technical specification
• EN 3052:2009 Aerospace series – Bolts, normal hexagonal head, close tolerance normal shank, short thread, in heat and corrosion resisting steel, passivated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 3053:1994 Aerospace series – Bearings, airframe rolling – Single row self-aligning roller bearings in steel – Dimensions and loads
• EN 3054:1994 Aerospace series – Bearings, airframe rolling – Single row self-aligning roller bearings in steel, cadmium plated – Dimensions and loads
• EN 3055:1994 Aerospace series – Bearings, airframe rolling – Single row self-aligining roller bearings in corrosion resisting steel – Dimensions and loads
• EN 3056:1994 Aerospace series – Bearings, airframe rolling – Rigid double row ball bearings in steel – Dimensions and loads
• EN 3057:1994 Aerospace series – Bearings, airframe rolling – Rigid double row ball bearings in steel, cadmium plated – Dimensions and loads
• EN 3058:1994 Aerospace series – Bearings, airframe rolling – Rigid double row ball bearings in corrosion resisting steel – Dimensions and loads
• EN 3059:2007 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in steel with flanged alignment housing, cadmium plated – Dimensions and loads
• EN 306:1997 Heat exchangers – Methods of measuring the parameters necessary for establishing the performance
• EN 3060:2007 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in steel, cadmium plated, with flanged alignment housing, cadmium plated – Dimensions and loads
• EN 3061:2007 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in corrosion resisting steel, with flanged alignment housing – Dimensions and loads
• EN 3063:1994 Aerospace series – Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy) – Classification: 1 210 MPa (at ambient temperature) / 730 °C
• EN 3064:1996 Aerospace series – Shank nuts, self-locking, serrated – Installation procedure
• EN 3065:1996 Aerospace series – Installation holes for self-locking, serrated shank nuts – Design standard
• EN 307:1998 Heat exchangers – Guidelines to prepare installation, operating and maintenance instructions required to maintain the performance of each type of heat exchangers
• EN 3079:2006 Aerospace series – Pipe coupling 8°30′ up to 28 000 kPa – Adaptors – Metric series – Technical specification
• EN 308:1997 Heat exchangers – Test procedures for establishing performance of air to air and flue gases heat recovery devices
• EN 3080:2006 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Tees, reduced, branch with thrust wire nut
• EN 3081:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Ferrules, welded with dynamic beam seal end, for repair
• EN 3082:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, bulkhead welded end, for repair
• EN 3082:2001/AC:2003 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, bulkhead welded end, for repair
• EN 3083:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, bulkhead, long welded end, for repair
• EN 3083:2001/AC:2003 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, bulkhead, long welded end, for repair
• EN 3084:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, welded end threaded for repair
• EN 3084:2001/AC:2003 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, welded end threaded for repair
• EN 309:2005 Particleboards – Definition and classification
• EN 31:2011 Wash basins – Connecting dimensions
• EN 310:1993 Wood-based panels – Determination of modulus of elasticity in bending and of bending strength
• EN 3-10:2009 Portable fire extinguishers – Part 10: Provisions for evaluating the conformity of a portable fire extinguisher to EN 3-7
• EN 3102:2013 Aerospace series – Sealants – Test methods – Determination of low-temperature flexibility
• EN 31092:1993 Textiles – Determination of physiological properties – Measurement of thermal and water-vapour resistance under steady-state conditions (sweating guarded – hotplate test) (ISO 11092:1993)
• EN 31092:1993/A1:2012 Textiles – Physiological effects – Measurement of thermal and water-vapour resistance under steady-state conditions (sweating guarded-hotplate test) – Amendment 1 (ISO 11092:1993/Amd 1:2012)
• EN 311:2002 Wood-based panels – Surface soundness – Test method
• EN 3112:1995 Aerospace series – Bolts, normal hexagonal head, threaded to head, in alloy steel, cadmium plated – Classification: 900 MPa (at ambient temperature) / 235 °C
• EN 3114-001:2006 Aerospace series – Test method – Microstructure of (a + ß) titanium alloy wrought products – Part 001: General requirements
• EN 3114-002:2007 Aerospace series – Test method – Microstructure of (a + ß) titanium alloy wrought products – Part 002: Microstructure of bars, sections, forging stock and forgings
• EN 3114-003:2006 Aerospace series – Test method – Microstructure of (a + ß) titanium alloy wrought products – Part 003: Microstructure of plate
• EN 3114-004:2006 Aerospace series – Test method – Microstructure of (a + ß) titanium alloy wrought products – Part 004: Microstructure of sheet for superplastic forming
• EN 3115:2009 Aerospace series – Aluminium alloy 7050-T73 – Wire for solid rivets — D = 10 mm
• EN 312:2010 Particleboards – Specifications
• EN 3120:2012 Aerospace series – Titanium alloy TI-P64003 – Cold worked and stress relieved – Seamless tube for pressure systems – 4 mm = D = 51 mm – 690 MPa = Rm = 1 030 MPa
• EN 313-1:1996 Plywood – Classification and terminology – Part 1: Classification
• EN 313-2:1999 Plywood – Classification and terminology – Part 2: Terminology
• EN 3135:1996 Aerospace series – Rivets, solid, universal head, in corrosion resisting steel FE-PA11, passivated, inch based series
• EN 3136:1996 Aerospace series – Rivets, universal head, in corrosion resisting steel FE-PA92HT, passivated, inch based series
• EN 3138:2001 Aerospace series – Rivets, solid, 100° countersunk normal head with dome, in corrosion resisting steel FE-PA2601, passivated, inch based series
• EN 3139:2001 Aerospace series – Rivets, solid, 100° countersunk normal head, in corrosion resisting steel FE-PA11, passivated, inch based series
• EN 3140:2001 Aerospace series – Rivets, solid, 100° countersunk normal head, in corrosion resisting steel FE-PA2601, passivated, inch based series
• EN 3141:1996 Aerospace series – Rivets, solid, universal head, in heat resisting nickel base alloy NI-P11, cadmium plated, inch based series
• EN 314-1:2004 Plywood – Bonding quality – Part 1: Test methods
• EN 314-2:1993 Plywood – Bonding quality – Part 2: Requirements
• EN 3142:1996 Aerospace series – Rivets, solid, universal head, in heat resisting nickel base alloy NI-P11, inch based series
• EN 31427:1994 Determination of silver in silver jewellery alloys – Volumetric (potentiometric) method using potassium bromide (ISO 11427:1993)
• EN 31427:1994/AC:1994 Determination of silver in silver jewellery alloys – Volumetric (potentiometric) method using potassium bromide (ISO 11427:1993)
• EN 3145:2001 Aerospace series – Round bars, hot rolled in steel – Normal tolerances – Diameter 6 mm < D < 250 mm - Dimensions
• EN 3146:2001 Aerospace series – Round bars, hot rolled in steel – Close tolerances – Diameter 6 mm < = D < = 250 mm - Dimensions
• EN 3148:2008 Aerospace series – Shank nuts, self-locking, flange restrained – Installation procedure
• EN 3149:1996 Aerospace series – Shank nuts – Installation holes, 60° swage, flanges – Design standard
• EN 315:2000 Plywood – Tolerances for dimensions
• EN 3150:1995 Aerospace series – Pins, shoulder, headless, in heat resisting nickel base alloy NI-P100HT (Inconel 718)
• EN 3151:1995 Aerospace series – Dowels, plain, in heat resisting nickel base alloy NI-P100HT (Inconel 718)
• EN 3152:2004 Aerospace series – Nuts, self-locking, MJ threads, in heat resisting steel FE-PA2601 (A286), silver plated or uncoated – Classification: 1 100 MPa (at ambient temperature) / 425 °C – Technical specification
• EN 3155-001:2009 Aerospace series – Electrical contacts used in elements of connection – Part 001: Technical specification
• EN 3155-002:2011 Aerospace series – Electrical contacts used in elements of connection – Part 002: List and utilization of contacts
• EN 3155-003:2005 Aerospace series – Electrical contacts used in elements of connection – Part 003: Contacts, electrical, female, type A, crimp, class S – Product standard
• EN 3155-004:2007 Aerospace series – Electrical contacts used in elements of connection – Part 004: Contacts, electrical, male, type A, crimp, class T – Product standard
• EN 3155-005:2006 Aerospace series – Electrical contacts used in elements of connection – Part 005: Contacts, electrical, female, type A, crimp, class T – Product standard
• EN 3155-005:2006/AC:2006 Aerospace series – Electrical contacts used in elements of connection – Part 005: Contacts, electrical, female, type A, crimp, class T – Product standard
• EN 3155-008:2005 Aerospace series – Electrical contacts used in elements of connection – Part 008: Contacts, electrical, male, type A, crimp, class S – Product standard
• EN 3155-009:2009 Aerospace series – Electrical contacts used in elements of connection – Part 009: Contacts, electrical, female, type A, crimp, class S – Product standard
• EN 3155-012:2006 Aerospace series – Electrical contacts used in elements of connection – Part 012: Contacts, electrical, triaxial, size 8, male, type D, solder, class R – Product standard
• EN 3155-013:2006 Aerospace series – Electrical contacts used in elements of connection – Part 013: Contacts, electrical, triaxial, size 8, female, type D, solder, class R – Product standard
• EN 3155-014:2006 Aerospace series – Electrical contacts used in elements of connection – Part 014: Contacts, electrical, male, type A, crimp, class S – Product standard
• EN 3155-015:2006 Aerospace series – Electrical contacts used in elements of connection – Part 015: Contacts, electrical, female, type A, crimp, class S – Product standard
• EN 3155-016:2006 Aerospace series – Electrical contacts used in elements of connection – Part 016: Contacts, electrical, male, type A, crimp, class S – Product standard
• EN 3155-017:2006 Aerospace series – Electrical contacts used in elements of connection – Part 017: Contacts, electrical, relay base, female, type A, crimp, class P – Product standard
• EN 3155-018:2005 Aerospace series – Electrical contacts used in elements of connection – Part 018: Contacts, electrical, male, type A, crimp, class S – Product standard
• EN 3155-019:2005 Aerospace series – Electrical contacts used in elements of connection – Part 019: Contacts, electrical, female, type A, crimp, class S – Product standard
• EN 3155-022:2006 Aerospace series – Electrical contacts used in elements of connection – Part 022: Contacts, electrical rectangular, male, type A, crimp, class R – Product standard
• EN 3155-023:2006 Aerospace series – Electrical contacts used in elements of connection – Part 023: Contacts, electrical rectangular, female, type A, crimp, class R – Product standard
• EN 3155-024:2006 Aerospace series – Electrical contacts used in elements of connection – Part 024: Contacts, electrical, triaxial, size 8, male, type D, crimp, class S – Product standard
• EN 3155-025:2006 Aerospace series – Electrical contacts used in elements of connection – Part 025: Contacts, electrical, triaxial, size 8, female, type D, crimp, class S – Product standard
• EN 3155-026:2010 Aerospace series – Electrical contacts used in elements of connection – Part 026: Contacts, electrical, male, type A, crimp, class R – Product standard
• EN 3155-027:2006 Aerospace series – Electrical contacts used in elements of connection – Part 027: Contacts, electrical, female, type A, crimp, class R – Product standard
• EN 3155-027:2006/AC:2006 Aerospace series – Electrical contacts used in elements of connection – Part 027: Contacts, electrical, female, type A, crimp, class R – Product standard
• EN 3155-028:2006 Aerospace series – Electrical contacts used in elements of connection – Part 028: Contacts, electrical, coaxial, shielded, size 16, male, type D, crimp, class R – Product standard
• EN 3155-029:2007 Aerospace series – Electrical contacts used in elements of connection – Part 029: Contacts, electrical, coaxial, shielded, size 16, female, type D, crimp, class R – Product standard
• EN 3155-030:2006 Aerospace series – Electrical contacts used in elements of connection – Part 030: Contacts, electrical, coaxial, shielded, size 12, male, type D, crimp, class R – Product standard
• EN 3155-031:2006 Aerospace series – Electrical contacts used in elements of connection – Part 031: Contacts, electrical, coaxial, shielded, size 12, female, type D, crimp, class R – Product standard
• EN 3155-032:2009 Aerospace series – Electrical contacts used in elements of connection – Part 032: Contacts, electrical, coaxial, 50 ohms, size 5, male, type D, crimp, class R – Product standard
• EN 3155-033:2009 Aerospace series – Electrical contacts used in elements of connection – Part 033: Contacts, electrical, coaxial, 50 ohms, size 5, female, type D, crimp, class R – Product standard
• EN 3155-034:2007 Aerospace series – Electrical contacts used in elements of connection – Part 034: Contacts, electrical, triaxial, size 08, male, type D, crimp, class R – Product standard
• EN 3155-035:2012 Aerospace series – Electrical contacts used in elements of connection – Part 035: Contacts, electrical, triaxial, size 08, female, type D, crimp, class R – Product standard
• EN 3155-039:2007 Aerospace series – Electrical contacts used in elements of connection – Part 039: Contacts, electrical, coaxial, size 16, female, type D, solder, class R – Product standard
• EN 3155-040:2007 Aerospace series – Electrical contacts used in elements of connection – Part 040: Contacts, electrical, coaxial, size 12, male, type D, solder, class R – Product standard
• EN 3155-041:2007 Aerospace series – Electrical contacts used in elements of connection – Part 041: Contacts, electrical, coaxial, size 12, female, type D, solder, class R – Product standard
• EN 3155-042:2006 Aerospace series – Electrical contacts used in elements of connection – Part 042: Contacts, electrical, triaxial, size 08, male 042, type D, solder, class P – Product standard
• EN 3155-043:2006 Aerospace series – Electrical contacts used in elements of connection – Part 043: Contacts, electrical, triaxial, size 08, female 043, type D, solder, class P – Product standard
• EN 3155-044:2007 Aerospace series – Electrical contacts used in elements of connection – Part 044: Contacts, electrical, male 044, type A, double crimping, class T – Product standard
• EN 3155-045:2006 Aerospace series – Electrical contacts used in elements of connection – Part 045: Contacts, electrical, female, type A, double crimping, class T – Product standard
• EN 3155-046:2007 Aerospace series – Electrical contacts used in elements of connection – Part 046: Contacts, electrical, male, type A, double crimping, class S – Product standard
• EN 3155-047:2007 Aerospace series – Electrical contacts used in elements of connection – Part 047: Contacts, electrical, female, type A, double crimping, class S – Product standard
• EN 3155-052:2007 Aerospace series – Electrical contacts used in elements of connection – Part 052: Contacts, electrical, male 052, type A, crimp, class S – Product standard
• EN 3155-053:2007 Aerospace series – Electrical contacts used in elements of connection – Part 053: Contacts, electrical, female 053, type A, crimp, class S – Product standard
• EN 3155-054:2006 Aerospace series – Electrical contacts used in elements of connection – Part 054: Contacts, electrical, male thermocouple NiAl, type C, crimp, class T – Product standard
• EN 3155-055:2006 Aerospace series – Electrical contacts used in elements of connection – Part 055: Contacts, electrical, female, thermocouple NiAl, type C, crimp, class T – Product standard
• EN 3155-056:2006 Aerospace series – Electrical contacts used in elements of connection – Part 056: Contacts, electrical, male, thermocouple NiCr, type C, crimp, class T – Product standard
• EN 3155-057:2006 Aerospace series – Electrical contacts used in elements of connection – Part 057: Contacts, electrical, female, thermocouple NiCr, type C, crimp, class T- Product standard
• EN 3155-058:2006 Aerospace series – Electrical contacts used in elements of connection – Part 058: Contacts, electrical, coaxial, size 16, male, type D, solder, class R Product standard
• EN 3155-059:2006 Aerospace series – Electrical contacts used in elements of connection – Part 059: Contacts, electrical, coaxial, size 16, female, type D, solder, class R Product standard
• EN 3155-060:2006 Aerospace series – Electrical contacts used in elements of connection – Part 060: Contacts, electrical, coaxial, size 12, male, type D, solder, class R Product standard
• EN 3155-061:2006 Aerospace series – Electrical contacts used in elements of connection – Part 061: Contacts, electrical, coaxial, size 12, female, type D, solder, class R Product standard
• EN 3155-063:2009 Aerospace series – Electrical contacts used in elements of connection – Part 063: Contacts, electrical, coaxial, 50 ohms, size 1, male, type D, solder, class R – Product standard
• EN 3155-064:2009 Aerospace series – Electrical contacts used in elements of connection – Part 064: Contacts, electrical, coaxial, 50 ohms, size 1, female, type D, solder, class R – Product standard
• EN 3155-065:2006 Aerospace series – Electrical contacts used in elements of connection – Part 065: Contacts, electrical, male, type A, crimp, class S, size 8 Product standard
• EN 3155-066:2006 Aerospace series – Electrical contacts used in elements of connection – Part 066: Contacts, electrical, female, type A, crimp, class S, size 8 – Product standard
• EN 3155-067:2009 Aerospace series – Electrical contacts used in elements of connection – Part 067: Contacts, electrical, coaxial, size 08, male, type D, solder, class R – Product standard
• EN 3155-068:2009 Aerospace series – Electrical contacts used in elements of connection – Part 068: Contacts, electrical, coaxial, size 08, female, type D, solder, class R – Product standard
• EN 3155-069:2009 Aerospace series – Electrical contacts used in elements of connection – Part 069: Contacts, electrical, coaxial, size 16, female, type D, solder, class P – Product standard
• EN 3155-070:2007 Aerospace series – Electrical contacts used in elements of connection – Part 070: Contacts, electrical, male, type A, crimp, class S – Product standard
• EN 3155-071:2007 Aerospace series – Electrical contacts used in elements of connection – Part 071: Contacts, electrical, female, type A, crimp, class S – Product standard
• EN 3155-074:2009 Aerospace series – Electrical contacts used in elements of connection – Part 074: Contacts, electrical, quadrax, size 8, male, type E, crimp, class R – Product standard
• EN 3155-075:2009 Aerospace series – Electrical contacts used in elements of connection – Part 075: Contacts, electrical, quadrax, size 8, female, type E, crimp, class R – Product standard
• EN 3155-076:2012 Aerospace series – Electrical contacts used in elements of connection – Part 076: Contacts, electrical, male, type A, crimp, class R – Product standard
• EN 3155-077:2012 Aerospace series – Electrical contacts used in elements of connection – Part 077: Contacts, electrical, female, type A, crimp, class R – Product standard
• EN 316:2009 Wood fibre boards – Definition, classification and symbols
• EN 3160:2007 Aerospace series – Steel FE-PM3801 (X5CrNiCu17-4) – Air melted, solution treated and precipitation treated, bar a or D = 200 mm, Rm = 1 310 MPa
• EN 3161:2007 Aerospace series – Steel FE-PM3801 (X5CrNiCu17-4) – Air melted, solution treated and precipitation treated, bar a or D = 200 mm, Rm = 930 MPa
• EN 3162:2007 Aerospace series – Steel FE-PM3801 (X5CrNiCu17-4) – Air melted, solution treated and precipitation treated, sheet and strip a = 6 mm, Rm = 930 MPa
• EN 3163:2007 Aerospace series – Steel FE-PM3801 (X5CrNiCu17-4) – Air melted, softened, forging stock a or D = 300 mm
• EN 317:1993 Particleboards and fibreboards – Determination of swelling in thickness after immersion in water
• EN 318:2002 Wood based panels – Determination of dimensional changes associated with changes in relative humidity
• EN 3182:2012 Aerospace series – Ball bearings, rigid in corrosion resisting steel cadmium plated, for control cable pulleys – Dimensions and loads
• EN 319:1993 Particleboards and fibreboards – Determination of tensile strength perpendicular to the plane of the board
• EN 3196:1994 Aerospace series – Nuts, hexagonal, self-locking, in heat resisting steel FE-PA92HT (A286), silver plated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 3197:2010 Aerospace series – Design and installation of aircraft electrical and optical interconnection systems
• EN 320:2011 Particleboards and fibreboards – Determination of resistance to axial withdrawal of screws
• EN 3201:2008 Aerospace series – Holes for metric threaded fasteners – Design standard
• EN 3202:1995 Aerospace series – Holes and traps for T-head bolts – Design standard
• EN 3207:1998 Aerospace series – Rubber compounds – Technical specification
• EN 321:2001 Wood-based panels – Determination of moisture resistance under cyclic test conditions
• EN 3212:1995 Aerospace series – Paints and varnishes – Corrosion test by alternate immersion in a buffered sodium chloride solution
• EN 3218-001:2006 Aerospace series – Connectors, rectangular, with metallic shells and screw-locking – Part 001: Technical specification
• EN 3218-002:2006 Aerospace series – Connectors, rectangular, with metallic shells and screw-locking – Part 002: Specification of performance and contact arrangements
• EN 3218-005:2006 Aerospace series – Connectors, rectangular, with metallic shells and screw-locking – Part 005: Plug with non-removable size 22 solder contacts – Product standard
• EN 3218-006:2006 Aerospace series – Connectors, rectangular, with metallic shells and screw-locking – Part 006: Receptacle with non-removable size 22 solder contacts – Product standard
• EN 3218-007:2006 Aerospace series – Connectors, rectangular, with metallic shells and screw-locking – Part 007: Plug with rear-removable size 20 crimp contacts – Product standard
• EN 3218-008:2006 Aerospace series – Connectors, rectangular, with metallic shells and screw-locking – Part 008: Receptacle with rear-removable size 20 crimp contacts – Product standard
• EN 3218-009:2006 Aerospace series – Connectors, rectangular, with metallic shells and screw-locking – Part 009: Protective covers for EN 3218-005 and EN 3218-007 connectors – Product standard
• EN 3218-010:2006 Aerospace series – Connectors, rectangular, with metallic shells and screw-locking – Part 010: Protective covers for EN 3218-006 and EN 3218-008 connectors – Product standard
• EN 3218-011:2006 Aerospace series – Connectors, rectangular, with metallic shells and screw-locking – Part 011: Tool, insert extraction for EN 3218-005 to EN 3218-008 connectors – Product standard
• EN 322:1993 Wood-based panels – Determination of moisture content
• EN 3226:2009 Nuts, hexagon, plain, normal height, normal across flats, steel, cadmium plated – Classification 1 100 MPa/235 °C
• EN 3227:2010 Aerospace series – Nuts, hexagonal, plain, normal height, normal across flats, in steel, cadmium plated, left hand thread – Classification: 1 100 MPa (at ambient temperature) / 235 °C
• EN 3228:2010 Aerospace series – Nuts, hexagonal, plain, reduced height, normal across flats, in steel, cadmium plated – Classification: 900 MPa (at ambient temperature) / 235 °C
• EN 3229:2009 Aerospace series – Nuts, hexagonal, plain, reduced height, normal across flats, in steel, cadmium plated, left hand thread – Classification: 900 MPa (at ambient temperature) / 235 °C
• EN 323:1993 Wood-based panels – Determination of density
• EN 3230:2001 Aerospace series – Nuts, hexagon, slotted / castellated, reduced height, normal across flats, in steel, cadmium plated – Classification: 900 MPa (at ambient temperature) / 235 °C
• EN 3236:1998 Aerospace series – Inserts, thin wall, self-locking, short, in heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plated internal thread
• EN 3237:1998 Aerospace series – Inserts, thin wall, self-locking, long, in heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plated internal thread
• EN 3238:2010 Aerospace series – Metallic materials – Test method – Shear test for wires and rivets
• EN 3239:1995 Aerospace series – Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated thread – Classification: 1 210 MPa (at ambient temperature) / 730 °C
• EN 3240:2007 Aerospace series – Nuts, self-locking, clip, in heat resisting steel FE-PA2601 (A286), uncoated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 324-1:1993 Wood-based panels – Determination of dimensions of boards – Part 1: Determination of thickness, width and length
• EN 3241:2008 Aerospace series – Nuts, self-locking, clip, in heat resisting steel FE-PA 92 HT (A 286), silver coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 324-2:1993 Wood-based panels – Determination of dimensions of boards – Part 2: Determination of squareness and edge straightness
• EN 3243:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Ferrules, welded, with dynamic beam seal end
• EN 3244:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, straight
• EN 3245:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, straight, reducer
• EN 3246:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, straight, bulkhead
• EN 3247:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, bulkhead, welded end
• EN 3248:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Adaptors, reduced pipe end, with lockring
• EN 325:2012 Wood-based panels – Determination of dimensions of test pieces
• EN 326-1:1994 Wood-based panels – Sampling, cutting and inspection – Part 1: Sampling and cutting of test pieces and expression of test results
• EN 326-2:2010 Wood-based panels – Sampling, cutting and inspection – Part 2: Initial type testing and factory production control
• EN 326-3:2003 Wood-based panels – Sampling, cutting and inspection – Part 3: Inspection of an isolated lot of panels
• EN 3264:2010 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Thrust wire nuts
• EN 3266:2001 Aerospace series – Pipe coupling in titanium alloy – Bulkhead nuts
• EN 3267:2001 Aerospace series – Washers, bulkhead, in titanium alloy
• EN 3268:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Pressure plugs
• EN 3269:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Ferrules, blind, with dynamic beam seal end
• EN 327:2000 Heat exchangers – Forced convection air cooled refrigerant condensors – Test procedure for establishing performance
• EN 327:2000/A1:2002 Heat exchangers – Forced convection air cooled refrigerant condensors – Test procedure for establishing performance
• EN 3270:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Blanking plugs with lockring
• EN 3270:2001/AC:2003 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Blanking plugs with lockring
• EN 3272:2001 Aerospace series – Pipe coupling 8°30′ – Dynamic beam seal end for ferrule, welded – Geometric configuration
• EN 3273:2001 Aerospace series – Pipe coupling 8°30′ – Dynamic beam seal end for elbows, tees and crosses – Geometric configuration
• EN 3274:2010 Aerospace series – Pipe coupling 8°30′ – Thread end – Geometric configuration
• EN 3275:2002 Aerospace series – Pipe coupling 8°30′ up to 28 000 kPa – Dynamic beam seal – Metric series – Technical specification
• EN 3278:2012 Aerospace series – Sleeves, tubular, protruding head, in corrosion resisting steel, passivated (0,25 mm wall thickness)
• EN 328:1999 Heat exchangers – Test procedures for establishing the performance of forced convection unit air coolers for refrigeration
• EN 328:1999/A1:2002 Heat exchangers – Test procedure for establishing the performance of forced convection unit air coolers for refrigeration
• EN 3280:2011 Aerospace series – Bearings, airframe rolling, rigid or self-aligning – Technical specification
• EN 3281:1994 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in steel – Diameter series 8 and 9 – Dimensions and loads
• EN 3282:1994 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in steel, cadmium plated – Diameter series 8 and 9 – Dimensions and loads
• EN 3283:1994 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in corrosion resisting steel – Diameter series 8 and 9 – Dimensions and loads
• EN 3284:1994 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in steel – Diameter series 0 and 2 – Normal clearance category – Dimensions and loads
• EN 3285:1994 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in steel, cadmium plated – Diameter series 0 and 2 – Normal clearance category – Dimensions and loads
• EN 3286:1994 Aerospace series – Bearings, airframe rolling – Rigid single row ball bearings in corrosion resisting steel – Diameter series 0 and 2 – Normal clearance category – Dimensions and loads
• EN 3287:1994 Aerospace series – Bearings, airframe rolling – Double row self-aligning ball bearings in steel – Diameter series 2 – Dimensions and loads
• EN 3288:1994 Aerospace series – Bearings, airframe rolling – Double row self-aligning ball bearings in steel, cadmium plated – Diameter series 2 – Dimensions and loads
• EN 3289:1994 Aerospace series – Bearings, airframe rolling – Double row self-aligning ball bearings in corrosion resisting steel – Diameter series 2 – Dimensions and loads
• EN 3290:1994 Aerospace series – Bearings, airframe rolling – Single row self-aligning roller bearings in steel – Diameter series 3 and 4 – Dimensions and loads
• EN 3291:1994 Aerospace series – Bearings, airframe rolling – Single row self-aligning roller bearings in steel, cadmium plated – Diameter series 3 and 4 – Dimensions and loads
• EN 3292:1994 Aerospace series – Bearings, airframe rolling – Single row self-aligning roller bearings in corrosion resisting steel – Diameter series 3 and 4 – Dimensions and loads
• EN 3293:2008 Aerospace series – Bolts, T-head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-P100HT (Inconel 718), uncoated – Classification: 1 275 MPa/650 °C
• EN 3294:2008 Aerospace series – Bolts, T-head, close tolerance, in heat resisting nickel base alloy NI-P101HT (Waspaloy), uncoated for increased height nuts -Classification: 1 210 MPa/730 °C
• EN 3297:1998 Aerospace series – Inserts, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-P100HT (Inconel 718) – Technical specification
• EN 3298:2008 Aerospace series – Inserts, thin wall, self-locking – Installation and removal procedure
• EN 3299:2007 Aerospace series – Shaft-nuts and threaded rings, self-locking, right- or left-hand MJ threads, in heat resisting steel FE-PA2601 (A286), silver plated – Technical specification
• EN 33:2011 WC pans and WC suites – Connecting dimensions
• EN 33:2011/AC:2013 WC pans and WC suites – Connecting dimensions
• EN 330:1993 Wood preservatives – Field test method for determining the relative protective effectiveness of a wood preservative for use under a coating and exposed out of ground contact: L-joint method
• EN 3301:2007 Aerospace series – Bolts, T-head, close tolerance medium thread length in heat resisting steel FE-PM1708 (FV535), uncoated – Classification: 1 000 MPa/550 °C
• EN 3302:2007 Aerospace series – Bolts in heat resisting steel FE-PM1708 (FV535) – Classification: 1 000 MPa/550 °C – Technical specification
• EN 3303:1997 Aerospace series – Screw, cap head, hexagon socket, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated – Classification: 1 100 MPa (at ambient temperature)/235°C
• EN 3304:1996 Aerospace series – Screws, 100° countersunk reduced head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315 °C
• EN 3305:1996 Aerospace series – Screws, 100° countersunk reduced head, offset cruciform recess, close tolerance normal shank, short thread, in alloy steel, cadmium plated – Classification: 1 100 MPa (at ambient temperature)/235 °C
• EN 3306:1996 Aerospace series – Screws, 100° countersunk normal head, offset cruciform recess, threaded to head, in titanium alloy, anodized, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315°C
• EN 3307:1996 Aerospace series – Screws, pan head, offset cruciform recess, threaded to head, in titanium alloy, anodized, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315 °C
• EN 3308:1996 Aerospace series – Screws, normal hexagonal head, threaded to head, in titanium alloy, anodized, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315°C
• EN 331:1998 Manually operated ball valves and closed bottom taper plug valves for gas installations for buildings
• EN 331:1998/A1:2010 Manually operated ball valves and closed bottom taper plug valves for gas installations for buildings
• EN 3310:2011 Aerospace series – Titanium alloy TI-P64001 (Ti-6Al-4V) – Not heat treated – Forging stock, for annealed forgings – De = 360 mm
• EN 3311:2009 Aerospace series – Titanium alloy TI-P64001 (Ti-6Al-4V) – Annealed – Bar for machining – D < 110 mm
• EN 3312:2012 Aerospace series – Titanium alloy Ti-6Al-4V – Annealed – Forgings De = 150 mm
• EN 3323:2009 Aerospace series – Bolts with double hexagon head, relieved shank. long thread, – In heat resisting steel FE-PM 38 (FV 535) – Classification: 1 000 MPa/550 °C
• EN 3324:2007 Aerospace series – Bolts, hexagon head, relieved shank, long thread, in heat resisting steel FE-PM1708 (FV535) – Classification: 1 000 MPa/550 °C – Unplated
• EN 3325:2007 Aerospace series – Bolts, T-head, relieved shank, long thread, in heat resisting steel, FE-PM1708 (FV535) – Classification: 1 000 MPa/550 °C – Unplated
• EN 3326:2007 Aerospace series – Bolts, D-head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-PH2601 (INCO 718) – Classification: 1 275 MPa/650 °C, unplated
• EN 3327:2008 Aerospace series – Bolts, double hexagon head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-P100HT (Inconel 718), uncoated – Classification: 1 275 MPa/650 °C
• EN 3328:2008 Aerospace series – Bolts, double hexagon head, close tolerance, medium thread length, in heat resisting steel FE-PM38 (FV535), uncoated – Classification: 1 000 MPa/550 °C
• EN 3329:2009 Aerospace series – Steel FE-PL1503 (35CrMo4) – Annealead – Sheet and strip – 0,3 mm = a = 2 mm – For prevailing torque nuts
• EN 3330:2009 Aerospace series – Steel FE-PL1503 (35CrMo4) – Annealead – Bar and wire – De = 40 mm – For prevailing torque nuts
• EN 3332:2005 Aerospace series – Aluminium alloy AL-P7475-T762 – Clad sheet and strip – 1,0 mm<="" td="">
• EN 3333:2005 Aerospace series – Aluminium alloy AL-P7475-T762 – Sheet and strip – 0,6 mm<="" td="">
• EN 3335:2005 Aerospace series – Aluminium alloy AL-P7475-O2 – Sheet for superplastic forming (SPF) – 0,8 mm<="" td="">
• EN 3338:2005 Aerospace series – Aluminium alloy AL-P7050 – T74511 – Extruded bar and section – a or D<="" td="">
• EN 3339:2006 Aerospace series – Aluminium alloy AL-P7010-T76 – Die forgings – a = 200 mm
• EN 334:2005+A1:2009 Gas pressure regulators for inlet pressures up to 100 bar
• EN 3341:2005 Aerospace series – Aluminium alloy AL-P6061-T4 or T42 – Sheet and strip – 0,4 mm<="" td="">
• EN 3342:2005 Aerospace series – Aluminium alloy AL-P6061 – T4 or T42 – Drawn or extruded bar and section – a or D<="" td="">
• EN 3344:2005 Aerospace series – Aluminium alloy AL-P7050 – T76511 – Extruded bar and section – a or D<="" td="">
• EN 3347:2005 Aerospace series – Aluminium alloy AL-P2024 – T8511 – Extruded bar and section – a or D<="" td="">
• EN 335:2013 Durability of wood and wood-based products – Use classes: definitions, application to solid wood and wood-based products
• EN 3351:2012 Aerospace series – Titanium alloy Ti-4Al-4Mo-2Sn – Solution treated and aged – Forgings – De = 150 mm
• EN 3354:2013 Aerospace series – Titanium alloy Ti-6Al-4V – Annealed – Sheet for superplastic forming – a = 6 mm
• EN 3355:2012 Aerospace series – Titanium alloy TI-P64001 (Ti-6Al-4V) – Annealed – Extruded section – De = 150 mm – 900 MPa = Rm = 1 160 MPa
• EN 3359:2007 Aerospace series – Steel FE-PM1503 (X3CrNiMoAl13-8-2) – Vacuum induction melted and consumable electrode remelted, softened, forging stock a or D = 300 mm
• EN 336:2013 Structural timber – Sizes, permitted deviations
• EN 3361:2007 Aerospace series – Steel FE-PM1802 (X5CrNiCu15-5) – Consumable electrode remelted, solution treated and precipitation treated, sheet and strip a = 6mm, 1 070 MPa = Rm = 1 220 MPa
• EN 3364:2007 Aerospace series – Steel FE-PM1802 (X5CrNiCu15-5) – Consumable electrode remelted, softened, forging stock a or D = 300 mm
• EN 3365:2007 Aerospace series – Steel FE-PM3901 (X15CrNi17-3) – Air melted, softened, forging stock a or D = 300 mm
• EN 3368:2008 Aerospace series – Aerospace design standard – Holes for locating pins
• EN 3372-001:2007 Aerospace series – Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures – 65 °C to 175 °C or 200 °C continuous – Part 001: Technical specification
• EN 3372-002:2007 Aerospace series – Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures – 65 °C to 175 °C or 200 °C continuous – Part 002: Specification of performance and contact arrangements
• EN 3372-003:2007 Aerospace series – Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures – 65 °C to 175 °C or 200 °C continuous – Part 003: Square flange receptacle – Product standard
• EN 3372-005:2007 Aerospace series – Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures – 65 °C to 175 °C or 200 °C continuous – Part 005: Receptacle, hermetic, round flange, solder mounting – Product standard
• EN 3372-006:2007 Aerospace series – Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures – 65 °C to 175 °C or 200 °C continuous – Part 006: Protective cover for receptacle – Product standard
• EN 3372-007:2007 Aerospace series – Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures – 65 °C to 175 °C or 200 °C continuous – Part 007: Protective cover for plug – Product standard
• EN 3372-008:2007 Aerospace series – Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures – 65 °C to 175 °C or 200 °C continuous – Part 008: Free plug with grounding spring – Product standard
• EN 3372-009:2007 Aerospace series – Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures – 65 °C to 175 °C or 200 °C continuous – Part 009: Receptacle, jam nut mounting – Product standard
• EN 3372-011:2007 Aerospace series – Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures – 65 °C to 175 °C or 200 °C continuous – Part 011: Dummy receptacle – Product standard
• EN 3373-001:2007 Aerospace series – Terminal lugs and in-line splices for crimping on electric conductors – Part 001: Technical specification
• EN 3373-002:2009 Aerospace series – Terminal lugs and in-line splices for crimping on electric conductors – Part 002: General and list of product standard
• EN 3373-007:2012 Aerospace series – Terminal lugs and in-line splices for crimping on electric conductors – Part 007: Nickel plated aluminium terminal lugs for crimping on nickel plated aluminium cable for inch series studs – Product standard
• EN 3373-008:2012 Aerospace series – Terminal lugs and in-line splices for crimping on electric conductors – Part 008: Copper lugs nickel plated ring shaped for copper conductors nickel plated for inch series studs up to 340 °C – Product standard
• EN 3373-010:2009 Aerospace series – Terminal lugs and in-line splices for crimping on electric conductors – Part 010: Terminal lugs, ring shaped, tin plated, for crimping on copper conductors, temperature up to 150 °C for metric and inch stud series – Product standard
• EN 3373-011:2009 Aerospace series – Terminal lugs and in-line splices for crimping on electric conductors – Part 011: Terminal lugs, ring shaped, nickel plated, for crimping on copper conductors, temperature up to 260 °C for metric and inch stud series – Product standard
• EN 3373-012:2005 Aerospace series – Terminal lugs and in-line splices for crimping on electric conductors – Part 012: In-line splices, insulated and sealed, for crimping on copper conductors, temperature up to 150 °C – Product standard
• EN 3373-013:2005 Aerospace series – Terminal lugs and in-line splices for crimping on electric conductors – Part 013: In-line splices, insulated and moisture resistant, for crimping on copper conductors, temperature up to 260 °C – Product standard
• EN 3373-014:2009 Aerospace series – Terminal lugs and in-line splices for crimping on electric conductors – Part 014: In-line splices, insulated and sealed, for crimping on copper conductors, temperature up to 200 °C – Product standard
• EN 3375-001:2007 Aerospace series – Cable, electrical, for digital data transmission – Part 001: Technical specification
• EN 3375-002:2012 Aerospace series – Cable, electrical, for digital data transmission – Part 002: General
• EN 3375-003:2007 Aerospace series – Cable, electrical, for digital data transmission – Part 003: Single braid – 77 Ohms – Type KG – Product standard
• EN 3375-004:2007 Aerospace series – Cable, electrical, for digital data transmission – Part 004: Double braid – 77 Ohms – Type WJ – Product standard
• EN 3375-005:2007 Aerospace series – Cable, electrical, for digital data transmission – Part 005: Double braid + metallic layer – 77 Ohms – Type WV – Product standard
• EN 3375-006:2006 Aerospace series – Cable, electrical, for digital data transmission – Part 006: Single braid – 78 Ohms – Type XM – Product standard
• EN 3375-007:2006 Aerospace series – Cable, electrical, for digital data transmission – Part 007: Double braid – 77 Ohms – Type WW – Product standard
• EN 3375-008:2009 Aerospace series – Cable, electrical, for digital data transmission – Part 008: Single braid – Star Quad 100 ohms – Type KD – Product standard
• EN 3375-009:2009 Aerospace series – Cable, electrical, for digital data transmission – Part 009: Single braid – CAN Bus – 120 Ohms – Type WX – Product standard
• EN 3377:1996 Aerospace series – Nuts, hexagonal, self-locking, in heat resisting steel FE-PA92HT (A 286) – Classification: 1 100 MPa (at ambient temperature)/425°C
• EN 3379:1996 Aerospace series – Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), for increased height nuts – Classification: 1 210 MPa (at ambient temperature)/730°C
• EN 338:2009 Structural timber – Strength classes
• EN 3380:1996 Aerospace series – Rings, retaining – Technical specification
• EN 3381:1996 Aerospace series – Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in titanium, anodized, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315 °C
• EN 3382:2012 Aerospace series – Rings retaining, internal, axial mounting, steel, phosphated
• EN 3383:2012 Aerospace series – Rings retaining, internal, axial mounting, steel, vacuum cadmium plated
• EN 3384:2012 Aerospace series – Rings retaining, external, axial mounting, steel, phosphated
• EN 3385:2012 Aerospace series – Rings retaining, external, axial mounting, steel, vacuum cadmium plated
• EN 3386:2012 Aerospace series – Rings retaining, radial mounting, steel, phosphated
• EN 3388:2009 Aerospace series – Fasteners, externally threaded, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) – Classification 1 275 MPa/650 °C – Manufacturing method optional – Technical specification
• EN 3389:2009 Aerospace series – Fasteners, externally threaded, in heat resisting nickel base alloy NI-PH1302 (Waspaloy) – Classification: 1 210 MPa/730 °C – Manufacturing method optional – Technical specification
• EN 341:2011 Personal fall protection equipment – Descender devices for rescue
• EN 3417:2012 Aerospace series – Rivets, solid, universal head, in nickel base alloy NI-P11, metric series
• EN 342:2004 Protective clothing – Ensembles and garments for protection against cold
• EN 342:2004/AC:2008 Protective clothing – Ensembles and garments for protection against cold
• EN 3425:2006 Aerospace series – Groove dimensions for axial mouting internal type retaining rings
• EN 3426:2006 Aerospace series – Groove dimensions for axial mounting external type retaining rings
• EN 3427:2006 Aerospace series – Groove dimensions for radial mounting retaining rings
• EN 343:2003+A1:2007 Protective clothing – Protection against rain
• EN 343:2003+A1:2007/AC:2009 Protective clothing – Protection against rain
• EN 3431:2007 Aerospace series – Nuts, hexagonal, self-locking, with counterbore and captive washer, in heat resisting steel, silver plated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 3435:2010 Aerospace series – Nuts, anchor, self-locking, floating, two lug, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature) / 315 °C
• EN 3444:2006 Aerospace series – Bolt, large bihexagonal head, close tolerance normal shank, medium length thread, in heat resisting nickel base alloy, passivated – Classification: 1 250 MPa (at ambient temperature) /650 C
• EN 3446:1995 Aerospace series – Bearings, precision ball without flange in corrosion resisting steel, for instruments and equipment – Dimensions and loads
• EN 3456:2012 Aerospace series – Titanium alloy TI-P64001 (Ti-6Al-4V) – Annealed – Sheet and strip, hot rolled — a = 6 mm
• EN 3459:2010 Aerospace series – Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) – Solution treated and aged – Plate – 6 mm < a = 50 mm
• EN 3464:2012 Aerospace series – Titanium alloy Ti-6Al-4V – Annealed – Plate – 6 mm < a = 100 mm
• EN 3469:2009 Aerospace series – Steel FE-PM1802 (X5CrNiCu15-5) – Consumable electrode remelted – Solution treated and precipitation treated – Forgings – a or D = 200 mm – Rm = 1 310 MPa
• EN 3474:2005 Aerospace series – Aluminium alloy AL-P2024-T81 – Sheet and strip – 0,25 mm<="" td="">
• EN 3475-100:2010 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 100: General
• EN 3475-201:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 201: Visual examination
• EN 3475-202:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 202: Mass
• EN 3475-203:2006 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 203: Dimensions
• EN 3475-301:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 301: Ohmic resistance per unit length
• EN 3475-302:2006 Aerospace series – Cable, electrical, aircraft use – Test methods – Part 302: Voltage proof test
• EN 3475-303:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 303: Insulation resistance
• EN 3475-304:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 304: Surface resistance
• EN 3475-305:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 305: Overload resistance
• EN 3475-306:2005 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 306: Continuity of conductors
• EN 3475-307:2010 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 307: Corona extinction voltage
• EN 3475-401:2002 Aerospace series – Cables, electrical, aircraft use – Test Methods – Part 401: Accelerated ageing
• EN 3475-402:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 402: Shrinkage and delamination
• EN 3475-403:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 403: Delamination and blocking
• EN 3475-403:2002/AC:2003 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 403: Delamination and blocking
• EN 3475-404:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 404: Thermal shock
• EN 3475-405:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 405: Bending at ambient temperature
• EN 3475-406:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 406: Cold bend test
• EN 3475-407:2009 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 407 : Flammability
• EN 3475-408:2005 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 408: Fire resistance
• EN 3475-409:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 409: Air-excluded ageing
• EN 3475-410:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 410: Thermal endurance
• EN 3475-411:2005 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 411: Resistance to fluids
• EN 3475-412:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 412: Humidity resistance
• EN 3475-413:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 413: Wrap back test
• EN 3475-414:2005 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 414: Differential scanning calorimeter (DSC test)
• EN 3475-415:2005 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 415: Rapid change of temperature
• EN 3475-416:2005 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 416: Thermal stability
• EN 3475-417:2009 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 417: Fire resistance of cables confined inside a harness
• EN 3475-418:2007 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 418: Thermal endurance for conductors
• EN 3475-501:2006 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 501: Dynamic cut-through
• EN 3475-502:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 502: Notch propagation
• EN 3475-503:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 503: Scrape abrasion
• EN 3475-504:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 504: Torsion
• EN 3475-505:2012 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 505: Tensile test on conductors and strands
• EN 3475-506:2007 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 506: Plating continuity
• EN 3475-507:2007 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 507: Adherence of plating
• EN 3475-508:2007 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 508: Plating thickness
• EN 3475-509:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 509: Solderability
• EN 3475-510:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 510: Tensile strength and elongation of extruded insulation, sheath and jacket material
• EN 3475-511:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 511: Cable-to-cable abrasion
• EN 3475-512:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 512: Flexure endurance
• EN 3475-513:2005 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 513: Deformation resistance (Installation with plastic cable ties)
• EN 3475-514:2007 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 514: Porosity of copper cladding on aluminium strands
• EN 3475-515:2009 Aerospace series – Cable, electrical, aircraft use – Test methods – Part 515: Crush resistance
• EN 3475-601:2007 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 601: Smoke density
• EN 3475-602:2007 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 602: Toxicity
• EN 3475-603:2011 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 603: Resistance to wet arc tracking
• EN 3475-603:2011/AC:2011 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 603: Resistance to wet arc tracking
• EN 3475-604:2010 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 604: Resistance to dry arc propagation
• EN 3475-605:2010 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 605: Wet short circuit test
• EN 3475-701:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 701: Strippability and adherence of insulation to the conductor
• EN 3475-702:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 702: Screen pushback capability
• EN 3475-703:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 703: Permanence of manufacturer’s marking
• EN 3475-704:2007 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 704: Flexibility
• EN 3475-705:2005 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 705: Contrast measurement
• EN 3475-706:2005 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 706: Laser markability
• EN 3475-801:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 801: Capacitance per unit length
• EN 3475-802:2009 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 802: Capacitance unbalance
• EN 3475-803:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 803: Capacitance variation
• EN 3475-804:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 804: Velocity of propagation
• EN 3475-805:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 805: Characteristic impedance
• EN 3475-806:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 806: Attenuation
• EN 3475-807:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 807: Transfer impedance
• EN 3475-808:2002 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 808: Cross-talk
• EN 3475-809:2009 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 809: Resistance unbalance
• EN 3475-810:2009 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 810: Structural return loss
• EN 3475-811:2009 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 811: Unbalance attenuation
• EN 3475-812:2009 Aerospace series – Cables, electrical, aircraft use – Test methods – Part 812: Return loss (VSWR)
• EN 3476:2006 Aerospace series – Steel FE-PL1501 (30CrMo12) – Air melted – Softened – Forging stock – a or D = 300 mm
• EN 3479:2007 Aerospace series – Steel FE-PM1802 (X5CrNiCu15-5) – Consumable electrode remelted – Solution treated and precipitation treated – Plate – 6 mm < a = 20 mm - 1 070 MPa = Rm = 1 220 MPa
• EN 348:1992 Protective clothing – Test method: Determination of behaviour of materials on impact of small splashes of molten metal
• EN 348:1992/AC:1993 Protective clothing – Test method: Determination of behaviour of materials on impact of small splashes of molten metal
• EN 3480:2007 Aerospace series – Steel FE-PA3601 (X6CrNiTi18-10) – Air melted – Softened – Plate – 6 mm < a = 50 mm - 500 MPa = Rm = 700 MPa
• EN 3487:2007 Aerospace series – Steel FE-PA3601 (X6CrNiTi18-10) – Air melted – Softened – Bar for machining – a or D = 250 mm – 500 MPa = Rm = 700 MPa
• EN 3488:2007 Aerospace series – Steel FE-PA3601 (X6CrNiTi18-10) – Air melted – Softened – Sheet and strip – a = 6 mm – 500 MPa = Rm = 700 MPa
• EN 349:1993+A1:2008 Safety of machinery – Minimum gaps to avoid crushing of parts of the human body
• EN 3490:2007 Aerospace series – Steel FE-PM3901 (X15CrNi17-3) – Air melted – Hardened and tempered – Bar for machining – De = 200 mm – 900 MPa = Rm = 1 100 MPa
• EN 3491:2006 Aerospace series – Steel FE-PM3901 (X15CrNi17-3) – Air melted – Hardened and tempered – Forgings – De = 100 mm – 900 MPa = Rm = 1 100 MPa
• EN 35:2000 Pedestal bidets with over-rim supply – Connecting dimensions
• EN 350-1:1994 Durability of wood and wood-based products – Natural durability of solid wood – Part 1: Guide to the principles of testing and classification of the natural durability of wood
• EN 350-2:1994 Durability of wood and wood-based products – Natural durability of solid wood – Part 2: Guide to natural durability and treatability of selected wood species of importance in Europe
• EN 3506:2001 Aerospace series – Hot rolled sheets and plates in heat resisting alloys – Thickness 2,0 mm < = a < = 100 mm - Dimensions
• EN 3507:2006 Aerospace series – Steel FE-PL1501 (30CrMo12) – Air melted – Hardened and tempered – Forgings – De = 100 mm – 930 MPa = Rm = 1 080 MPa
• EN 351-1:2007 Durability of wood and wood-based products – Preservative-treated solid wood – Part 1: Classification of preservative penetration and retention
• EN 351-2:2007 Durability of wood and wood-based products – Preservative-treated solid wood – Part 2: Guidance on sampling for the analysis of preservative-treated wood
• EN 352-1:2002 Hearing protectors – General requirements – Part 1: Ear-Muffs
• EN 352-2:2002 Hearing protectors – General requirements – Part 2: Ear-plugs
• EN 352-3:2002 Hearing protectors – General requirements – Part 3: Ear-muffs attached to an industrial safety helmet
• EN 3523:2007 Aerospace series – Steel FE-PL1505 (15CrMoV6) – Air melted – Hardened and tempered – Bar for machining – De = 100 mm – 1 080 MPa = Rm = 1 280 MPa
• EN 352-4:2001 Hearing protectors – Safety requirements and testing – Part 4: Level-dependent ear-muffs
• EN 352-4:2001/A1:2005 Hearing protectors – Safety requirements and testing – Part 4: Level-dependent ear-muffs
• EN 3524:2007 Aerospace series – Steel FE-PL1505 (15CrMoV6) – Air melted – Hardened and tempered – Sheet and strip – 2 mm = a = 6 mm – 1 080 MPa = Rm = 1 280 MPa
• EN 352-5:2002 Hearing protectors – Safety requirements and testing – Part 5: Active noise reduction ear-muffs
• EN 352-5:2002/A1:2005 Hearing protectors – Safety requirements and testing – Part 5: Active noise reduction ear-muffs
• EN 3525:2007 Aerospace series – Steel FE-PL1505 (15CrMoV6) – Air melted – Hardened and tempered – Plate – 6 mm < a = 20 mm - 1 080 MPa = Rm = 1 280 MPa
• EN 352-6:2002 Hearing protectors – Safety requirements and testing – Part 6: Ear-muffs with electrical audio input
• EN 3526:2007 Aerospace series – Steel FE-PL1505 (15CrMoV6) – Air melted – Hardened and tempered – Sheet and strip – 0,5 mm = a = 6 mm – 980 MPa = Rm = 1 180 MPa
• EN 352-7:2002 Hearing protectors – Safety requirements and testing – Part 7: Level-dependent ear-plugs
• EN 3527:2007 Aerospace series – Steel FE-PL1504 (33CrMoV12) – Air melted – Softened – Forging stock – a or D = 300 mm
• EN 352-8:2008 Hearing protectors – Safety requirements and testing – Part 8: Entertainment audio ear-muffs
• EN 3528:2013 Aerospace series – Steel X2NiCoMo18-8-5 (1.6359) – Vacuum induction melted and vacuum arc remelted – Solution treated and precipitation treated – Bar – a or D = 150 mm – 1 750 MPa = Rm = 2 000 MPa
• EN 3529:2010 Aerospace series – Steel FE-PM2701 (X2NiCoMo18-8-5) – Vacuum induction melted and vacuum arc remelted – Solution treated and precipitation treated – Forgings – a or D = 150 mm – 1 750 MPa = Rm = 2 000 MPa
• EN 353-1:2002 Personal protective equipment against falls from a height – Part 1: Guided type fall arresters including a rigid anchor line
• EN 3531:2007 Aerospace series – Steel FE-PM2701 (X2NiCoMo18-8-5) – Vacuum induction melted and vacuum arc remelted – Solution treated and precipitation treated – Sheet and strip – a = 6 mm – 1 750 MPa = Rm = 2 000 MPa
• EN 353-2:2002 Personal protective equipment against falls from a height – Part 2: Guided type fall arresters including a flexible anchor line
• EN 3532:2007 Aerospace series – Steel FE-PM2701 (X2NiCoMo18-8-5) – Vacuum induction melted and vacuum arc remelted – Solution treated and precipitation treated – Plate – 6 mm < a = 40 mm - 1 750 MPa = Rm = 2 000 MPa
• EN 3536:2006 Aerospace series – Nuts, hexagon, self-locking, in heat resisting steel, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315 °C
• EN 3537:2010 Aerospace series – Nuts, anchor, self-locking, fixed, two lug, with counterbore, in heat resisting steel, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315 °C
• EN 3538:2010 Aerospace series – Nuts, anchor, self-locking, fixed, two lug, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315 °C
• EN 3539:2010 Aerospace series – Nuts, anchor, self-locking, one lug, fixed, with counterbore, in heat resisting steel, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature) / 315 °C
• EN 354:2010 Personal fall protection equipment – Lanyards
• EN 3541:1992 Aerospace series – Rod ends, adjustable, self-aligning ball bearing with threaded shank – Dimensions, torques, clearances and loads
• EN 3542:1998 Aerospace series – Inserts, screw thread, helical coil, self-locking, in heat resisting nickel base alloy NI-PH2801 (Inconel X750)
• EN 3543:1997 Aerospace series – Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in heat and corrosion resisting steel, passivated – Classification: 1 100 MPa (at ambient temperature)/425°C
• EN 3545-001:2008 Aerospace series – Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures – 55 °C to 175 °C – Part 001: Technical specification
• EN 3545-002:2008 Aerospace series – Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures – 55 °C to 175 °C – Part 002: Specification of performance and contact arrangements
• EN 3545-003:2005 Aerospace series – Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures – 55 °C to 175 °C – Part 003: Connectors with female contacts – Product standard
• EN 3545-004:2005 Aerospace series – Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures – 55 °C to 175 °C – Part 004: Connectors with male contacts – Product standard
• EN 3545-005:2006 Aerospace series – Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures – 55 °C to 175 °C – Part 005: Female coding and attachment System for mounting on free housing (plug) – Product standard
• EN 3545-006:2006 Aerospace series – Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures – 55 °C to 175 °C – Part 006: Male coding and attachment System for mounting on fixed housing (receptacle) – Product standard
• EN 3545-007:2005 Aerospace series – Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures – 55 °C to 175 °C – Part 007: Cable clamp – Product standard
• EN 3545-008:2006 Aerospace series – Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures – 55 C to 175 C – Part 008: Tools for assembly/removal of coding and attachment system – Product standard
• EN 3545-009:2008 Aerospace series – Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures – 55 °C to 175 °C – Part 009: Protective cover for plug and receptacle – Product standard
• EN 355:2002 Personal protective equipment against falls from a height – Energy absorbers
• EN 3552:2005 Aerospace series – Aluminium alloy AL-P2618A-T6 or T62 – Clad sheet and strip – 0,4 mm<="" td="">
• EN 3553:2004 Aerospace series – Aluminium alloy AL-P2618A – T6511 – Extruded bar and section – a or D
• EN 356:1999 Glass in building – Security glazing – Testing and classification of resistance against manual attack
• EN 3561:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Ferrules with dynamic beam seal end, welded and reduced at pipe end
• EN 3561:2001/AC:2003 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Ferrules with dynamic beam seal end, welded and reduced at pipe end
• EN 3566:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Adaptors with lockring
• EN 3566:2001/AC:2003 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Adaptors with lockring
• EN 3567-001:2001 Aerospace series – In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B – Part 001: Technical specification
• EN 3567-003:2001 Aerospace series – In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B – Part 003: Single in-line couplers – Product standard
• EN 3567-004:2001 Aerospace series – In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B – Part 004: Double in-line couplers – Product standard
• EN 357:2004 Glass in building – Fire resistant glazed elements with transparent or translucent glass products – Classification of fire resistance
• EN 358:1999 Personal protective equipment for work positioning and prevention of falls from a height – Belts for work positioning and restraint and work positioning lanyards
• EN 36:1998 Wall-hung bidets with overrim supply – Connecting dimensions
• EN 360:2002 Personal protective equipment against falls from a height – Retractable type fall arresters
• EN 361:2002 Personal protective equipment against falls from a height – Full body harnesses
• EN 3611:1995 Aerospace series – Spigots – Dimensions and fit selection – Design standard
• EN 3612:1996 Aerospace series – Undercuts for splines – Design standard
• EN 3613:2009 Aerospace series – Bolts, normal hexagonal head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated – Classification: 1 275 MPa/650 °C
• EN 3614:2009 Aerospace series – Bolts, normal hexagonal head, relieved shank, long thread, in heat resisting steel FE-PA2601 (A286), silver plated – Classification: 900 MPa / 650 °C
• EN 362:2004 Personal protective equipment against falls from a height – Connectors
• EN 3626:2006 Aerospace series – Nuts, hexagon, self-locking in steel, cadmium plated, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/235 °C
• EN 363:2008 Personal fall protection equipment – Personal fall protection systems
• EN 3630:2008 Aerospace series – Fluid fittings, flanged, straight – Sealing by O-ring for 0,8 mm thick tubes
• EN 3631:2008 Aerospace series – Fluid fittings, flanged, 90° elbowed – Sealing by O-ring for 0,8 mm thick tubes
• EN 3633:2008 Aerospace series – Installation hole for fluid fittings, flanged
• EN 3635:2008 Aerospace series – Weld lip – Geometrical configuration
• EN 3636:2008 Aerospace series – Screws, reduced pan head, offset cruciform recess, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated – Classification: 900 MPa/650 °C
• EN 3637:2008 Aerospace series – Nuts, self-locking, bi-hexagonal (double reduced), in heat resisting nickel base alloy – NI-P101HT (Waspaloy), silver plated, Classification: 1210 MPa/730 °C
• EN 3638:2007 Aerospace series – Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) – Consumable electrode remelted – Solution and precipitation treated – Sheet, strip and plate – 0,5 mm = a = 10 mm
• EN 364:1992 Personal protective equipment against falls from a height – Test methods
• EN 364:1992/AC:1993 Personal protective equipment against falls from a height – Test methods
• EN 3642:1996 Aerospace series – Rivets, solid, 100° countersunk normal head with dome, in titanium TI-PO2, anodized, inch based series
• EN 3643:1996 Aerospace series – Rivets, solid, 100° countersunk normal head, in titanium TI-PO2, anodized, inch based series
• EN 3644:1996 Aerospace series – Rivets, solid, universal head, in titanium TI-PO2, anodized, inch based series
• EN 3645-001:2013 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 001: Technical specification
• EN 3645-002:2007 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 002: Specification of performance and contact arrangements
• EN 3645-003:2006 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 003: Receptacle square flange mounting – Product standard
• EN 3645-004:2006 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 004: Receptacle, hermetic, square flange mounting – Product standard
• EN 3645-005:2006 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 005: Receptacle, hermetic, round flange, brasage mounting – Product standard
• EN 3645-006:2006 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 006: Protective cover for receptacle – Product standard
• EN 3645-007:2007 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 007: Protective cover for plug – Product standard
• EN 3645-008:2007 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 008: Non release plug with grounding ring – Product standard
• EN 3645-009:2006 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 009: Receptacle, round flange, jam nut mounting – Product standard
• EN 3645-010:2006 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 010: Receptacle, hermetic, round flange, jam nut mounting – Product standard
• EN 3645-011:2006 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 011: Lanyard release plug with grounding fingers – Type 1 – Product standard
• EN 3645-012:2006 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 012: Lanyard release plug with grounding fingers – Type 2 – Product standard
• EN 3645-013:2007 Aerospace series – Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous – Part 013: Dummy receptacle – Product standard
• EN 3646-001:2007 Aerospace series – Connectors, electrical, circular, bayonet coupling, op-erating temperature 175 °C or 200 °C continuous – Part 001: Technical specification
• EN 3646-002:2007 Aerospace series – Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous – Part 002: Specification of performance and contact arrangements
• EN 3646-003:2006 Aerospace series – Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous – Part 003: Receptacle, square flange mounting – Product standard
• EN 3646-004:2013 Aerospace series – Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous – Part 004: Receptacle, jam-nut mounting – Product standard
• EN 3646-005:2006 Aerospace series – Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous – Part 005: Receptacle, hermetic, square flange mounting – Product standard
• EN 3646-006:2006 Aerospace series – Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous – Part 006: Receptacle, hermetic, jam-nut mounting – Product standard
• EN 3646-007:2006 Aerospace series – Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous – Part 007: Receptacle, hermetic, round flange, welding or brazing mounting – Product standard
• EN 3646-008:2006 Aerospace series – Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous – Part 008: Plug – Product standard
• EN 3646-009:2006 Aerospace series – Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous – Part 009: Protective cover for receptacle – Product standard
• EN 3646-010:2006 Aerospace series – Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous – Part 010: Protective cover for plug – Product standard
• EN 3646-011:2006 Aerospace series – Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous – Part 011: Dummy receptacle – Product standard
• EN 365:2004 Personal protective equipment against falls from a height – General requirements for instructions for use, maintenance, periodic examination, repair, marking and packaging
• EN 365:2004/AC:2006 Personal protective equipment against falls from a height – General requirements for instructions for use, maintenance, periodic examination, repair, marking and packaging
• EN 3653:2010 Aerospace series – Nuts, anchor, self-locking, floating, self-aligning, one lug, in steel, cadmium plated, MoS2 lubricated – Classification: 900 MPa (at ambient temperature) / 235 °C
• EN 3658:2008 Aerospace series – Tube bend radii, for engine application – Design standard
• EN 3660-001:2006 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 001: Technical specification
• EN 3660-002:2006 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 002: Index of product standards
• EN 3660-003:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 003: Grommet nut, style A for EN 2997 and EN 4067 – Product standard
• EN 3660-004:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 004: Cable outlet, style A, straight, unsealed with clamp strain relief for EN 2997 and EN 4067 – Product standard
• EN 3660-005:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 005: Cable outlet, style A, 90°, unsealed with clamp strain relief for EN 2997 and EN 4067 – Product standard
• EN 3660-006:2010 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 006: Cable outlet, self-locking, style C, straight, shielded (cone grounding), unsealed with clamp strain relief – Product standard
• EN 3660-007:2010 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 007: Cable outlet, self-locking, style C, 90°, shielded (cone grounding), unsealed with clamp strain relief – Product standard
• EN 3660-008:2010 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 008: Cable outlet, self-locking, style C, 45°, shielded (cone grounding), unsealed with clamp strain relief – Product standard
• EN 3660-009:2007 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 009: Cable outlet, style J, straight, sealed, for heat shrinkable boot – Product standard
• EN 3660-010:2010 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 010: Cable outlet, style K, straight, shielded, sealed, for heat shrinkable boot – Product standard
• EN 3660-011:2010 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 011: Cable outlet, style K, 90°, shielded, sealed, for heat shrinkable boot – Product standard
• EN 3660-012:2008 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 012: Grommet nut, style A for EN 3372 – Product standard
• EN 3660-013:2008 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 013: Cable outlet, style A, straight, unsealed, with cable tie strain relief – Product standard
• EN 3660-014:2008 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 014: Cable outlet, style A, 90°, unsealed, with cable tie strain relief – Product standard
• EN 3660-015:2008 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 015: Cable outlet, style A, 45 , unsealed, with cable tie strain relief – Product standard
• EN 3660-016:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 016: Grommet nut, style A, self-locking and non self-locking for EN 3645 – Product standard
• EN 3660-017:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 017: Cable outlet, style A, straight, unsealed, with cable tie strain relief – Product standard
• EN 3660-018:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 018: Cable outlet, style A, 90°, unsealed, with cable tie strain relief – Product standard
• EN 3660-019:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 019: Cable outlet, style A, 45°, unsealed, with cable tie strain relief – Product standard
• EN 3660-020:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 020: Cable outlet, style A, straight, unsealed, self-locking with clamp strain relief for EN 3645 – Product standard
• EN 3660-021:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 021: Cable outlet, style A, 90°, unsealed, self-locking with clamp strain relief for EN 3645 – Product standard
• EN 3660-022:2008 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 022: Cable outlet, style A, straight, composite, unsealed, with cable tie strain relief – Product standard
• EN 3660-023:2008 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 023: Cable outlet, style A, 90 , composite, unsealed, with cable tie strain relief – Product standard
• EN 3660-024:2008 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 024: Grommet nut, style A, composite – Product standard
• EN 3660-025:2013 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 025: Cable outlet, style A, straight, unsealed, with cable tie strain relief for EN 3646 – Product standard
• EN 3660-026:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 026: Cable outlet, style A , 90°, unsealed, with cable tie strain relief for EN 3646 – Product standard
• EN 3660-027:2013 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 027: Cable outlet, style A, 45°, unsealed, with cable tie strain relief for EN 3646 – Product standard
• EN 3660-036:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 036: spacer pad for cable outlet, style Z – Product standard
• EN 3660-037:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 037: bushing strip, elastomer, for cable outlet, style Z Product standard
• EN 3660-038:2013 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 038: Manual installation tool, style Z, for installation of stainless steel shield termination band EN 3660-033, to cable outlet accessories – Product standard
• EN 3660-062:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 062: Cable outlet, style K, 90°, for heat shrinkable boot, shielded, sealed, self-locking for EN 3645 – Product standard
• EN 3660-063:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 063: Cable outlet, style K, straight, for heat shrinkable boot, shielded, sealed, self-locking for EN 3645 – Product standard
• EN 3660-064:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 064: Cable outlet, style K, straight, for heat shrinkable boot, shielded, sealed, self-locking for EN 2997 and EN 4067 – Product standard
• EN 3660-065:2009 Aerospace series – Cable outlet accessories for circular and rectangular electrical and optical connectors – Part 065: Cable outlet, style K, 90°, for heat shrinkable boot, shielded, sealed, self-locking for EN 2997 and EN 4067 – Product standard
• EN 3661-001:2006 Aerospace series – Circuit breakers, single-pole, temperature compensated, rated current 20 A to 50 A – Part 001: Technical specification
• EN 3661-005:2006 Aerospace series – Circuit breakers, single-pole, temperature compensated, rated current 20 A to 50 A – Part 005: With polarized signal contact – Product standard
• EN 3661-006:2006 Aerospace series – Circuit breakers, single-pole, temperature compensated, rated current 20 A to 50 A – Part 006: With polarized signal contact – Bus bar version – Product standard
• EN 3662-001:2006 Aerospace series – Circuit breakers, three-pole, temperature compensated, rated current 20 A to 50 A – Part 001: Technical specification
• EN 3662-005:2006 Aerospace series – Circuit breakers, three-pole, temperature compensated, rated current 20 A to 50 A – Part 005: With polarized signal contact – Product standard
• EN 3662-006:2006 Aerospace series – Circuit breakers, three-pole, temperature compensated, rated current 20 A to 50 A – Part 006: With polarized signal contact – Bus-bar version – Product standard
• EN 3663:2001 Aerospace series – Pipe coupling – O-rings in rubber NBR, 75 IRHD, – Temperature range: – 55 °C to + 135 °C
• EN 3663:2001/AC:2003 Aerospace series – Pipe coupling – O-rings in rubber NBR, 75 IRHD, Temperature range: – 55 °C to 135 °C
• EN 3665:1997 Aerospace series – Test methods for paints and varnishes – Filiform corrosion resistance test on aluminium alloys
• EN 3668:2006 Aerospace series – Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) – Non heat treated – Forging stock – a or D = 250 mm
• EN 367:1992 Protective clothing – Protection against heat and fire – Method of determining heat transmission on exposure to flame
• EN 367:1992/AC:1992 Protective clothing – Protection against heat and fire – Method of determining heat transmission on exposure to flame
• EN 3671:2007 Aerospace series – Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) – Non heat treated – Forging stock – a or D = 250 mm
• EN 3672:2008 Aerospace series – Shank nuts, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated, for 30° swage – Classification: 1 210 MPa (at ambient temperature)/730 °C
• EN 3676:1998 Aerospace series – Inserts, thin wall, self-locking – Design standard
• EN 3677:2007 Aerospace series – Steel FE-PM3801 (X5CrNiCu17-4) – Air melted – Solution treated and precipitation treated – Forgings – a or D = 200 mm – Rm = 1 310 MPa
• EN 3678:2007 Aerospace series – Steel FE-PM3801 (X5CrNiCu17-4) – Air melted – Solution treated and precipitation treated – Forgings – a or D = 200 mm – Rm = 930 MPa
• EN 3682-001:2013 Aerospace series – Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous – Part 001: Technical specification
• EN 3682-002:2013 Aerospace series – Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous – Part 002: Specification of performance and contact arrangements
• EN 3682-003:2012 Aerospace series – Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous – Part 003: Inserts – Product standard
• EN 3682-004:2012 Aerospace series – Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous – Part 004: Size 2 receptacle – Product standard
• EN 3682-005:2013 Aerospace series – Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous – Part 005: Size 2 plug – Product standard
• EN 3682-006:2013 Aerospace series – Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous – Part 006: Size 3 receptacle – Product standard
• EN 3682-007:2013 Aerospace series – Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous – Part 007: Size 3 plug – Product standard
• EN 3682-008:2013 Aerospace series – Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous – Part 008: Size 4 receptacle – Product standard
• EN 3682-009:2013 Aerospace series – Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous – Part 009: Size 4 plug – Product standard
• EN 3683:2007 Aerospace series – Test methods – Titanium alloy wrought products – Determination of primary a content – Point count method and line intercept method
• EN 3684:2007 Aerospace series – Test methods – Titanium alloy wrought products – Determination of ß transus temperature – Metallographic method
• EN 3685:2008 Aerospace series – Bolts in heat resisting steel FE-PA2601 (A286) – Classification: 1 100 MPa/650 °C – Technical specification
• EN 3686:2008 Aerospace series – Bolts, double hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated – Classification: 1 100 MPa/650 °C
• EN 3686:2008/AC:2009 Aerospace series – Bolts, double hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated – Classification: 1 100 MPa/650 °C
• EN 3687:2010 Aerospace series – Bolts, normal hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated – Classification: 1 100 MPa/650 °C
• EN 3687:2010/AC:2011 Aerospace series – Bolts, normal hexagon head, relieved shank, long thread, in heat resisting steel FE-PA2601 (A286), silver plated – Classification: 1 100 MPa/650 °C
• EN 3688:2001 Aerospace series – T-ring fillers in titanium alloy for welding pipes – 14 000 kPa nominal pressure
• EN 3688:2001/AC:2003 Aerospace series – T-ring fillers in titanium alloy for welding pipes – 14 000 kPa nominal pressure
• EN 3689:2001 Aerospace series – T-ring fillers in titanium alloy for welding pipes – 28 000 kPa nominal pressure
• EN 3689:2001/AC:2003 Aerospace series – T-ring fillers in titanium alloy for welding pipes – 28 000 kPa nominal pressure
• EN 3690:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, bulkhead, long
• EN 3690:2001/AC:2003 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, bulkhead, long
• EN 3691:2001 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, bulkhead, long, welded end
• EN 3691:2001/AC:2003 Aerospace series – Pipe coupling 8°30′ in titanium alloy – Unions, bulkhead, long welded end
• EN 3696:2001 Aerospace series – Washers in heat resisting steel
• EN 3697:2013 Aerospace series – Acrylonitrile-butadiene rubber (NBR) – Low temperature resistant – Hardness 60 IRHD
• EN 3698:2013 Aerospace series – Acrylonitrile-butadiene rubber (NBR) – Low temperature resistant – Hardness 70 IRHD
• EN 3-7:2004+A1:2007 Portable fire extinguishers – Part 7: Characteristics, performance requirements and test methods
• EN 370:1993 Wood preservatives – Determination of eradicant efficacy in preventing emergence of Anobium punctatum (De Geer)
• EN 3706:2012 Aerospace series – Headless threaded plugs, cross recess, in aluminium alloy 5086
• EN 3707:2012 Aerospace series – Headless threaded plugs – Installation holes
• EN 3708-001:2006 Aerospace series – Modular interconnection systems – Terminal junction systems – Part 001: Technical specification
• EN 3708-002:2006 Aerospace series – Modular interconnection systems – Terminal junction systems – Part 002: Performance specification
• EN 3708-003:2006 Aerospace series – Modular interconnection systems – Terminal junction systems – Part 003: Removable feedback modules version, sealed – Product standard
• EN 3708-004:2006 Aerospace series – Modular interconnection systems – Terminal junction systems – Part 004: Removable feedback modules version, unsealed – Product standard
• EN 3708-005:2006 Aerospace series – Modular interconnection systems – Terminal junction systems – Part 005: Frames with accessories for feedback modules version, sealed and unsealed – Product standard
• EN 3709:2006 Aerospace series – Wrenches and sockets, bi-hexagonal – Technical specification
• EN 3710:2008 Aerospace series – Sockets, bi-hexagonal – Technical Specification
• EN 3711:2008 Aerospace series – Wrench-double ended, bi-hexagonal – Straight, cranked, offset
• EN 3712:2007 Aerospace series – Nuts, anchor, self-locking, one lug, fixed, reduced series, with counterbore, in steel, cadmium plated, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature) / 235 °C
• EN 3716-001:2006 Aerospace series – Connector, single-way, with triaxial interface, for transmission of digital data – Part 001: Technical specification
• EN 3716-002:2006 Aerospace series – Connectors, single-way with triaxial interface, for transmission of digital data – Part 002: Conditions of use and list of product standards
• EN 3716-003:2006 Aerospace series – Connectors, single-way with triaxial interface, for transmission of digital data – Part 003: Solder receptacle – Product standard
• EN 3716-004:2006 Aerospace series – Connectors, single-way with triaxial interface, for transmission of digital data – Part 004: Solder plug – Product standard
• EN 3716-005:2006 Aerospace series – Connector, single-way with triaxial interface, for transmission of digital data – Part 005: Crimp receptacle – Product standard
• EN 3716-006:2006 Aerospace series – Connector, single-way with triaxial interface, for transmission of digital data – Part 006: Crimp plug – Product standard
• EN 3717:2008 Aerospace series – Tubes – Selection for engines fluid systems
• EN 3718:2012 Aerospace series – Test method for metallic materials – Ultrasonic inspection of tubes
• EN 3719:2010 Aerospace series – Aluminium or aluminium alloy conductors for electrical cables – Product standard
• EN 3720:1995 Aerospace series – Nuts, bihexagonal, self-locking, in heat resisting steel FE-PA92HT (A286), MoS2 coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 3721:1995 Aerospace series – Nuts, bihexagonal, self-locking, deep counterbored, in heat resisting steel FE-PA92HT (A286), MoS2 coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 3722:1995 Aerospace series – Shank nuts, self-locking, in heat resisting steel FE-PA92HT (A286), MoS2 coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 3723:1996 Aerospace series – Nuts, hexagonal, self-locking, in heat resisting steel, FE-PA92HT (A286), MoS2 coated – Classification: 1 100 MPa (at ambient temperature)/425°C
• EN 3724:2004 Aerospace series – Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated – Strength Class: 1 100 MPa (at ambient temperature)
• EN 3725:2004 Aerospace series – Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated – Strength class: 1 100 MPa (at ambient temperature)
• EN 3726:2004 Aerospace series – Nuts, self-locking, clip, in heat resisting steel FE-PA2601 (A286), MoS2 coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C
• EN 3727:2006 Aerospace series – Bearings, airframe rolling rigid with flanged alignment housing – Technical specification
• EN 3728:2008 Aerospace series – Shaft-nuts, self-locking, left-hand thread, in heat resisting steel FE-PA92HT (A286), silver plated
• EN 3729:2008 Aerospace series – Rings, threaded, self-locking, left-hand thread, in heat resisting steel FE-PA92HT (A286), silver plated
• EN 3730:2009 Aerospace series – Clamps, saddle fixed and sliding version in aluminium alloy with rubber cushioning – Dimension, masses
• EN 3733-001:2009 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous – Part 001: Technical specification
• EN 3733-002:2008 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature 150 °C continuous – Part 002: List of product standards
• EN 3733-003:2008 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature 150 °C continuous – Part 003: Plug connector for cable according to EN 4532, product standard
• EN 3733-004:2008 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature 150 °C continuous – Part 004: Receptacle, connector, four hole fixing cable according to EN 4532, product standard
• EN 3733-005:2007 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature 150 °C continuous – Part 005: Receptacle, connector, two hole fixing cable according to EN 4532, product standard
• EN 3733-006:2008 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature 150 °C continuous – Part 006: Receptacle, connector, jam nut fixing for cable according to EN 4532, product standard
• EN 3733-007:2007 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous – Part 007: Ferrule (optical contact) for EN 4532 (200 µm/280 µm fibre) – Product standard
• EN 3733-008:2006 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 C continuous – Part 008: Plug sub-assembly for cable to EN 4532 (200 µm/280 µm fibre) – Product standard
• EN 3733-009:2006 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 C continuous – Part 009: Receptacle sub-assembly for cable to EN 4532 (200 µm/280 µm fibre) – Product standard
• EN 3733-101:2008 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous – Part 101: Protective cover receptacle – Product standard
• EN 3733-103:2008 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous – Part 103: Protective cover jam nut receptacle – Product standard
• EN 3733-104:2008 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous – Part 104: Receptacle connector dummy four holes fixing – Product standard
• EN 3733-105:2008 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous – Part 105: Receptacle connector dummy two holes fixing – Product standard
• EN 3733-106:2008 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous – Part 106: Receptacle connector dummy jam nut – Product standard
• EN 3733-108:2008 Aerospace series – Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous – Part 108: Cable support boot – Product standard
• EN 3740:1996 Aerospace series – Bolts, shouldered, thin hexagonal head, close tolerance shank, short thread, in titanium alloy, anodized, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315 °C
• EN 374-1:2003 Protective gloves against chemicals and micro-organisms – Part 1: Terminology and performance requirements
• EN 3741:2004 Aerospace series – Nuts, clip, metric – Installation holes and assembly
• EN 374-2:2003 Protective gloves against chemicals and micro-organisms – Part 2: Determination of resistance to penetration
• EN 374-3:2003 Protective gloves against chemicals and micro-organisms – Part 3: Determination of resistance to permeation by chemicals
• EN 374-3:2003/AC:2006 Protective gloves against chemicals and micro-organisms – Part 3: Determination of resistance to permeation by chemicals
• EN 3745-100:2008 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 100: General
• EN 3745-201:2002 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 201: Visual examination
• EN 3745-202:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 202: Fibre dimensions
• EN 3745-203:2008 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 203: Cable dimensions
• EN 3745-205:2002 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 205: Cable longitudinal dimensional stability
• EN 3745-301:2012 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 301: Attenuation
• EN 3745-302:2002 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 302: Numerical aperture
• EN 3745-303:2007 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 303: Bandwidth
• EN 3745-305:2002 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 305: Immunity to ambient light coupling
• EN 3745-306:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 306: Variation of attenuation during temperature cycling
• EN 3745-401:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 401: Accelerated ageing
• EN 3745-402:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 402: Temperature cycling
• EN 3745-404:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 404: Thermal shock
• EN 3745-405:2012 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 405: Low/High temperature bend test
• EN 3745-406:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 406: Cold bend test
• EN 3745-407:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 407: Flammability
• EN 3745-410:2007 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 410: Thermal life
• EN 3745-411:2007 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 411: Resistance to fluids
• EN 3745-412:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 412: Humidity resistance
• EN 3745-501:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 501: Optical fibre proof test
• EN 3745-502:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 502: Tensile stength for short length of optical fibres
• EN 3745-503:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 503: Scrape abrasion
• EN 3745-504:2002 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 504: Micro bending test
• EN 3745-505:2007 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 505: Cable tensile strength
• EN 3745-506:2009 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 506: Impact resistance
• EN 3745-507:2002 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 507: Cut-through
• EN 3745-508:2002 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 508: Torsion
• EN 3745-509:2002 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 509: Kink test
• EN 3745-510:2012 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 510: Bending test
• EN 3745-511:2002 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 511: Cable to cable abrasion
• EN 3745-512:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 512: Flexure endurance
• EN 3745-513:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 513: Crush resistance
• EN 3745-514:2009 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 514: Cable twist bend
• EN 3745-515:2012 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 515: Buffer insertion force
• EN 3745-516:2012 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 516: Severe cable bend test
• EN 3745-517:2012 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 517: Cable tie clamping test
• EN 3745-601:2007 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 601: Smoke density
• EN 3745-602:2008 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 602: Toxicity
• EN 3745-603:2008 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 603: Nuclear radiation
• EN 3745-701:2002 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 701: Strippability
• EN 3745-703:2005 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 703: Durability of manufacturer’s marking
• EN 3745-705:2007 Aerospace series – Fibres and cables, optical, aircraft use – Test methods – Part 705: Contrast measurement
• EN 3746:2007 Aerospace series – O-rings, in fluorosilicone rubber (FVMQ) – Hardness 80 IRHD
• EN 3747:2007 Aerospace series – O-rings, in fluorosilicone rubber (FVMQ) – Technical specification
• EN 3748:2001 Aerospace series – O-ring grooves – Dimensions
• EN 3750:2010 Aerospace series – Nuts, anchor, self-locking, fixed, 90° corner, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature) / 315 °C
• EN 3752:2004 Aerospace series – Nuts, self-locking, MJ threads, in heat resisting steel FE-PA2601 (A286), MoS2 coated – Classification: 1 100 MPa (at ambient temperature) / 425 °C – Technical specification
• EN 3753:2010 Aerospace series – Nuts, anchor, self-locking, fixed, 60° corner, with counterbore, in alloy steel, cadmium plated, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature) / 235 °C
• EN 3757:2009 Aerospace series – Nuts, anchor, self-locking, floating, self-aligning, two lugs, in heat resisting steel, MoS2 lubricated – Classification: 900 MPa (at ambient temperature) / 315 °C
• EN 3759:1996 Aerospace series – Screws, pan head, offset cruciform recess, threaded to head, in heat and corrosion resisting steel, passivated – Classification: 1 100 MPa (at ambient temperature)/425 °C
• EN 3760:1996 Aerospace series – Screws, 100° countersunk normal head, offset cruciform recess, threaded to head, in heat and corrosion resisting steel, passivated – Classification: 1 100 MPa (at ambient temperature)/425 °C
• EN 3763:2010 Aerospace series – Nuts, hexagonal, self-locking, ball seat, in heat resisting steel, MoS2 lubricated – Classification: 900 MPa (at ambient temperature) / 315 °C
• EN 3768:2012 Aerospace series – Nuts, anchor, self-locking, one lug, fixed, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315 °C
• EN 3769:1997 Aerospace series – Electrolytic polishing of corrosion resisting steels and heat resisting alloys
• EN 377:1993 Lubricants for applications in appliances and associated controls using combustible gases except those designed for use in industrial processes
• EN 377:1993/A1:1996 Lubricants for applications in appliances and associated controls using combustible gases except those designed for use in industrial processes
• EN 3773-001:1999 Aerospace series – Circuit breakers, single-pole, temperature compensated, rated currents 1 A to 25 A, switching capacity 65 /n/1000 A max. – Part 001: Technical specification
• EN 3773-003:1999 Aerospace series – Circuit breakers, single-pole, temperature compensated, rated currents 1 A to 25 A, switching capacity 65 /n/1000 A max. – Part 003: Metric thread terminals – Product standard
• EN 3773-004:1999 Aerospace series – Circuit breakers, single-pole, temperature compensated, rated currents 1 A to 25 A, switching capacity 65 /n/1000 A max. – Part 004: UNC thread terminals – Product standard
• EN 3774-001:1999 Aerospace series – Circuit breakers, three-pole, temperature compensated, rated currents 2 A to 25 A, switching capacity 25 /n – Part 001: Technical specification
• EN 3774-003:1999 Aerospace series – Circuit breakers, three-pole, temperature compensated, rated currents 2 A to 25 A, switching capacity 65 /n – Part 003: Metric thread terminals – Product standard
• EN 3774-004:1999 Aerospace series – Circuit breakers, three-pole, temperature compensated, rated currents 2 A to 25 A, switching capacity 65 /n – Part 004: UNC thread terminals – Product standard
• EN 3777:2010 Aerospace series – Pins, quick release, single and double acting – Technical specification
• EN 3781:2008 Aerospace series – Grooves for spiral wound retaining rings – Design standard
• EN 378-1:2008+A2:2012 Refrigerating systems and heat pumps – Safety and environmental requirements – Part 1: Basic requirements, definitions, classification and selection criteria
• EN 3782:2008 Aerospace series – Holes for 100° countersunk head screws – Design standard
• EN 378-2:2008+A2:2012 Refrigerating systems and heat pumps – Safety and environmental requirements – Part 2: Design, construction, testing, marking and documentation
• EN 378-3:2008+A1:2012 Refrigerating systems and heat pumps – Safety and environmental requirements – Part 3: Installation site and personal protection
• EN 3783:2013 Aerospace series – Fibre composite materials – Normalisation of fibre dominated mechanical properties
• EN 378-4:2008+A1:2012 Refrigerating systems and heat pumps – Safety and environmental requirements – Part 4: Operation, maintenance, repair and recovery
• EN 3788:2001 Aerospace series – Pipe coupling 8°30′ – Protective caps
• EN 3788:2001/AC:2003 Aerospace series – Pipe coupling 8°30′ – Protective caps
• EN 3789:2001 Aerospace series – Pipe coupling 8°30′ – Protective plugs with external threads
• EN 3789:2001/AC:2003 Aerospace series – Pipe coupling 8°30′ – Protective plugs with external threads
• EN 379:2003+A1:2009 Personal eye-protection – Automatic welding filters
• EN 3790:2001 Aerospace series – Pipe coupling 8°30′ – Protective caps with internal threads
• EN 3790:2001/AC:2003 Aerospace series – Pipe coupling 8°30′ – Protective caps with internal threads
• EN 3-8:2006 Portable fire extinguishers – Part 8: Additional requirements to EN 3-7 for the construction, resistance to pressure and mechanical tests for extinguishers with a maximum allowable pressure equal to or lower than 30 bar
• EN 3-8:2006/AC:2007 Portable fire extinguishers – Part 8: Additional requirements to EN 3-7 for the construction, resistance to pressure and mechanical tests for extinguishers with a maximum allowable pressure equal to or lower than 30 bar
• EN 380:1993 Timber structures – Test methods – General principles for static load testing
• EN 381-1:1993 Protective clothing for users of hand-held chainsaws – Part 1: Test rig for testing resistance to cutting by a chainsaw
• EN 381-10:2002 Protective clothing for users of hand-held chainsaws – Part 10: Test method for upper body protectors
• EN 381-11:2002 Protective clothing for users of hand-held chainsaws – Part 11: Requirements for upper body protectors
• EN 381-2:1995 Protective clothing for users of hand-held chain saws – Part 2: Test methods for leg protectors
• EN 381-3:1996 Protective clothing for users of hand-held chain-saws – Part 3: Test methods for footwear
• EN 3813:2013 Aerospace series – Titanium alloy TI-P64001 (Ti-6Al-4V) – Annealed – Bar and wire for forged fasteners – De = 50 mm
• EN 381-4:1999 Protective clothing for users of hand-held chainsaws – Part 4: Test methods for chainsaw protective gloves
• EN 381-5:1995 Protective clothing for users of hand-held chain saws – Part 5: Requirements for leg protectors
• EN 3816:2006 Aerospace series – Steel FE-PA3601 (X6CrNiTi18-10) – Air melted – Softened and cold rolled – Sheet and strip a = 3 mm – Rm = 800 MPa
• EN 381-7:1999 Protective clothing for users of hand-held chainsaws – Part 7: Requirements for chainsaw protective gloves
• EN 381-8:1997 Protective clothing for users of hand-held chain saws – Part 8: Test methods for chain saw protective gaiters
• EN 3818:2004 Aerospace series – Bolts, MJ threads, in titanium alloy TI-P64001 – Strength class: 1 100 MPa (at ambient temperature) – Technical specification
• EN 381-9:1997 Protective clothing for users of hand-held chain saws – Part 9: Requirements for chain saw protective gaiters
• EN 3819:2008 Aerospace series – Clearance for wrenches and sockets
• EN 3820:2006 Aerospace series – Metric bolts, normal hexagon head, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated – Classification: 1 100 MPa (at ambient temperature)/315 °C
• EN 382-1:1993 Fibreboards – Determination of surface absorption – Part 1: Test method for dry process fibreboards
• EN 382-2:1993 Fibreboards – Determination of surface absorption – Part 2: Test method for hardboards
• EN 383:2007 Timber Structures – Test methods – Determination of embedment strength and foundation values for dowel type fasteners
• EN 3831:2004 Aerospace series – Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH), MoS2 coated
• EN 3832:2004 Aerospace series – Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) – Classification: 1 550 MPa (at ambient temperature) / 650 °C
• EN 3833:2004 Aerospace series – Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), passivated – Classification: 1 550 MPa (at ambient temperature) / 650 °C – Technical specification
• EN 3834:2010 Aerospace series – Nuts, anchor, self-locking, floating, two lug, incremental counterbore, in corrosion resisting steel, MoS2 lubricated – Classification: 900 MPa (at ambient temperature) / 315 °C
• EN 3838:2010 Aerospace series – Requirements and tests on user-applied markings on aircraft electrical cables
• EN 384:2010 Structural timber – Determination of characteristic values of mechanical properties and density
• EN 3840:2007 Aerospace series – Paints and varnishes – Technical specification
• EN 3841-100:2004 Aerospace series – Circuit breakers – Test methods – Part 100: General
• EN 3841-201:2004 Aerospace series – Circuit breakers – Test methods – Part 201: Visual inspection
• EN 3841-202:2004 Aerospace series – Circuit breakers – Test methods – Part 202: Dimensions and masses
• EN 3841-301:2004 Aerospace series – Circuit breakers – Test methods – Part 301: Voltage drop
• EN 3841-302:2004 Aerospace series – Circuit breakers – Test methods – Part 302: Insulation resistance
• EN 3841-303:2004 Aerospace series – Circuit breakers – Test methods – Part 303: Dielectric strength
• EN 3841-304:2004 Aerospace series – Circuit breakers – Test methods – Part 304: Tripping points
• EN 3841-305:2004 Aerospace series – Circuit breakers – Test methods – Part 305: Short-circuit performance
• EN 3841-306:2004 Aerospace series – Circuit breakers – Test methods – Part 306: Service life
• EN 3841-307:2004 Aerospace series – Circuit breakers – Test methods – Part 307: Performance with a locked tripping system
• EN 3841-308:2004 Aerospace series – Circuit breakers – Test methods – Part 308: Lightning
• EN 3841-401:2004 Aerospace series – Circuit breakers – Test methods – Part 401: Sand and dust
• EN 3841-402:2004 Aerospace series – Circuit breakers – Test methods – Part 402: Corrosion
• EN 3841-403:2004 Aerospace series – Circuit breakers – Test methods – Part 403: Humidity
• EN 3841-404:2004 Aerospace series – Circuit breakers – Test methods – Part 404: Explosion proofness
• EN 3841-405:2004 Aerospace series – Circuit breakers – Test methods – Part 405: Fluid resistance
• EN 3841-406:2004 Aerospace series – Circuit breakers – Test methods – Part 406: Flammability
• EN 3841-407:2004 Aerospace series – Circuit breakers – Test methods – Part 407: Temperature variation
• EN 3841-501:2004 Aerospace series – Circuit breakers – Test methods – Part 501: Actuator button travel
• EN 3841-502:2004 Aerospace series – Circuit breakers – Test methods – Part 502: Operating forces
• EN 3841-503:2004 Aerospace series – Circuit breakers – Test methods – Part 503: Strength of actuating components
• EN 3841-504:2004 Aerospace series – Circuit breakers – Test methods – Part 504: Strength of mounting elements
• EN 3841-505:2004 Aerospace series – Circuit breakers – Test methods – Part 505: Strength of main terminals
• EN 3841-506:2004 Aerospace series – Circuit breakers – Test methods – Part 506: Vibration performance
• EN 3841-507:2004 Aerospace series – Circuit breakers – Test methods – Part 507: Mechanical shocks
• EN 3841-508:2004 Aerospace series – Circuit breakers – Test methods – Part 508: Centrifugal acceleration
• EN 3841-509:2004 Aerospace series – Circuit breakers – Test methods – Part 509: Insertion and extraction forces of signal contact terminals
• EN 3841-510:2004 Aerospace series – Circuit breakers – Test methods – Part 510: Strength of signal contact terminals
• EN 3841-511:2004 Aerospace series – Circuit breakers – Test methods – Part 511: Combined test: temperature, altitude and vibration
• EN 3842:2001 Aerospace series – Circular tubes for fluids in corrosion resistant steel – Diameter 3,2 mm < = D < = 100 mm – Thickness 0,32 mm < = a < = 2,5 mm – Dimensions
• EN 3843:2010 Aerospace series – Nuts, bihexagonal, self-locking, with counterbore, in heat resisting steel, passivated – Classification: 1 100 MPa (at ambient temperature) / 650 °C
• EN 3844-1:2011 Aerospace series – Flammability of non metallic materials – Part 1: Small burner test, vertical – Determination of the vertical flame propagation
• EN 3844-2:2011 Aerospace series – Flammability of non metallic materials – Part 2: Small burner test, horizontal – Determination of the horizontal flame propagation
• EN 3844-3:2011 Aerospace series – Flammability of non metallic materials – Part 3: Small burner test, 45° – Determination of the resistance of material to flame and glow propagation and to flame penetration
• EN 3848:2001 Aerospace series – Semi-finished metallic products – Methods of measuring form deviations
• EN 3851:2003 Aerospace series – Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 – Swivel nuts, straight
• EN 3852:2002 Aerospace series – Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 – Straight unions, welded, threaded
• EN 3853:2002 Aerospace series – Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 – Straight unions, threaded
• EN 3854:2002 Aerospace series – Pipe couplings, 60°, spherical in titanium alloy TI-P64001 – Ferrules, welded
• EN 3855:2002 Aerospace series – Pipe couplings, 60°, spherical in titanium alloy TI-P64001 – Caps
• EN 3856:2002 Aerospace series – Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 – Swivel nuts for thrust wire
• EN 3857:2002 Aerospace series – Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 – Elbows 90°, welded
• EN 3858:2002 Aerospace series – Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 – Thrust wires in steel FE-PA 13
• EN 3861:2013 Aerospace series – Non-metallic materials – Glass transparencies – Material standard – Thermally tempered soda lime float glass
• EN 3862:2013 Aerospace series – Non-metallic materials – Glass transparencies – Material standard – Chemically tempered soda lime float glass
• EN 3863:2013 Aerospace series – Non-metallic materials – Glass transparencies – Test methods – Determination of flatness
• EN 3864:2013 Aerospace series – Non-metallic materials – Glass transparencies – Test methods – Determination of modulus of rupture
• EN 3866:2013 Aerospace series – Non-metallic materials – Glass tranparencies – Test methods – Determination of ream and surface ripple
• EN 3867:2004 Aerospace series – Pipe couplings, loose flanges and seals – Flanges in titanium alloy TI-P64001
• EN 3868:2004 Aerospace series – Pipe couplings, loose flanges and seals – Flange connectors, welded, in titanium alloy TI-P64001
• EN 3869:2004 Aerospace series – Pipe couplings, loose flanges and seals – Seals in fluorocarbon rubber and armature in aluminium alloy
• EN 3872:2005 Aerospace series – Aluminium alloy AL-R39002-H112 – Die forgings – a <200 mm
• EN 3873:2010 Aerospace series – Test methods for metallic materials – Determination of fatigue crack growth rates using Corner-Cracked (CC) test pieces
• EN 388:2003 Protective gloves against mechanical risks
• EN 3882:2001 Aerospace series – Heat resisting alloy NI-WH1801 (NiCr20Co18Ti3Al2) – Filler metal for welding
• EN 3883:2001 Aerospace series – Heat resisting alloy NI-WH2301 (NiCr22Fe19Mo9Co2) – Filler metal for welding
• EN 3884:2001 Aerospace series – Heat resisting alloy NI-WH2601 (NiCr19Nb5Mo3Ti) – Filler metal for welding
• EN 3885:2001 Aerospace series – Heat resisting alloy NI-WH3601 (NiCr22Mo9Nb4) – Filler metal for welding
• EN 3886:2001 Aerospace series – Heat resisting alloy NI-WH1303 (NiCo20Cr20Mo5Ti2Al) – Filler metal for welding
• EN 3887:2001 Aerospace series – Heat resisting alloy CO-WH4101 (CoCr20W15Ni) – Filler metal for welding
• EN 3888:2001 Aerospace series – Heat resisting alloy CO-WH1402 (CoCr22Ni22W15) – Filler metal for welding
• EN 3889:2001 Aerospace series – Steel FE-WM3801 (X5CrNiCu17-4) – Filler metal for welding
• EN 3890:2001 Aerospace series – Steel FE-WM1502 (X11CrNiMoVN12-3) – Filler metal for welding
• EN 3892:2001 Aerospace series – Titanium alloy TI-W64001 – Filler metal for welding
• EN 3893:2001 Aerospace series – Titanium alloy TI-W19001 – Filler metal for welding
• EN 3894:2001 Aerospace series – Heat resisting alloy NI-WD3201 (NiMo25Fe6Cr5) – Filler metal for welding
• EN 3895:2001 Aerospace series – Heat resisting alloy NI-WH3901 (NiCr16Mo15) – Filler metal for welding
• EN 3896:2001 Aerospace series – Steel FE-WM1501 (X13CrNiMoCo12-3-2-2) – Filler metal for welding
• EN 3897:2001 Aerospace series – Steel FE-WA4801 (X6CrNiMnNb18-10) – Filler metal for welding
• EN 3899:2004 Aerospace series – Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH) – Technical specification
• EN 39:2001 Loose steel tubes for tube and coupler scaffolds – Technical delivery conditions
• EN 3-9:2006 Portable fire extinguishers – Part 9: Additional requirements to EN 3-7 for pressure resistance of CO2 extinguishers
• EN 3-9:2006/AC:2007 Portable fire extinguishers – Part 9: Additional requirements to EN 3-7 for pressure resistance of CO2 extinguishers
• EN 3905:2008 Aerospace series – Six lobe recesses for bolts – Technical specification
• EN 3907:2004 Aerospace series – Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated – Classification: 1 100 MPa (at ambient temperature) / 350 °C
• EN 3909:2007 Aerospace series – Test fluids and test methods for electric components and sub-assemblies
• EN 3911:2010 Aerospace series – Six lobe recess – Geometrical definition
• EN 3912:2007 Aerospace series – Bolts, pan head, six lobe recess, relieved shank, long thread, in heat resisting steel FE-PA2601 (FE-PA92HT, A286), silver plated – Classification: 1 100 MPa (at ambient temperature) / 650 °C
• EN 3913:2007 Aerospace series – Insert, thin wall, self-locking, short, in heat resisting nickel base alloy NI-PH2601 (Ni-P100HT, Inconel 718), silver plated on internal thread, for salvage of components
• EN 3914:2008 Aerospace series – Insert, thin wall, self-locking, long, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), silver plated on internal thread, for salvage of components
• EN 3915:2008 Aerospace series – Insert, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), for salvage of components – Classification: 1 275 MPa (at ambient temperature) / 550 °C – Technical specification
• EN 3916:2008 Aerospace series – Insert, thin wall – Salvage procedure for components
• EN 3917:1998 Aerospace series – Nickel base alloy NI-B41201 (NiCr14Si5B3C) – Filler metal for brazing – Powder or paste
• EN 3918:1998 Aerospace series – Nickel base alloy NI-B41201 (NiCr14Si5B3C) – Filler metal for brazing – Tape
• EN 3919:1998 Aerospace series – Nickel base alloy NI-B41202 (NiCr14Si5B3) – Filler metal for brazing – Amorphous foil
• EN 3920:2001 Aerospace series – Nickel base alloy NI-B41202 (NiCr14Fe5Si5B3) – Filler metal for brazing – Powder or paste
• EN 3921:2001 Aerospace series – Nickel base alloy NI-B41203 (NiCr7Si5B3) – Filler metal for brazing – Amorphous foil
• EN 3922:1998 Aerospace series – Nickel base alloy Ni-B41203 (NiCr7Si5B3) – Filler metal for brazing – Borided foil
• EN 3923:2001 Aerospace series – Nickel base alloy NI-B41203 (NiCr7Si5B3Fe3) – Filler metal for brazing – Powder or paste
• EN 3924:1998 Aerospace series – Nickel base alloy NI-B41203 (NiCr7Si5B3) – Filler metal for brazing – Tape
• EN 3925:2001 Aerospace series – Nickel base alloy NI-B40001 (NiSi5B3) – Filler metal for brazing – Amorphous foil
• EN 3926:2001 Aerospace series – Nickel base alloy NI-B40001 (NiSi5B3) – Filler metal for brazing – Borided foil
• EN 3927:2001 Aerospace series – Nickel base alloy NI-B40001 (NiSi5B3) – Filler metal for brazing – Powder or paste
• EN 3928:1998 Aerospace series – Nickel base alloy NI-B40001 (NiSi5B3) – Filler metal for brazing – Tape
• EN 3930:2001 Aerospace series – Nickel base alloy NI-B31001 (NiCr19Si10) – Filler metal for brazing – Powder or paste
• EN 3931:1998 Aerospace series – Nickel base alloy NI-B31001 (NiCr19Si10) – Filler metal for brazing – Tape
• EN 3932:2001 Aerospace series – Nickel base alloy NI-B13001 (NiP11) – Filler metal for brazing – Amorphous foil
• EN 3933:2001 Aerospace series – Nickel base alloy NI-B13001 (NiP11) – Filler metal for brazing – Powder or paste
• EN 3934:2001 Aerospace series – Nickel base alloy NI-B21001 (NiCr15B4) – Filler metal for brazing – Amorphous foil
• EN 3935:2001 Aerospace series – Nickel base alloy NI-B21001 (NiCr15B4) – Filler metal for brazing – Borided foil
• EN 3936:2001 Aerospace series – Nickel base alloy NI-B21001 (NiCr15B4) – Filler metal for brazing – Powder or paste
• EN 3937:2001 Aerospace series – Nickel base alloy NI-B44101 (NiW12Cr10Si4Fe3B3) – Filler metal for brazing – Powder or paste
• EN 3938:2001 Aerospace series – Nickel base alloy NI-B46001 (NiCo20Si5B3) – Filler metal for brazing – Amorphous foil
• EN 3939:2001 Aerospace series – Nickel base alloy NI-B46001 (NiCo20Si5B3) – Filler metal for brazing – Powder or paste
• EN 3940:1998 Aerospace series – Nickel base alloy NI-B46001 (NiCoSi5B3) – Filler metal for brazing – Tape
• EN 3941:2001 Aerospace series – Nickel base alloy NI-B41204 (NiCr13Si4B3) – Filler metal for brazing – Amorphous foil
• EN 3942:2001 Aerospace series – Nickel base alloy NI-B41204 (NiCr13Si4B3) – Filler metal for brazing – Borided foil
• EN 3943:2001 Aerospace series – Nickel base alloy NI-B41204 (NiCr13Fe4Si4B3) – Filler metal for brazing – Powder or paste
• EN 3944:1998 Aerospace series – Nickel base alloy NI-B41204 (NiCr13Si4B3) – Filler metal for brazing – Tape
• EN 3945:2001 Aerospace series – Nickel base alloy NI-B48801 (NiMn19Si6Cu4B) – Filler metal for brazing – Powder or paste
• EN 3946:2001 Aerospace series – Nickel base alloy NI-B15701 (NiPd34Au30) – Filler metal for brazing – Powder or paste
• EN 3947:1998 Aerospace series – Nickel base alloy NI-B15701 (NiPd34Au30) – Filler metal for brazing – Rolled foil
• EN 3948:1998 Aerospace series – Nickel base alloy NI-B15701 (NiPd34Au30) – Filler metal for brazing – Wire
• EN 3952:2001 Aerospace series – Silver base alloy AG-B10001 (AgCu28) – Filler metal for brazing – Wire
• EN 3953:2001 Aerospace series – Silver base alloy AG-B12401 (AgCu40Zn5Ni) – Filler metal for brazing – Wire
• EN 3954:2001 Aerospace series – Silver base alloy AG-B12401 (AgCu40Zn5Ni) – Filler metal for brazing – Powder or paste
• EN 3955:2001 Aerospace series – Silver base alloy AG-B12401 (AgCu40Zn5Ni) – Filler metal for brazing – Rolled foil
• EN 3956:2001 Aerospace series – Silver base alloy AG-B14001 (AgCu42Ni2) – Filler metal for brazing – Wire
• EN 3957:2001 Aerospace series – Silver base alloy AG-B14001 (AgCu42Ni2) – Filler metal for brazing – Powder or paste
• EN 3958:2001 Aerospace series – Silver base alloy AG-B14001 (AgCu42Ni2) – Filler metal for brazing – Rolled foil
• EN 3959:2001 Aerospace series – Cobalt base alloy CO-B41601 (CoCr19Ni17Si8W4) – Filler metal for brazing – Powder or paste
• EN 3960:2001 Aerospace series – Gold base alloy AU-B40001 (AuNi18) – Filler metal for brazing – Powder or paste
• EN 3960:2001/AC:2002 Aerospace series – Gold base alloy AU-B40001 (AuNi18) – Filler metal for brazing – Powder or paste
• EN 3961:2001 Aerospace series – Gold base alloy AU-B40001 – Filler metal for brazing – Rolled foil
• EN 3962:2001 Aerospace series – Gold base alloy AU-B40001 – Filler metal for brazing – Wire
• EN 3963:2001 Aerospace series – Copper CU-BU9001 – Filler metal for brazing – Rolled foil
• EN 3964:2001 Aerospace series – Copper CU-BU9001 – Filler metal for brazing – Wire
• EN 3965:2001 Aerospace series – Titanium alloy TI-B17001 – Filler metal for brazing – Rolled foil
• EN 3969:2006 Aerospace series – Steel FE-PL1507 (40CrMoV12) – Air melted – Annealed – Forging stock – a or D = 350 mm
• EN 397:2012+A1:2012 Industrial safety helmets
• EN 3971:2006 Aerospace series – Steel FE-PL1507 (40CrMoV12) – Consumable electrode remelted – Annealed – Forging stock – a or D = 350 mm
• EN 3972:2006 Aerospace series – Steel FE-PL1507 (40CrMoV12) – Consumable electrode remelted – Hardened and tempered – Bar for machining – De = 50 mm – 1 250 MPa = Rm = 1 400 MPa
• EN 3973:2006 Aerospace series – Steel FE-CM3801 (X5CrNiCuNb16-4) – Homogenized, solution treated and precipitation hardened – Investment casting – De = 50 mm – Rm = 1 030 MPa
• EN 3976:2006 Aerospace series – Titanium and titanium alloys – Test method – Chemical analysis for the determination of hydrogen content
• EN 3979:2005 Aerospace series – Aluminium alloy AL-P8090-O2 – Sheet for superplastic forming (SPF) – 0,8 mm < a < 6 mm
• EN 3983:2013 Aerospace series – Aluminium alloy AL-P7050- – T7651 – Plate – 6 mm < a = 160 mm
• EN 3987:2009 Aerospace series – Test methods for metallic materials – Constant amplitude force-controlled high cycle fatigue testing
• EN 3997:2007 Aerospace series – Aluminium alloy AL-P2024-T3 – Sheet and strip 0,4 mm = a = 6 mm
• EN 3998:2007 Aerospace series – Aluminium alloy AL-P2024-T4 or T42 – Sheet and strip 0,3 mm = a = 6 mm
• EN 3999:2007 Aerospace series – Aluminium alloy AL-P2024-T351 – Sheet and strip with improved chemical milling capability 1,6 mm = a = 6 mm

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