EN European Norm Tests Part 45

EN Standards are European Standards. These standards specify requirements for a particular item, material, component, system or service, or describe in detail a particular method or procedure, and tests are performed accordingly.

• EN 3475-407 : 2009 ; Aviation series. Cables, electricity, aircraft use. Test methods. flammability
• EN 3475-408 : 2005 ; Aviation series. Cables, electricity, aircraft use. Test methods. fire resistance
• EN 3475-411 : 2005 ; Aviation series. Cables, electricity, aircraft use. Test methods. Resistance to liquids
• EN 3475-411 : 2014 ; Aviation series. Cables, electricity, aircraft use. Test methods. Resistance to liquids
• EN 3475-414: 2005; Aviation series. Cables, electricity, aircraft use. Test methods. Differential scanning calorimetry (DSC test)
• EN 3475-415 : 2005 ; Aviation series. Cables, electricity, aircraft use. Test methods. rapid temperature change
• EN 3475-416 : 2005 ; Aviation series. Cables, electricity, aircraft use. Test methods. thermal stability
• EN 3475-417 : 2009 ; Aviation series. Cables, electricity, aircraft use. Test methods. Fire resistance of cables trapped in a harness
• EN 3475-418 : 2007 ; Aviation series. Cables, electricity, aircraft use. Test methods. Thermal endurance for conductors
• EN 3475-501 : 2006 ; Aviation series. Cables, electricity, aircraft use. Test methods. dynamic transition
• EN 3475-505 : 2007 ; Aviation series. Cables, electricity, aircraft use. Test methods. Tensile test on conductors and wires
• EN 3475-505 : 2012 ; Aviation series. Cables, electricity, aircraft use. Test methods. Tensile test on conductors and wires
• EN 3475-506 : 2007 ; Aviation series. Cables, electricity, aircraft use. Test methods. Coating continuity
• EN 3475-507 : 2007 ; Aviation series. Cables, electricity, aircraft use. Test methods. Adhesion of the coating
• EN 3475-508 : 2007 ; Aviation series. Cables, electricity, aircraft use. Test methods. Coating thickness
• EN 3475-513 : 2005 ; Aviation series. Cables, electricity, aircraft use. Test methods. Deformation resistance (installation with plastic cable ties)
• EN 3475-514 : 2007 ; Aviation series. Cables, electricity, aircraft use. Test methods. Porosity of copper coating on aluminum strips
• EN 3475-514 : 2014 ; Aviation series. Cables, electricity, aircraft use. Test methods. Porosity of copper coating on aluminum strips
• EN 3475-515 : 2009 ; Aviation series. Cable, electricity, aircraft use. Test methods. crush resistance
• EN 3475-601 : 2007 ; Aviation series. Cables, electricity, aircraft use. Test methods. smoke density
• EN 3475-602: 2007; Aviation series. Cables, electricity, aircraft use. Test methods. toxicity
• EN 3475-603 : 2007 ; Aviation series. Cables, electricity, aircraft use. Test methods. Resistance to wet arc tracking
• EN 3475-603 : 2011 ; Aviation series. Cables, electricity, aircraft use. Test methods. Resistance to wet arc tracking
• EN 3475-604: 2010; Aviation series. Cables, electricity, aircraft use. Test methods. Resistance to dry arc propagation
• EN 3475-605: 2010; Aviation series. Cables, electricity, aircraft use. Test methods. Wet short circuit test
• EN 3475-704 : 2007 ; Aviation series. Cables, electricity, aircraft use. Test methods. Flexibility
• EN 3475-705 : 2005 ; Aviation series. Cable, electricity, aircraft use. Test methods. Contrast measurement
• EN 3475-706 : 2005 ; Aviation series. Cables, electricity, aircraft use. Test methods. laser markability
• EN 3475-802 : 2009 ; Aviation series. Cables, electricity, aircraft use. Test methods. capacitance imbalance
• EN 3475-809 : 2009 ; Aviation series. Cables, electricity, aircraft use. Test methods. resistance imbalance
• EN 3475-810: 2009; Aviation series. Cables, electricity, aircraft use. Test methods. Structural loss of return
• EN 3475-811 : 2009 ; Aviation series. Cables, electricity, aircraft use. Test methods. imbalance weight loss
• EN 3475-812 : 2009 ; Aviation series. Cables, electricity, aircraft use. Test methods. Return loss (VSWR)
• EN 3476 : 2006 ; Aviation series. Steel FE-PL1501 (30CrMo12). The air has melted. Softened. Tattoo stock. a or D 3L 300 mm.
• EN 3479 : 2007 ; Aviation series. Steel FE-PM1802 (X5CrNiCu15-5). The consumable electrode was remelted. Solution treated and precipitation treated. Plate. 6mm 0L and 3L 20mm. 1070 MPa 3L Rm 3L 1220 MPa.
• EN 3480 : 2007 ; Aviation series. Steel FE-PA3601 (X6CrNiTi18-10). The air has melted. Softened. Plate. 6mm $0L and 3L 50mm. 500 MPa 3L Rm 3L 700 MPa.
• EN 3487 : 2007 ; Aviation series. Steel FE-PA3601 (X6CrNiTi18-10). The air has melted. Softened. Bar for processing. a or D 3L 250 mm. 500 MPa 3L Rm 3L 700 MPa.
• EN 3488 : 2007 ; Aviation series. Steel FE-PA3601 (X6CrNiTi18-10). The air has melted. Softened. Sheet and strip. 3L 6mm. 500 MPa 3L Rm 3L 700 MPa.
• EN 3490: 2007; Aviation series. Steel FE-PM3901 (X15CrNi17-3). The air has melted. Hardened and tempered. Bar for processing. 3L 200mm. 900 MPa 3L Rm 3L 1100 MPa.
• EN 3491: 2006; Aviation series. Steel FE-PM3901 (X15CrNi17-3). The air has melted. Hardened and tempered. Tattoos. 3L 100mm. 900 MPa 3L Rm 3L 1100 MPa.
• EN 3507: 2006; Aviation series. Steel FE-PL1501 (30CrMo12). The air has melted. Hardened and tempered. Tattoos. 3L 100mm. 930 MPa 3L Rm 3L 1080 MPa.
• EN 3523: 2007; Aviation series. Steel FE-PL1505 (15CrMoV6). The air has melted. Hardened and tempered. Bar for processing. 3L 100mm. 1080 MPa $3L Rm $3L 1280 MPa.
• EN 3524 : 2007 ; Aviation series. Steel FE-PL1505 (15CrMoV6). The air has melted. Hardened and tempered. Sheet and strip. 2mm 3L and 3L 6mm. 1080 MPa $3L Rm $3L1280 MPa.
• EN 3525: 2007; Aviation series. Steel FE-PL1505 (15CrMoV6). The air has melted. Hardened and tempered. Plate. 6mm 3Q and 3L 20mm. 1080 MPa $3L Rm $3L 1280 MPa.
• EN 3526: 2007; Aviation series. Steel FE-PL1505 (15CrMoV6). The air has melted. Hardened and tempered. Sheet and strip. 0,5mm 3L and 3L 6mm. 980 MPa 3L Rm 3L 1180 MPa.
• EN 3527 : 2007 ; Aviation series. Steel FE-PL1504 (33CrMoV12). The air has melted. Softened. Tattoo stock. a or D 3L 300 mm.
• EN 3528: 2013; Aviation series. Steel X2NiCoMo18-8-5 (1;6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Rod. a or D 3L 150 mm. 1 750 MPa 3L Rm 3L 2 000 MPa.
• EN 3529: 2010; Aviation series. Steel FE-PM2701 (X2NiCoMo18-8-5). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Tattoos. a or D 3L 150 mm. 1750 MPa 3L Rm 3L 2000 MPa.
• EN 3531: 2007; Aviation series. Steel FE-PM2701 (X2NiCoMo18-8-5). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Sheet and strip. 3L 6mm. 1750 MPa 3L Rm 3L 2000 MPa.
• EN 3532: 2007; Aviation series. Steel FE-PM2701 (X2NiCoMo18-8-5). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated plate. 6mm 0L and 3L 40mm. 1750 MPa 3L Rm 3L 2000 MPa.
• EN 3536: 2006; Aviation series. Nuts, hexagonal, self-locking, of heat-resistant steel, MoS2 lubricated. Classification : 1100 MPa (at ambient temperature)/315^DC.
• EN 3537: 2010; Aviation series. Nuts, anchor, self-locking, fixed, two-lug, countersunk, of heat-resistant steel, MoS2 lubricated. Classification : 1100 MPa (at ambient temperature)/315^DC.
• EN 3538: 2010; Aviation series. Nuts, anchor, self-locking, fixed, two lugs, reduced series, countersunk, of heat resistant steel, MoS2 lubricated. Classification : 1100 MPa (at ambient temperature)/315^DC.
• EN 3539: 2010; Aviation series. Nuts, anchor, self-locking, single shoe, fixed, countersunk, of heat-resistant steel, MoS2 lubricated. Classification : 1100 MPa (at ambient temperature)/315^DC.
• EN 3541: 1992; Tie rod ends, adjustable, self-aligning ball bearing with threaded shaft. Dimensions, torques, clearances and loads.
• EN 3542: 1998; Tips, thread, helical coil, self-locking, of heat-resistant nickel-based alloy NI-PH2801 (Inconel X750).
• EN 3543: 1997; Screws, 100$0D countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, heat and corrosion resistant steel, passivated. Classification : 1100 MPa (at ambient temperature)/425^DC.
• EN 3545-001: 2005; Aviation series. Connectors, electrical, rectangular, backsealed and sealed, plastic housing, locking device, operating temperatures -5 ^DC to 175 ^DC. Technical specification
• EN 3545-001: 2008; Aviation series. Connectors, electrical, rectangular, backsealed and sealed, plastic housing, locking device, operating temperatures -55^DC to 175^DC. Technical specification
• EN 3545-002: 2005; Aviation series. Connectors, electrical, rectangular, backsealed and sealed, plastic housing, locking device, operating temperatures – 55^DC to 175^DC. Features of performance and communication arrangements
• EN 3545-002 : 2008 ; Aviation series. Connectors, electrical, rectangular, back sealed and sealed, plastic housing, locking device, operating temperatures -55 ^DC to 175 ^DC . Features of performance and communication arrangements
• EN 3545-003: 2005; Aviation series. Connectors, electrical, rectangular, sealed and with sealed back, plastic housing, locking device, operating temperatures -55 ^DC to 175 ^DC. Female contact connectors. product standard
• EN 3545-004: 2005; Aviation series. Connectors, electrical, rectangular, sealed and with sealed back, plastic housing, locking device, operating temperatures -55 ^DC to 175 ^DC. Male contact connectors. product standard
• EN 3545-005 : 2006 ; Aviation series. Connectors, electrical, rectangular, backsealed and sealed, plastic housing, locking device, operating temperatures -55^DC to 175^DC. Male coding and connection system for free body (plug) mounting. product standard
• EN 3545-005: 2014; Aviation series. Connectors, electrical, rectangular, sealed and with sealed back, plastic housing, locking device, operating temperatures -55 ^DC to 175 ^DC. Female coding and connection system for free body (plug) mounting. product standard
• EN 3545-006: 2006; Aviation series. Connectors, electrical, rectangular, backsealed and sealed, plastic housing, locking device, operating temperatures -55^DC to 175^DC. Male coding and connection system for attaching to fixed body (slot). product standard
• EN 3545-006: 2015; Aviation series. Connectors, electrical, rectangular, backsealed and sealed, plastic housing, locking device, operating temperatures -55^DC to 175^DC. Male coding and attachment. System for mounting on a fixed body (slot). product standard
• EN 3545-007: 2005; Aviation series. Connectors, electrical, rectangular, sealed and with sealed back, plastic housing, locking device, operating temperatures -55 ^DC to 175 ^DC. Cable clamp. product standard
• EN 3545-007: 2014; Aviation series. Connectors, electrical, rectangular, backsealed and sealed, plastic housing, locking device, operating temperatures – 55 ^DC to 175 ^DC. Cable clamp. product standard
• EN 3545-008: 2006; Aviation series. Connectors, electrical, rectangular, backsealed and sealed, plastic housing, locking device, operating temperatures -55^DC to 175^DC. Tools for assembly/disassembly of coding and connection systems. product standard
• EN 3545-009 : 2008 ; Aviation series. Connectors, electrical, rectangular, sealed and with sealed back, plastic housing, locking device, operating temperatures -55 °C to 175 °C. Protective cover for plug and socket. product standard
• EN 3552 : 2005 ; Aviation series. Aluminum alloy AL-P2618A-T6 or T62 ; Coated sheet and strip. 0,4mm 3L and 3L 6mm.
• EN 3553: 2004; Aviation series. Aluminum alloy AL-P2618A-T6511 ; Extruded bar and section. a or D 3L 160 mm.
• EN 3611: 1995; spigots. Dimensions and selection. Design standard.
• EN 3613: 2009; Aviation series. Bolts, normal hex head, embossed shank, long thread, heat resistant nickel base alloy NIPH2601 (Inconel 718), silver plated. Classification : 1275 MPa/650 ^DC.
• EN 3614: 2009; Aviation series. Bolts, normal hex head, embossed shank, long thread, heat resistant steel FE-PA2601 (A286), silver plated. Classification : 900 MPa/650^DC.
• EN 3626: 2006; Aviation series. Nuts, hex, self-locking steel, cadmium plated, MoS$d2 lubricated. Classification : 1100 MPa (at ambient temperature) / 235^DC.
• EN 3630: 2008; Aviation series. Fluid fittings, flanged, straight. O-ring sealing for 0,8 mm thick pipes.
• EN 3631 : 2008 ; Aviation series. Fluid fittings, flanged, 90$0D elbow. O-ring sealing for 0,8 mm thick pipes.
• EN 3631 : 2014 ; Aviation series. Fluid fittings, flanged, 90$0D elbow. O-ring sealing for 0,8 mm thick pipes.
• EN 3633: 2008; Aviation series. Mounting hole for fluid fittings, flanged.
• EN 3635 : 2008 ; Aviation series. Source lip. Geometric configuration.
• EN 3635 : 2014 ; Aviation series. Source lip. Geometric configuration.
• EN 3636: 2008; Aviation series. Screws, reduced round head, offset cruciform recess, embossed stem, long thread, heat resistant steel FE-PA92HT (A286), silver plated. Classification : 900 MPa/650^DC.
• EN 3637 : 2008 ; Aviation series. Nuts, self-locking, two hexagons (double reduced), heat resistant nickel base alloy NI-P101HT (Waspaloy), silver plated, Classification : 1210 MPa/730 ^DC.
• EN 3638: 2007; Aviation series. Heat resistant alloy FE-PA2601 (X6NiCrTiMoV26-15). The consumable electrode was remelted. It was subjected to solution and precipitation treatment. Sheet, strip and sheet. 0,5mm 3L and 3L 10mm.
• EN 3642: 1997; Rivets, solid, 100$0D countersunk normal head, domed, titanium TI-PO2, anodized, inch base series.
• EN 3643: 1997; Rivets, solid, 100$0D countersunk regular head, titanium TI-PO2, anodized, inch base series.
• EN 3644: 1997; Rivets, solid, universal head, titanium TI-PO2, anodized, inch base series.
• EN 3645-001: 2007; Aviation series. Connectors, electric, circular, bucket guard, triple start threaded coupling, operating temperature 175^DC or continuous 200^DC. Technical specification
• EN 3645-001: 2013; Aviation series. Connectors, electric, circular, bucket guard, triple start threaded coupling, operating temperature 175^DC or continuous 200^DC. Technical specification
• EN 3645-001: 2015; Aviation series. Connectors, electric, circular, bucket guard, triple start threaded coupling, operating temperature 175^DC or continuous 200^DC. Technical specification
• EN 3645-002: 2007; Aviation series. Connectors, electric, circular, bucket guard, triple start threaded coupling, operating temperature 175^DC or continuous 200^DC. Features of performance and communication arrangements
• EN 3645-002: 2015; Aviation series. Connectors, electric, circular, bucket guard, triple start threaded coupling, operating temperature 175^DC or continuous 200^DC. Features of performance and communication arrangements
• EN 3645-003: 2006; Aviation series. Connectors, electric, circular, bucket guard, triple start threaded coupling, operating temperature 175^DC or continuous 200^DC. Socket square flange mounting. product standard
• EN 3645-003: 2015; Aviation series. Connectors, electric, circular, bucket guard, triple start threaded coupling, operating temperature 175 ^DC or 200 ^DC continuous. Socket square flange mounting. product standard
• EN 3645-004: 2006; Aviation series. Connectors, electric, circular, bucket guard, triple start threaded coupling, operating temperature 175^DC or continuous 200^DC. Socket, hermetic, square flange mounting. product standard
• EN 3645-005: 2006; Aviation series. Connectors, electric, circular, bucket guard, triple start threaded coupling, operating temperature 175^DC or continuous 200^DC. Socket, hermetic, round flange, brasage mounting. product standard
• EN 3645-006: 2006; Aviation series. Connectors, electric, circular, bucket guard, triple start threaded coupling, operating temperature 175^DC or continuous 200^DC. Protective cover for the socket. product standard
• EN 3645-006: 2015; Aviation series. Connectors, electric, circular, bucket guard, triple start threaded coupling, operating temperature 175^DC or continuous 200^DC. Protective cover for the socket. product standard

Standards facilitate international trade by ensuring compatibility and interoperability of components, products and services. European Standards (ENs) are documents approved by three European Standardization Organizations (ESO), CEN, CENELEC or ETSI; Recognized as competent in the field of voluntary technical standardization for EU Regulation 1025/2012.