EN European Norm Tests Part 50

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 4101: 2005; Aviation series. Aluminum alloy AL-P2024-T4 ; Sheet and strip with enhanced stretch forming. 0,4mm 3L and 3L 6mm.
• EN 4102: 2005; Aviation series. Aluminum alloy AL-P2219-T81 ; Coated sheet and strip. 0,5mm 3La 3L6mm.
• EN 4105: 1998; Nickel-based alloy NI-B40002 (NiSi4B2). Filler metal for soldering. Tape.
• EN 4106: 2013; Aviation series. non-metallic materials. Structural adhesive systems. Paste glue. Technical specification.
• EN 4108 : 2006 ; Aviation series. Keys, crow's feet, coupling socket, socket driver.
• EN 4111 : 2006 ; Aviation series. Wrenches, threaded, sockets for pipe fittings. Technical specification.
• EN 4113 : 2009 ; Aviation series. Clamps, ring (“P” type) of corrosion resistant steel, passivated, rubber cushioned. Dimensions, masses.
• EN 4114: 2009; Aviation series. Clamps, ring ("P" type) aluminum alloy with rubber cushioning. Dimensions, masses.
• EN 4115 : 2010 ; Aviation series. Cushion, rubber for clamps. Dimensions, masses.
• EN 4118: 2004; Aviation series. Nuts, two hexagonal, self-locking, of heat-resistant steel FE-PA2601 (A286), silver-plated on thread. Classification : 1100 MPa (at ambient temperature) / 650^DC.
• EN 4119: 2004; Aviation series. Nuts, two hexagonal, self-locking, countersunk, heat resistant steel FE-PA2601 (A286), silver plated on thread. Classification : 1100 MPa (at ambient temperature) / 650^DC.
• EN 4120 : 2004 ; Nuts, two hexagonal, self-locking, heat-resistant nickel-based alloy NI-PH1302 (Waspaloy), silver-plated on thread. Classification : 1210 MPa (at ambient temperature) / 730^DC.
• EN 4124 : 2004 ; Aviation series. Shank nuts, self-locking, heat resistant nickel base alloy NI-PH1302 (Waspaloy), silver plated on thread, for 60$0D forging. classification 1 210 MPa (at ambient temperature) / 730^DC.
• EN 4127 : 2009 ; Aviation series. Bolts, normal hex head, rough tolerance normal shank, short thread, titanium alloy, aluminum IVD coated. Classification : 1100 MPa (at ambient temperature) / 425 ^DC.
• EN 4128: 2009; Aviation series. Bolts, normal hex head, rough tolerance normal shank, short thread, heat resistant nickel base alloy, aluminum IVD coated. Classification : 1250 MPa (at ambient temperature) / 425 ^DC.
• EN 4128: 2016; Aviation series. Bolts, normal hex head, rough tolerance shank, short thread, heat resistant nickel base alloy, aluminum IVD plated. Classification : 1 250 MPa (at ambient temperature) / 425 ^DC.
• EN 4129: 2009; Aviation series. Bolts, normal hex head, rough tolerance normal shank, medium thread, alloy steel, cadmium plated. Classification : 1100 MPa (at ambient temperature) / 235^DC.
• EN 4130: 2009; Aviation series. Bolts, normal hex head, rough tolerance normal shank, medium thread, titanium alloy, aluminum IVD coated. Classification : 1100 MPa (at ambient temperature) / 425 ^DC.
• EN 4131: 2009; Aviation series. Bolts, normal hex head, rough tolerance normal shank, medium length thread, heat resistant nickel base alloy, aluminum IVD coated. Classification : 1250 MPa (at ambient temperature) / 425 ^DC.
• EN 4132 : 2009 ; Aviation series. Bolts, normal hex head, rough tolerance normal shank, long thread, alloy steel, cadmium plated. Classification : 1100 MPa (at ambient temperature)/235^DC.
• EN 4133: 2009; Aviation series. Bolts, normal hex head, rough tolerance normal shank, long thread, titanium alloy, aluminum IVD coated. Classification : 1100 MPa (at ambient temperature) / 425 ^DC.
• EN 4134 : 2009 ; Aviation series. Bolts, normal hex head, rough tolerance normal shank, long thread, heat resistant nickel base alloy, aluminum IVD coated. Classification : 1250 MPa (at ambient temperature)/425^DC.
• EN 4135: 2009; Aviation series. Bolts, normal double hex head, rough tolerance normal shank, medium length thread, titanium alloy, anodized, MoS2 lubricated. Classification : 1100 MPa (at ambient temperature)/315^DC.
• EN 4136 : 2009 ; Aviation series. Bolts, normal double hex head, rough tolerance normal shank, long thread, alloy steel, cadmium plated. Classification : 1100 MPa)/235^DC at ambient temperature.
• EN 4137: 2009; Aviation series. Bolts, normal double hex head, stepped shank, long thread, titanium alloy, anodized, MoS2 lubricated. Classification : 1100 MPa (at ambient temperature)/315^DC.
• EN 4138: 2009; Aviation series. Screws, round head, cross-shaped recess, rough tolerance normal shank, medium-length thread, alloy steel, cadmium plated. Classification : 1100 MPa (at ambient temperature) / 235^DC.
• EN 4138: 2016; Aviation series. Screws, round head, cross-shaped recess, rough tolerance normal shank, medium-length thread, alloy steel, cadmium plated. Classification : 1 100 MPa (at ambient temperature) / 235 ^DC.
• EN 4156 : 2013 ; Aviation series. Rod ends with self-aligning double row ball bearings and threaded shaft made of steel. Inner ring and balls in corrosion resistant steel. Dimensions and loads. inch series.
• EN 4158 : 2006 ; Aviation series. Paints and varnishes. Test method for measuring the electrical surface resistance of conductive layers.
• EN 4159 : 2011 ; Aviation series. Paints and Varnishes. Determination of resistance to microbial growth.
• EN 4160: 2011; Aviation series. Paints and varnishes. Determination of the effect of thermal exposure.
• EN 4161: 2009; Aviation series. Screws, round head, cross-shaped recess, rough tolerance normal shank, long thread, alloy steel, cadmium plated. Classification : 1100 MPa (at ambient temperature) / 235 ^DC.
• EN 4162: 2009; Aviation series. Screws 100$0D countersunk normal head, offset cruciform recess, coarse tolerance normal shank, medium length thread, alloy steel, cadmium plated. 1100 MPa (at ambient temperature) / 235^DC.
• EN 4162: 2016; Aviation series. Screws 100$0D countersunk normal head, offset cruciform recess, coarse tolerance normal shank, medium length thread, alloy steel, cadmium plated. Classification : 1 100 MPa (at ambient temperature) / 235 ^DC.
• EN 4163: 2009; Aviation series. Screws 100$0D countersunk normal head, offset cruciform recess, rough tolerance normal shank, long thread, alloy steel, cadmium plated. 1100 MPa (at ambient temperature) / 235^DC.
• EN 4163: 2016; Aviation series. Screws 100$0D countersunk normal head, offset cruciform recess, rough tolerance normal shank, long thread, alloy steel, cadmium plated. Classification : 1 100 MPa (at ambient temperature) / 235 ^DC.
• EN 4165-001: 2007; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Technical specification
• EN 4165-001: 2015; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175 ^DC continuous. Technical specification
• EN 4165-002 : 2007 ; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Features of performance and communication arrangements
• EN 4165-002 : 2015 ; Connectors, electrical, rectangular, modular. Operating temperature 175 ^DC continuous. Features of performance and communication arrangements
• EN 4165-003: 2008; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Modules series 2 and series 3 ; product standard
• EN 4165-003: 2016; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175 ^DC continuous. Modules series 2 and series 3 ; product standard
• EN 4165-004 : 2007 ; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Stackable mounting slots 2 and 4 modules, series 2 ; product standard
• EN 4165-005 : 2007 ; Aviation series. Connectors, electrical, rectangular, Modular. Operating temperatures 175 ^DC continuous. Stackable slots 2 and 4 modules, series 3 ; product standard
• EN 4165-006: 2007; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Plug for 2 and 4 modules, series 2 ; product standard
• EN 4165-007: 2007; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Plug for 2 and 4 modules, series 3 ; product standard
• EN 4165-008: 2007; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Rack and panel plug for 2 and 4 modules, series 2 ; product standard
• EN 4165-009: 2007; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Rack and panel plug for 2 and 4 modules, series 3 ; product standard
• EN 4165-010: 2007; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Rack and panel rear mount plug for 2 and 4 modules, series 2 ; product standard
• EN 4165-011: 2007; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Flange mounting slot 2 and 4 modules, series 2 ; product standard
• EN 4165-012: 2005; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175 ^DC continuous. Flange mounting slot 2 or 4 modules, series 3 ; product standard
• EN 4165-013: 2005; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Cable clamp for connectors modules 2 and 4, series 2 and series 3 ; product standard
• EN 4165-013: 2016; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175 ^DC continuous. Cable clamp for connectors modules 2 and 4, series 2 and series 3 ; product standard
• EN 4165-014: 2005; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175 ^DC continuous. Shielded accessory body, 2 and 4 modules for connectors, series 2 and series 3 ; product standard
• EN 4165-015 : 2005 ; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175 ^DC continuous. Round flue for accessory (1 per module cavity). product standard
• EN 4165-015 : 2015 ; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Round flue for accessory (1 per module cavity), 2 and 4 modules. product standard
• EN 4165-016: 2005; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Double oval chimney for accessory (2 in 1 modules). product standard
• EN 4165-017: 2005; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Empty flue for accessory (1 per module cavity). product standard
• EN 4165-018 : 2007 ; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Protective cover for slot 2 or 4 modules, series 2 and series 3 ; product standard
• EN 4165-018 : 2015 ; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175 ^DC continuous. Protective cover for all sockets series 2 ; product standard
• EN 4165-020: 2007; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Coupling system keyway for socket. product standard
• EN 4165-021: 2007; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Coupling system keyway for plug. product standard
• EN 4165-022: 2005; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Insertion/removal tool for removing modules. product standard
• EN 4165-023: 2007; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Kits for the mounting slot coding component. product standard
• EN 4165-024: 2011; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175 ^DC continuous. Single module plug. product standard
• EN 4165-025: 2011; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Module slot. Product Standard
• EN 4165-026: 2011; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175 ^DC continuous. Accessories for single modules. product standard
• EN 4165-026: 2015; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175 ^DC continuous. Accessories for single module connector. product standard
• EN 4165-027: 2015; Aviation series. Connectors, electrical, rectangular, modular. Operating temperature 175^DC continuous. Rack and panel rear mount plug for 2 and 4 modules, series 3 ; product standard
• EN 4166: 2004; Aviation series. Clips, spring tension, three parts. PTFE bushings.
• EN 4167: 2004; Aviation series. Clips, spring tension, three parts. Internal clips made of heat-resistant steel FE-PA2601 (A286).
• EN 4168: 2004; Aviation series. Clips, spring tension, three parts. FE-PA2601 (A286) outer clips in heat resistant steel.
• EN 4170 : 2007 ; Aviation series. Paints and varnishes. Test method for measurement of resistance to cold crack temperature cycling.
• EN 4171 : 2011 ; Aviation series. Paints and varnishes. Test method for determining the phosphoric acid index.
• EN 4172 : 2006 ; Aviation series. Lock bolts, salient head, shear type, close tolerance, titanium alloy TI-P64001, anodized, metric series. Classification : 1 100 MPa (at ambient temperature) / 315^DC.
• EN 4173: 2006; Aviation series. Lock bolts, 100 countersunk normal head, shear type, close tolerance, titanium alloy TI-P64001, anodized, metric series. Classification : 1100 MPa (at ambient temperature) / 315^DC.
• EN 4174 : 2006 ; Aviation series. Collars, press-lock, scissor type, aluminum alloy 2024, anodized or chromated, metric series.
• EN 4175 : 2005 ; Aviation series. Collars, flanged thrust lock, scissor type, titanium TI-P99002, metric series.
• EN 4176: 2005; Aviation series. Lock bolts, 100$0D countersunk head normal head or protruding head, tension-/shear type, close tolerance, titanium alloy TI-P64001, anodized or aluminum pigment coated. Catches made of titanium TI-P99002 or 2024 aluminum alloy; Metric series. Technical specification.
• EN 4178: 2009; Aviation series. Screws, round head, six lobed recess, rough tolerance normal body, medium length thread, titanium alloy, anodized, MoS2 lubricated. 1100 MPa (at ambient temperature) / 315 ^DC.
• EN 4179 : 2000 ; Qualification and approval of personnel for non-destructive testing.
• EN 4179 : 2005 ; Aviation series. Qualification and approval of personnel for non-destructive testing.
• EN 4179 : 2009 ; Aviation series. Qualification and approval of personnel for non-destructive testing.
• EN 4195 : 2011 ; Aviation series. Paints and varnishes. Test method for determination of chromate leak.
• EN 4198 : 2006 ; Aviation series. Rod ends, self-lubricating lined adjustable spherical plain bearing and threaded shaft made of corrosion-resistant steel. Dimensions and loads.
• EN 4199-001 : 2006 ; Aviation series. Lashing straps for airplanes. Technical specification
• EN 4199-001 : 2013 ; Aviation series. Lashing straps for airplanes. Technical specification
• EN 4199-002 : 2006 ; Aviation series. Lashing straps for airplanes. Product standard index
• EN 4199-003: 2009; Aviation series. Lashing straps for airplanes. Plain stranded conductor copper, tin plated -65^DC to 150^DC and copper, nickel plated -65^DC to 260^DC lashing strap assemblies. product standard
• EN 4199-003: 2014; Aviation series. Lashing straps for airplanes. Plain stranded conductor copper, tin plated – 65^DC to 150^DC and copper, nickel plated – 65^DC to 260^DC lashing strap assemblies. product standard
• EN 4199-004 : 2009 ; Aviation series. Lashing straps for airplanes. Round lashing straps, copper, tin plated -65 ^DC to 150 ^DC and nickel plated -65 ^DC to 260 ^DC. product standard
• EN 4199-004: 2014; Aviation series. Lashing straps for airplanes. Round lashing straps, copper, -150^DC tin plated up to 65^DC and -260^DC nickel plated up to 65^DC. Product Standard
• EN 4199-005 : 2009 ; Aviation series. Lashing straps for airplanes. Flat stranded conductors copper, tin plated -65^DC to 150^DC and copper, nickel-plated, -65^DC to 260^DC. product standard
• EN 4199-006 : 2006 ; Aviation series. Lashing straps for airplanes. Round braided copper conductors for connecting tapes, tin plated up to 150^DC or nickel plated up to 260^DC. product standard
• EN 4202: 2005; Aviation series. Aluminum alloy AL-P6082-T651 ; Plate. 6mm $0L and 3L 25mm.
• EN 4203: 2005; Aviation series. Aluminum alloy AL-P8090-T89 ; Sheet. 0,6mm 3L and 3L 6mm.
• EN 4204: 2005; Aviation series. Aluminum alloy AL-P8090 ; T841 ; Sheet. 0,6mm 3L and 3L 6mm.
• EN 4209 : 2005 ; Aviation series. Aluminum alloy AL-P2219-T851 ; Plate. 6mm $0La 3L50mm.
• EN 4211: 2005; Aviation series. Aluminum alloy AL-P2024-T42 ; Cover plate. 6mm $0L and 3L 25mm.
• EN 4212 : 2005 ; Aviation series. Aluminum alloy AL-P5086-H111 ; Plate. 6mm $0L and 3L8 0mm.

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.