EN European Norm Tests Part 49

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 3946: 2001; Aviation series. Nickel-based alloy NI-B15701 (NiPd34Au30). Filler metal for soldering. Powder or paste.
• EN 3947: 1998; Nickel-based alloy NI-B15701 (NiPd34Au30). Filler metal for soldering. Rolled foil.
• EN 3948: 1998; Nickel-based alloy NI-B15701 (NiPd34Au30). Filler metal for soldering. Phone.
• EN 3969: 2006; Aviation series. Steel FE-PL1507 (40CrMoV12). The air has melted. annealed. Tattoo stock. a or D 3L 350 mm.
• EN 3971 : 2006 ; Aviation series. Steel FE-PL1507 (40CrMoV12). The consumable electrode was remelted. annealed. Tattoo stock. a or D 3L 350 mm.
• EN 3972: 2006; Aviation series. Steel FE-PL1507 (40CrMoV12). The consumable electrode was remelted. Hardened and tempered. Bar for processing. 3L 50mm. 1250 MPa 3L Rm 3L 1400 MPa.
• EN 3973: 2006; Aviation series. Steel FE-CM3801 (X5CrNiCuNb16-4). Homogenised, solution treated and precipitation hardened. Investment breakdowns. 3L 50mm. 3 million dollars 1030 MPa.
• EN 3976 : 2006 ; Aviation series. Titanium and titanium alloys. Test method. Chemical analysis for determination of hydrogen content.
• EN 3979 : 2005 ; Aviation series. Aluminum alloy AL-P8090-O2 ; Sheet for superplastic forming (SPF). 0,8mm 3L and 3L 6mm.
• EN 3982: 2015; Aviation series. Aluminum alloy AL-P7050 ; AlZn6CuMgZr. T7451 ; Plates. 6mm $0L and 3L 160mm.
• EN 3983: 2013; Aviation series. Aluminum alloy AL-P7050-. T7651; Plate. 6mm $0L and 3L 160mm.
• EN 3987: 2009; Aviation series. Test methods for metallic materials. Constant amplitude force controlled high speed fatigue test.
• EN 3997 : 2007 ; Aviation series. Aluminum alloy AL-P2024-T3 ; Sheet and strip 0,4 mm 3Q 3Q and 3Q 6 mm.
• EN 3997 : 2015 ; Aviation series. Aluminum alloy AL-P2024-Al Cu4Mg1-T3 ; Sheet and strip. 0,4mm 3L and 3L 6mm.
• EN 3998 : 2007 ; Aviation series. Aluminum alloy AL-P2024-T4 or T42 ; Sheet and strip. 0,3mm 3L and 3L 6mm.
• EN 3999 : 2007 ; Aviation series. Aluminum alloy AL-P2024-T351 ; Plate and strip with improved chemical milling capacity 1,6 mm 3L and 3L 6 mm.
• EN 4001 : 2007 ; Aviation series. Aluminum alloy AL-P2024-T351 ; Coated sheet and strip with improved chemical grinding capacity 1,6 mm 3L and 3L 6 mm.
• EN 4002: 2007; Aviation series. Aluminum alloy AL-P2219-T81 ; Sheet and strip 0,5 mm 3L and 3L 6 mm.
• EN 4003: 2006; Aviation series. Aluminum alloy AL-P2219-T87 ; Sheet and strip 0,5 mm 3L and 3L 6 mm.
• EN 4004: 2007; Aviation series. Aluminum alloy AL-P3103-H16 ; Sheet and strip. 0,4mm 3L and 3L 6mm.
• EN 4005: 2007; Aviation series. Aluminum alloy AL-P5052-O. Sheet and strip 0,3mm 3L and 3L 6mm.
• EN 4006: 2007; Aviation series. Aluminum alloy AL-P6082-T4 or T42 ; Sheet and strip 0,4 mm 3L and 3L 6 mm.
• EN 4007 : 2005 ; Aviation series. Aluminum alloy AL-P6082-T6 or T62 ; Sheet and strip. 0,4mm 3L and 3L 6mm.
• EN 4008-001: 2006; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Technical specification
• EN 4008-002: 2006; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. List of product standards
• EN 4008-005: 2006; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Positioner M22520/2-01 for crimping tool ; product standard
• EN 4008-006: 2006; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Positioner M22520/7 for crimping tool ; product standard
• EN 4008-007: 2006; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Positioner M22520/2-01 for crimping tool ; product standard
• EN 4008-007: 2011; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Positioner M22520/2-01 for crimping tool ; product standard
• EN 4008-008: 2006; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Positioner M22520/7-01 for crimping tool ; product standard
• EN 4008-008: 2011; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Positioner M22520/7-01 for crimping tool ; product standard
• EN 4008-011: 2006; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Positioner M22520/2-01 for crimping tool ; product standard
• EN 4008-012: 2006; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Positioner M22520/2-01 for crimping tool ; product standard
• EN 4008-013: 2006; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Positioner M22520/2-01 for crimping tool ; product standard
• EN 4008-014: 2006; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Turret for crimping tool M22520/31-01 ; product standard
• EN 4008-015: 2007; Aviation series. Electrical and optical connection elements. Crimping tool and related accessories. Positioner M22520/2-01 for crimping tool ; product standard
• EN 4008-017: 2006; Aviation series. Electrical and optical connection elements. Crimping tools and related accessories. Head for crimping tool M22520/4-01 ; product standard
• EN 4008-018: 2014; Aviation series. Electrical and optical connection elements. Crimping tool and related accessories. Positioner M22520/2-01 for crimping tool ; product standard
• EN 4009: 2004; Aviation series. Bolts, double hex head, close tolerance shank, medium length thread, of heat resistant nickel base alloy NI-PH2601 (Inconel 718). Classification : 1550 MPa (at ambient temperature).
• EN 4011: 2004; Aviation series. Nuts, two hexagons, self-locking, heat resistant nickel-based alloy NI-PH2601 (Inconel 718), silver plated. Classification : 1550 MPa (at ambient temperature)/600^DC.
• EN 4013: 2004; Aviation series. Shaft nuts, self-locking, of heat-resistant nickel-based alloy NI-PH2601 (Inconel 718), silver-plated. Classification : 1550 MPa (at ambient temperature) / 600^DC.
• EN 4014: 2004; Aviation series. Inserts, thick wall, self-locking. Design standard.
• EN 4018: 2009; Aviation series. Titanium alloy pipe coupling 8$0D30′. Elbows 90$0D with compression wire nut.
• EN 4020: 2009; Aviation series. Titanium alloy pipe coupling 8$0D30′. Elbows 90$0D, welded end with thrust wire nut.
• EN 4023: 2010; Aviation series. Titanium alloy pipe coupling 8$0D30′. Elbows $45D.
• EN 4024: 2009; Aviation series. Titanium alloy pipe coupling 8$0D30′. Elbows, 45$0D welded end with thrust wire nut.
• EN 4025: 2010; Aviation series. Titanium alloy pipe coupling 8$0D30′. Elbows $45D, partition wall.
• EN 4033: 2007; Aviation series. Bearings, body rolling. Rigid single row ball bearings in corrosion resistant steel. Diameter series 8 and 9, reduced internal radial clearance. Dimensions and loads.
• EN 4034: 2007; Aviation series. Bearings, body rolling. Double row self-aligning ball bearings with flanged outer ring made of corrosion resistant steel, reduced internal radial clearance. Dimensions and loads.
• EN 4035: 2006; Aviation series. Rod ends are adjustable with a corrosion resistant steel self-aligning double row ball bearing, reduced internal radial clearance and a titanium alloy threaded shaft. Dimensions and loads.
• EN 4036: 2006; Aviation series. Adjustable rod ends with self-aligning double row ball bearing and threaded shaft in corrosion resistant steel, reduced internal radial clearance. Dimensions and loads.
• EN 4040: 2006; Aviation series. Bearings, spherical plain of corrosion-resistant steel with large inner ring, self-lubricating lining. High loads at ambient temperature. Dimensions and loads.
• EN 4041: 2006; Aviation series. Bearings, body rolling. Rigid single-row ball bearings in corrosion-resistant steel with enlarged inner ring and flanged alignment bushes. Dimensions and loads.
• EN 4047: 2004; Aviation series. Nuts, self-locking, MJ threads, of heat-resistant nickel-based alloy NI-PH2601 (Inconel 718), silver-plated. Classification : 1550MPa (at ambient temperature)/600^DC. Technical specification.
• EN 4048: 2004; Aviation series. Nuts, self-locking, MJ threads in heat resistant nickel base alloy NI-PH2601 (Inconel 718), MoS$d2 coated. classification 1 550 MPa (at ambient temperature) / 425^DC. Technical specification.
• EN 4049-001: 2006; Aviation series. Thermocouple extension cable. Operating temperatures from -65^DC to 260^DC. Technical specification
• EN 4049-002 : 2005 ; Aviation series. Thermocouple extension cable. Operating temperatures from -65^DC to 260^DC. general
• EN 4049-003: 2006; Aviation series. Thermocouple extension cable. Operating temperatures from -65^DC to 260^DC. Single core nickel chrome/nickel aluminum. product standard
• EN 4049-004 : 2006 ; Aviation series. Thermocouple extension cable. Operating temperatures from -650DC to 260^DC. Double core nickel chrome/nickel aluminum shielded and sheathed. product standard
• EN 4050-1: 2012; Aviation series. Test method for metallic materials. Ultrasonic inspection of bars, plates, forging stock and forgings. General Requirements
• EN 4050-2: 2012; Aviation series. Test method for metallic materials. Ultrasonic inspection of bars, plates, forging stock and forgings. Performance of the test
• EN 4050-3: 2012; Aviation series. Test method for metallic materials. Ultrasonic inspection of bars, plates, forging stock and forgings. reference blocks
• EN 4050-4: 2012; Aviation series. Test method for metallic materials. Ultrasonic inspection of bars, plates, forging stock and forgings. Accept conditions
• EN 4056-001: 2006; Aviation series. Cable ties for cable bundles. Technical specification
• EN 4056-001: 2015; Aviation series. Cable ties for cable bundles. Technical specification
• EN 4056-002: 2014; Aviation series. Cable ties for cable bundles. Product standards directory
• EN 4056-003: 2016; Aviation series. Cable ties for cable bundles. Plastic cable ties. Operating temperatures -65 ^DC to 105 ^DC and -65 ^DC to 150 ^DC. product standard
• EN 4056-004: 2014; Aviation series. Cable ties for cable bundles. Plastic cable ties. For operating temperatures – 55^DC to 105^DC and – 55^DC to 150^DC. product standard
• EN 4056-006: 2014; Aviation series. Cable ties for cable bundles. Peek cable ties. For operating temperatures. -55 ^DC to 240 ^DC. product standard
• EN 4057-100 : 2006 ; Aviation series. Cable ties for cable bundles. Test methods. general
• EN 4057-201 : 2005 ; Aviation series. Cable ties for cable bundles. Test methods. visual exam
• EN 4057-202: 2005; Aviation series. Cable ties for cable bundles. Test methods. Examination of mass and dimensions
• EN 4057-301 : 2005 ; Aviation series. Cable ties for cable bundles. Test methods. salt fog test
• EN 4057-302: 2006; Aviation series. Cable ties for cable bundles. Test methods. flammability
• EN 4057-303: 2005; Aviation series. Cable ties for cable bundles. Test methods. Resistance to liquids
• EN 4057-304: 2006; Aviation series. Cable ties for cable bundles. Test methods. Loop tensile strength at maximum operating temperature
• EN 4057-305: 2005; Aviation series. Cable ties for cable bundles. Test methods. color fastness
• EN 4057-306: 2006; Aviation series. Cable ties for cable bundles. Test methods. heat aging test
• EN 4057-307 : 2006 ; Cable ties for cable bundles. Test methods. Resistance to ultraviolet radiation
• EN 4057-401 : 2006 ; Aviation series. Cable ties for cable bundles. Test methods. Loop tensile strength
• EN 4057-402: 2006; Aviation series. Cable ties for cable bundles. Test methods. Lifecycle
• EN 4057-402: 2014; Aviation series. Cable ties for cable bundles. Test methods. Lifecycle
• EN 4057-404: 2006; Aviation series. Cable ties for cable bundles. Test methods. Low temperature setup
• EN 4057-405 : 2005 ; Aviation series. Cable ties for cable bundles. Test methods. Compass safe distance
• EN 4057-406 : 2006 ; Aviation series. Cable ties for cable bundles. Test methods. Locking device hold
• EN 4057-407 : 2005 ; Aviation series. Cable ties for cable bundles. Test methods. Verifying application agent settings
• EN 4069: 1996; Nuts, hexagonal, flat, reduced in height, reduced on flat surfaces, of heat-resistant steel, passivated. Classification : 600MPa (at ambient temperature)/650^DC.
• EN 4071: 2009; Aviation series. Bolts, normal hex head, close tolerance normal shank, short thread, titanium alloy, aluminum IVD coated. Classification : 1100 MPa (at ambient temperature) / 425 ^DC.
• EN 4072: 2009; Aviation series. Screws, 100$0D countersunk normal head, offset cruciform recess, close tolerance regular shank, short thread, in titanium alloy, aluminum IVD coated. Classification : 1100 MPa (at ambient temperature) / 425 °C.
• EN 4072: 2016; Aviation series. Screws, 100$0D countersunk normal head, offset cruciform recess, narrow tolerance shank, short thread in titanium alloy, aluminum IVD coated. Classification : 1 100 MPa (at ambient temperature) / 425 ^DC.
• EN 4073: 2009; Aviation series. Screws, round head, six-lobe socket, coarse tolerance normal shank, medium-length thread, alloy steel, cadmium plated. Classification 1100 MPa (at ambient temperature) / 235^DC.
• EN 4073: 2016; Aviation series. Screws, round head, hexagonal recess, coarse tolerance shank, medium thread, alloy steel, cadmium plated. Classification : 1 100 MPa (at ambient temperature) / 235 ^DC.
• EN 4074: 2009; Aviation series. Screws, round head, six-lobed recess, rough tolerance normal shank, medium-length thread, titanium alloy, aluminum IVD coated. Classification : 1100 MPa (at ambient temperature)/425^DC.
• EN 4075 : 2008 ; Aviation series. Screws, round head, cross-shaped protruding recess, threaded, corrosion-resistant steel, passivated. Classification : 490 MPa (at ambient temperature) / 425 ^DC.
• EN 4078: 2009; Aviation series. Tips, threaded, thin-walled, interlocking and self-locking, of heat-resistant steel, MoS2 lubricated. Classification : 1100 MPa (at ambient temperature) / 315^DC.
• EN 4084: 2009; Aviation series. Nuts, anchor, self-locking, fixed, two-lug, countersunk, alloy steel, cadmium-plated, MoS2 lubricated. Classification : 1100 MPa (at ambient temperature) / 235^DC.
• EN 4085: 2001; Aviation series. Nickel-based alloy NI-B40002 (NiSi4B2). Filler metal for soldering. Amorphous foil.
• EN 4098: 2007; Aviation series. Steel FE-PL1507 (40CrMoV12). Remelted, hardened and tempered, forgings De 3L 50 mm, 1250 MPa 3L Rm 3L 1400 MPa.
• EN 4099 : 2005 ; Aviation series. Aluminum alloy AL-P2219-T6 or T62 ; Coated sheet and strip. 0,5mm 3L and 3L 6mm.
• EN 4100 : 2005 ; Aviation series. Aluminum alloy AL-P2219-T6 or T62 ; Sheet and strip. 0,5mm 3L and 3L 6mm.

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.