EN European Norm Tests Part 40

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 2684: 2004; Aviation series. Aluminum alloy AL-P7010-T7651 ; Plate. 6mm $0L and 3L 140mm.
• EN 2687: 2004; Aviation series. Aluminum alloy AL-P7010-T7451 ; Plate. 6mm $0L and 3L 160mm.
• EN 2693: 1994; Aluminum alloy. AL-P5086-H111; Sheet and strip 0,3mm 3L and 3L 6mm.
• EN 2693: 2005; Aviation series. Aluminum alloy AL-P5086-H111 ; Sheet and strip. 0,3mm 3La 3L6mm.
• EN 2694: 1994; Aluminum alloy. AL-P6061-T6 or T62 ; Sheet and strip 0,4 mm 3L and 3L 6 mm.
• EN 2694: 2005; Aviation series. Aluminum alloy AL-P6061-T6 or T62 ; Sheet and strip. 0,4mm 3L and 3L 6mm.
• EN 2695 : 1994 ; Aluminum alloy. AL-P6081-T6 ; Sheet and strip 0,3mm 3L and 3L 6mm.
• EN 2695 : 2005 ; Aviation series. Aluminum alloy AL-P6081-T6 ; Sheet and strip. 0,3mm 3La 3L6mm.
• EN 2696: 1994; Aluminum alloy. AL-P7075-T6 or T62 ; Sheet and strip 0,4 mm 3L and 3L 6 mm.
• EN 2696 : 2005 ; Aviation series. Aluminum alloy AL-P7075-T6 or T62 ; Sheet and strip. 0,4mm 3La 3L6mm.
• EN 2702: 2005; Aviation series. Aluminum alloy. AL-P6061; T6 or T62 ; Drawn or extruded bar and section. a or D 3L 200 mm.
• EN 2703 : 2005 ; Aviation series. Aluminum alloy AL-P2024-T4 or T42 ; Coated sheet and strip. 0,3mm 3L and 3L 6mm.
• EN 2704: 2015; Aviation series. Aluminum alloy AL-P2024 ; AlCu4Mg1; T3511 ; Drawn sticks. Also 3L 75mm.
• EN 2713-002: 2006; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 200^DC. Screened and jacketed. general
• EN 2713-003: 2005; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 200 ^DC. Screen (spiral) and jacketed, inkjet printable. product standard
• EN 2713-004: 2006; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 200^DC. Screen (braided) and jacketed, inkjet printable. product standard
• EN 2713-005 : 2006 ; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 200^DC. Screened (spiral) and jacketed, CO2 laser printable. product standard
• EN 2713-006: 2006; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 200^DC. Screened (braided) and jacketed, CO$d2 ​​laser printable. product standard
• EN 2713-007: 2005; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 200^DC. Screen (spiral) and jacketed, UV laser printable. product standard
• EN 2713-008: 2006; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 200$0D. Screened (braided) and jacketed, UV laser printable. product standard
• EN 2713-009: 2006; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 200^DC. Screen (spiral) and jacketed, YAG X3 laser printable. product standard
• EN 2713-010: 2006; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 200^DC. Screened (braided) and jacketed, YAG X3 laser printable. product standard
• EN 2713-011: 2006; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 200^DC. Silver plated copper screen (spiral) and jacketed, UV laser printable. product standard
• EN 2714-002: 2005; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. Screened and jacketed. general
• EN 2714-002: 2012; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. Screened and jacketed. general
• EN 2714-003: 2005; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. Screen (spiral) and jacketed, inkjet printable. product standard
• EN 2714-004: 2006; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. Screen (braided) and jacketed, inkjet printable. product standard
• EN 2714-005 : 2006 ; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. Screened (spiral) and jacketed, CO2 laser printable. product standard
• EN 2714-006: 2006; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. Screened (braided) and jacketed, CO2 laser printable. product standard
• EN 2714-007: 2005; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. Screen (spiral) and jacketed, UV laser printable. product standard
• EN 2714-008: 2006; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. Screened (braided) and jacketed, UV laser printable. product standard
• EN 2714-009 : 2007 ; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55 ^DC to 260 ^DC. Screen (spiral) and jacketed, YAG X3 laser printable. product standard
• EN 2714-010: 2006; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. Screened (braided) and jacketed, YAG X3 laser Printable. product standard
• EN 2714-011: 2005; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. DM family, shielded (spiral) and jacketed, UV laser printable. product standard
• EN 2714-012: 2005; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. DM family, screened (braided) and jacketed, UV laser printable. product standard
• EN 2714-013: 2005; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. DR family, shielded (spiral) and jacketed, UV laser printable. product standard
• EN 2714-014: 2009; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55^DC to 260^DC. The DR family is 5 to 10 cores, taped, screened (braided) and sheathed, UV laser printable. product standard
• EN 2714-014: 2016; Aviation series. General purpose cables, electrical, single and multi-core. Operating temperatures from -55 ^DC to 260 ^DC. DR family, 4 to 11 cores, taped, screened (braided) and jacketed, UV laser printable. product standard
• EN 2731 : 2005 ; Aviation series. Magnesium alloy MG-C46001 ; T6 ; Sand casting.
• EN 2732: 2005; Magnesium alloy MG-C46001-T6 ; Cold casting.
• EN 2744: 1992; non-metallic materials. Preferred test temperatures.
• EN 2746: 1998; Glass fiber reinforced plastics. Bending test. Three point bending method.
• EN 2747: 1998; Glass fiber reinforced plastics. Tensile test.
• EN 2752 : 1990 ; Specifications for nut, anchor, self-locking fixed, two shoes, reduced series, countersunk. Classification : 1100 MPa/235^DC.
• EN 2753: 1996; Nuts, anchor, self-locking, fixed, single shoe, countersunk, alloy steel, cadmium plated, MoS$d2 lubricated. classification 1100 MPa (at ambient temperature) / 235^DC.
• EN 2754 : 2006 ; Aviation series. Nuts, anchor, self-locking, two lugs, countersunk floating. Classification : 1100 MPa/235^DC.
• EN 2755 : 2009 ; Aviation series. Bearings spherical plain of corrosion-resistant steel with self-lubricating lining. High load at ambient temperature. Technical specification.
• EN 2756: 2010; Aviation series. Lamps, incandescent. Test methods.
• EN 2757: 2011; Aviation series. Structural adhesives system. Test method. Determination of drying and ignition residues of primers.
• EN 2781: 1998; non-metallic materials. Structural adhesives. Test methods. Determination of lining thickness.
• EN 2786 : 2008 ; Aviation series. Electrolytic silver plating of fasteners.
• EN 2794-001: 1999; Circuit breakers, single pole, temperature compensated, rated currents 20 A - 50 A. Technical specifications
• EN 2794-001: 2014; Aviation series. Circuit breakers, single pole, temperature compensated, rated current 20 A - 50 A. Technical specifications
• EN 2794-003: 1999; Circuit breakers, single pole, temperature compensated, rated currents 20 A - 50 A. Metric threaded terminals. product standard
• EN 2794-004 : 1999 ; Circuit breakers, single pole, temperature compensated, rated currents 20 A - 50 A. UNC threaded terminals. product standard
• EN 2794-004: 2014; Aviation series. Circuit breakers, single pole, temperature compensated, rated currents 20 A - 50 A. UNC threaded terminals. product standard
• EN 2802: 2005; Aluminum alloy AL-P7475-T761 ; Sheet and strip. 0,6mm 3L and 3L 6mm.
• EN 2803: 2005; Aviation series. Aluminum alloy AL-P7475-T761 ; Coated sheet and strip. 1,0mm 3L and 3L 6mm.
• EN 2812: 2009; Aviation series. Stripping of electrical wires.
• EN 2815 : 2009 ; Aviation series. Steel FE-PM1802 (X5CrNiCu15-5). The consumable electrode was remelted. Solution treated and precipitation treated. Bar for processing. a or D 3L 200 mm. $3 million, 965 MPa.
• EN 2817 : 2009 ; Aviation series. Steel FE-PM1802 (X5CrNiCu15-5). The consumable electrode was remelted. Solution treated and precipitation treated. Bar for processing. a or D 3L 200 mm. $3 million, 1070 MPa.
• EN 2818: 2009; Aviation series. Steel FE-PM1802 (X5CrNiCu15-5). The consumable electrode was remelted. Solution treated and precipitation treated. Tattoos. a or D 3L 200 mm. $3 million, 1070 MPa.
• EN 2821 : 2007 ; Aviation series. Steel FE-PM1802 (X5CrNiCu15-5). The consumable electrode was remelted. Solution treated and precipitation treated. Bar for processing. a or D 3L 200 mm. $3 million, 1310 MPa.
• EN 2824: 2011; Aviation series. Combustion behavior of non-metallic materials under the influence of radiated heat and flames. Determination of smoke density and gas components in the smoke of materials. Test equipment apparatus and media.
• EN 2825: 2011; Aviation series. Combustion behavior of non-metallic materials under the influence of radiated heat and flames. Determination of smoke density.
• EN 2826: 2011; Aviation series. Combustion behavior of non-metallic materials under the influence of radiated heat and flames. Determination of gas components in smoke.
• EN 2828: 1993; Adhesion test for metallic coatings by polishing.
• EN 2829: 1995; Adhesion test for metallic coatings by ball forging.
• EN 2830: 1993; Adhesion test for metallic coatings with shear action.
• EN 2831: 1993; Hydrogen embrittlement of steels. Test by bending slowly.
• EN 2832: 1993; Hydrogen embrittlement of steels. Notched specimen test.
• EN 2833-005: 2013; Aviation series. Glass fiber thermoset pre-impregnation. Technical specification. Glass fabric/phenolic resin pre-impregnation
• EN 2835: 2012; Aviation series. Chloroprene rubber (CR). Heat resistance. Hardness 40 IRHD.
• EN 2836: 2012; Aviation series. Chloroprene rubber (CR). Heat resistance. Hardness 50 IRHD.
• EN 2837: 2012; Aviation series. Chloroprene rubber (CR). Heat resistance. Hardness 60 IRHD .
• EN 2838: 2013; Aviation series. Chloroprene rubber (CR). Heat resistance. Hardness 70 IRHD.
• EN 2839: 2013; Aviation series. Chloroprene rubber (CR). Heat resistance. Hardness 80 IRHD.
• EN 2840: 2013; Aviation series. Acrylonitrile-butadiene rubber (NBR). Mineral oil resistant. Hardness 50 IRHD.
• EN 2841: 2013; Aviation series. Acrylonitrile-butadiene rubber (NBR). Mineral oil resistant. Hardness 60 IRHD.
• EN 2842: 2013; Aviation series. Acrylonitrile-butadiene rubber (NBR). Mineral oil resistant. Hardness 70 IRHD.
• EN 2843: 2013; Aviation series. Acrylonitrile-butadiene rubber (NBR). Mineral oil resistant. Hardness 80 IRHD.
• EN 2844: 2013; Aviation series. Acrylonitrile-butadiene rubber (NBR). Mineral oil resistant. Hardness 90 IRHD.
• EN 2845: 2013; Aviation series. Acrylonitrile-butadiene rubber (NBR). It is resistant to fuel and synthetic oil. Hardness 50 IRHD.
• EN 2846: 2013; Aviation series. Acrylonitrile-butadiene rubber (NBR). It is resistant to fuel and synthetic oil. Hardness 60 IRHD.
• EN 2847: 2013; Aviation series. Acrylonitrile-butadiene rubber (NBR). It is resistant to fuel and synthetic oil. Hardness 70 IRHD.
• EN 2848: 2013; Aviation series. Acrylonitrile-butadiene rubber (NBR). It is resistant to fuel and synthetic oil. Hardness 80 IRHD.
• EN 2849: 2013; Aviation series. Acrylonitrile-butadiene rubber (NBR). It is resistant to fuel and synthetic oil. Hardness 90 IRHD.
• EN 2851 : 1992 ; Marking of parts and assemblies other than engines. Indicators in the drawings.
• EN 2852 : 2010 ; Aviation series. Nuts, hexagonal, flat, normal height, normal on flat surfaces, heat resistant steel passivated. Classification : 1100 MPa/650^DC.
• EN 2853 : 2005 ; Current values ​​for electrical cables with EN 2083 conductors;
• EN 2854-002 : 2009 ; Aviation series. Cables, general purpose electrical. cross sections greater than or equal to 9 mm2; Operating temperatures from -55^DC to 260^DC. general
• EN 2854-003: 2009; Aviation series. Cables, general purpose electrical. Sections greater than or equal to 9 mm$u2; Operating temperatures from -55 ^DC to 260 ^DC. product standard
• EN 2856 : 2006 ; Aviation series. Nut, anchor, self-locking, fixed, closed corner, reduced series, countersunk. Classification : 1100 MPa/235^DC.
• EN 2858-1 : 1994 ; Titanium and titanium alloys. Tattoo stock and forging. Technicial Specifications. General Requirements
• EN 2858-2 : 1994 ; Titanium and titanium alloys. Tattoo stock and forging. Technical specifications.. Forged stock
• EN 2858-3 : 1994 ; Titanium and titanium alloys. Tattoo stock and forging. Technicial Specifications. Pre-production and production forgings
• EN 2859: 1995; Bolts, normal hex head, close tolerance normal shank, short thread, alloy steel, cadmium plated. Classification : 1100 MPa (at ambient temperature)/235^DC.
• EN 2859 : 2006 ; Aviation series. Bolts, normal hex head, close tolerance normal shank, short thread, alloy steel, cadmium plated. Classification : 1100 MPa (at ambient temperature) / 235^DC.
• EN 2862: 2009; Aviation series. Nuts, anchor, self-locking, fixed, 90$0D corner, countersunk, alloy steel, cadmium plated, MoS2 lubricated. Classification : 1100 MPa (at ambient temperature)/235^DC.
• EN 2863: 2010; Aviation series. Nuts, anchor, self-locking, fixed, 90$0D corner, countersunk, of heat-resistant steel, MoS2 lubricated. Classification : 1100 MPa (at ambient temperature) / 315^DC.

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.