EN European Norm Tests Part 53

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 4612-013: 2011; Aviation series. For cables, electrical, general purpose, single and multi-core assembly. XLETFE Family. Jacketed or screened and jacketed. SX, TC and UC. Nickel plated copper. Operating temperatures from -65^DC to 150^DC. Single extruded wall for equipment only with jacket and screen (spiral). UV laser printable. product standard
• EN 4613 : 2009 ; Aviation series. Self-lubricating lined spherical plain bearings in corrosion-resistant steel, narrow series. Dimensions and loads. inch series.
• EN 4614 : 2009 ; Aviation series. Large range of spherical plain bearings in corrosion-resistant steel with self-lubricating linings. Dimensions and loads. inch series.
• EN 4615 : 2005 ; Aviation series. Magnesium alloy MG-C18002 ; T4 ; Sand casting.
• EN 4616 : 2005 ; Aviation series. Magnesium alloy MG-C18002 ; T4 ; Cold casting.
• EN 4617 : 2006 ; Aviation series. Recommended practices to standardize company standards.
• EN 4618 : 2009 ; Aviation series. Aircraft indoor air quality standards, criteria and determination methods.
• EN 4619 : 2010 ; Aviation series. Bits, MJ threads, self-locking, with self-opening keys. Installation and uninstallation procedure.
• EN 4620: 2010; Aviation series. Bits, MJ threads, self-locking, with self-opening keys. Design standard.
• EN 4621 : 2010 ; Aviation series. Bits, MJ threads, self-locking, self-release keys. Technical specification.
• EN 4622: 2010; Aviation series. Bits, MJ threads, self-locking, with self-broaching keys, heat-resistant steel FE-PA2601 (A286), MoS2 coated.
• EN 4623: 2010; Aviation series. Bits, MJ threads, self-locking, with self-broaching keys, heat resistant nickel base alloy NI-PH2601 (Inconel 718), silver plated.
• EN 4624 : 2010 ; Aviation series. Bits, MJ threads, self-locking, with self-broaching keys, heat resistant nickel base alloy NI-PH1302 (Waspaloy), silver plate.
• EN 4626-001: 2008; Aviation series. Connectors, optical, rectangular, multi-contact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule. Operating temperatures -65 ^DC to 125 ^DC (cable dependent). Wash the contacts. Technical specification
• EN 4626-002 : 2008 ; Aviation series. Connectors, optical, rectangular, multi-contact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule. Operating temperatures -65^DC to 125^DC (cable dependent). Wash the contacts. Features of performance and communication arrangements
• EN 4626-003: 2008; Aviation series. Connectors, optical, rectangular, multi-contact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule. Operating temperatures -65^DC to 125^DC (cable dependent). Wash the contacts. plug adapter
• EN 4626-004 : 2008 ; Aviation series. Connectors, optical, rectangular, multi-contact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule. Operating temperatures -65^DC to 125^DC (cable dependent). Wash the contacts. Adapter for socket
• EN 4626-101: 2008; Aviation series. Connectors, optical, rectangular, multi-contact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule. Operating temperatures -65^DC to 125^DC (cable dependent). Wash the contacts. Optical contact for plug (sub-mount). product standard
• EN 4626-201 : 2009 ; Aviation series. Connectors, optical, rectangular, multi-contact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule. Operating temperatures -65 ^DC to 125 ^DC (cable dependent). Wash the contacts. Optical contact for socket (sub-mount). product standard
• EN 4626-202: 2009; Aviation series. Connectors, optical, rectangular, multi-contact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule. Operating temperatures -65^DC to 125^DC (cable dependent). Wash the contacts. Optical contact assembly for 900 $Gmm buffered fiber socket. product standard
• EN 4627 : 2007 ; Aviation series. Steel FE-PM 3504 (X4CrNiMo16-5-1). The air has melted. Hardened and tempered. Tattoos. 3L 150mm. 1100 MPa 3L Rm 3L 1300 MPa.
• EN 4627: 2014; Aviation series. Steel X4CrNiMo16-5-1 (1;4418). The air has melted. Hardened and tempered. Tattoos. 3L 200mm. 1 150 MPa 3L Rm 3L 1 300 MPa.
• EN 4628 : 2007 ; Aviation series. Steel FE-PM 3504 (X4CrNiMo16-5-1). The air has melted. Hardened and tempered. Rod. 3L 150mm. 1100 MPa 3L Rm 3L 1300 MPa.
• EN 4628 : 2013 ; Aviation series. Steel X4CrNiMo16-5-1 (1;4418). The air has melted. Hardened and tempered. Rod. 3L 200mm. 1 150 MPa 3L Rm 3L 1 300 MPa.
• EN 4629 : 2007 ; Aviation series. Steel FE-PM 3504 (X4CrNiMo16-5-1). The air has melted. Hardened and tempered. Tattoo stock. 3L 300mm.
• EN 4629 : 2013 ; Aviation series. Steel X4CrNiMo16-5-1 (1;4418). The air has melted. Softened. Tattoo stock. 3L 300mm.
• EN 4630 : 2007 ; Aviation series. Steel FE-PM 3504 (X4CrNiMo16-5-1). The air has melted. Hardened and tempered. Tattoos. 3L 200mm. 900 MPa 3L Rm 3L 1050 MPa.
• EN 4630: 2014; Aviation series. Steel X4CrNiMo16-5-1 (1;4418). The air has melted. Hardened and tempered. Tattoos. 3L 200mm. 900 MPa $3L Rm $3L 1 050 MPa.
• EN 4631 : 2007 ; Aviation series. Steel FE-PM 3504 (X4CrNiMo16-5-1). The air has melted. Hardened and tempered. Rod. 3L 200mm. 900 MPa 3L Rm 3L 1050 MPa.
• EN 4631 : 2013 ; Aviation series. Steel X4CrNiMo16-5-1 (1;4418). The air has melted. Hardened and tempered. Rod. 3L 200mm. 900 MPa $3L Rm $3L 1 050 MPa.
• EN 4632-001: 2008; Aviation series. Welded and brazed assemblies for aerospace structures. Weldability and brazeability of materials. General Requirements
• EN 4632-002 : 2008 ; Aviation series. Welded and brazed assemblies for aerospace structures. Weldability and brazeability of materials. Homogeneous assemblies aluminum and aluminum alloys
• EN 4632-003: 2010; Aviation series. Weldability and brazeability of materials in aerospace construction. Welding and brazing of homogeneous structures of unalloyed and low alloyed steels
• EN 4632-004: 2012; Aviation series. Weldability and brazeability of materials in aerospace construction. Welding and brazing of homogeneous structures of high alloy steels
• EN 4632-005 : 2009 ; Aviation series. Weldability and brazeability of materials in aerospace construction. Homogeneous groups of heat-resistant Ni or Co-based alloys
• EN 4632-006: 2013; Aviation series. Weldability and brazeability of materials in aerospace construction. Homogeneous groups of titanium alloys
• EN 4635: 2009; Aviation series. Screws, 100$0D countersunk, six lobed recess, short thread, of heat resistant nickel base alloy NI-PH2601 (Inconel 718). Classification : 1270 MPa (at ambient temperature) / 650 ^DC.
• EN 4636: 2009; Aviation series. Screws, 100$0D countersunk, six lobed recess, short thread, titanium alloy TI-P64001, aluminum pigment coated. Classification : 1100 MPa (at ambient temperature) / 315^DC.
• EN 4637 : 2010 ; Aviation series. Blast media. White corundum.
• EN 4638: 2010; Aviation series. Blast media. Brown corundum, non-ferrous.
• EN 4639-001: 2007; Aviation series. Connectors, optical, rectangular, modular, multi-contact, 1,25 diameter ferrule, with removable alignment sleeve holder. Technical specification
• EN 4639-002 : 2007 ; Aviation series. Connectors, optical, rectangular, modular, multi-contact, 1,25 diameter ferrule, with removable alignment sleeve holder. List of product standards
• EN 4639-003: 2007; Aviation series. Connectors, optical, rectangular, modular, multi-contact, 1,25 diameter ferrule, with removable alignment sleeve holder. Male optical module. product standard
• EN 4639-004 : 2007 ; Aviation series. Connectors, optical, rectangular, modular, multi-contact, 1,25 diameter ferrule, with removable alignment sleeve holder. Female optical module. product standard
• EN 4639-005 : 2007 ; Aviation series. Connectors, optical, rectangular, modular, multi-contact, 1,25 diameter ferrule, with removable alignment sleeve holder. Removable alignment arm holder. product standard
• EN 4639-101: 2007; Aviation series. Connectors, optical, rectangular, modular, multi-contact, 1,25 diameter ferrule, with removable alignment sleeve holder. Optical contact for EN 4641-100 cable ; Operating temperatures from -65^DC to 125^DC. product standard
• EN 4639-102: 2007; Aviation series. Connectors, optical, rectangular, modular, multi-contact, 1,25 diameter ferrule, with removable alignment sleeve holder. Optical contact for EN 4641-102 cable ; Operating temperatures from -55^DC to 100^DC. product standard
• EN 4640-001: 2009; Aviation series. Connectors, optic, rectangular, rack and panel, multiple contacts, 1,25 diameter ferrule, with removable alignment sleeve holder. Technical specification
• EN 4640-002: 2009; Aviation series. Connectors, optic, rectangular, rack and panel, multiple contacts, 1,25 diameter ferrule, with removable alignment sleeve holder. List of product standards
• EN 4640-003: 2008; Aviation series. Connectors, optic, rectangular, rack and panel, multiple contacts, 1,25 diameter ferrule, with removable alignment sleeve holder. Plug in the optical connector. product standard
• EN 4640-004: 2008; Aviation series. Connectors, optic, rectangular, rack and panel, multiple contacts, 1,25 diameter ferrule, with removable alignment sleeve holder. Socket optical connector. product standard
• EN 4641-001: 2009; Aviation series. Cables, optics, 125 μm diameter plating. Technical specification
• EN 4641-100 : 2015 ; Aviation series. Cables, optical plated 125 $Gmm diameter. Tight construction 62,5/125 $Gmm core GI fiber 1,8 mm outer diameter. product standard
• EN 4641-101: 2015; Aviation series. Cables, optical plated 125 $Gmm diameter. Tight construction 62,5 $Gmm core GI fiber 0,9 mm outer diameter. product standard
• EN 4641-102: 2009; Aviation series. Cables, optic 125 $Gmm outer diameter sheathed. Semi-loose 62,5/125 $Gmm GI fiber nominal 1,8 mm OD. product standard
• EN 4641-103: 2010; Aviation series. Cables, optical plated 125 $Gmm diameter. Semi-loose, reinforced single-sided construction 62,5/125 $Gmm GI fiber nominal 2,74 mm, outer diameter. product standard
• EN 4641-104: 2010; Aviation series. Cables, optical plated 125 $Gmm diameter. Semi-loose, reinforced duplex construction 62,5/125 $Gmm GI fiber nominal, 4,95mm OD. product standard
• EN 4641-105 : 2010 ; Aviation series. Cables, optical plated 125 $Gmm diameter. Semi-loose, ruggedized four-axis construction 62,5/125 $Gmm GI fiber nominal, 5,72mm OD. product standard
• EN 4641-301 : 2011 ; Aviation series. Cables, optical plated 125 $Gmm diameter. Tight construction 50/125 $Gmm GI fiber nominal 1,8 mm OD. product standard
• EN 4642: 2009; Aviation series. Steel FE-PM 3504 (X4CrNiMo16-5-1). The air has melted. Hardened and tempered. Sheet and plate. 0,6mm 3L and 3L 50mm. 900 MPa 3L Rm 3L 1050 MPa.
• EN 4644-001: 2012; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Technical specification
• EN 4644-002: 2012; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Features of performance and communication arrangements
• EN 4644-003: 2009; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC continuous. Inserts rectangles. product standard
• EN 4644-003: 2011; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Inserts rectangles. product standard
• EN 4644-003: 2016; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Inserts rectangles. product standard
• EN 4644-012 : 2015 ; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Socket, size 1, class A, C and E. product standard
• EN 4644-014: 2015; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Socket, size 1, grounding block, class B and F. product standard
• EN 4644-021: 2015; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175^DC (or 125^DC) continuous. Plug, size 2, without mounting holes, class A, C and E. product standard
• EN 4644-022: 2015; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175^DC (or 125^DC) continuous. Plug, size 2, with mounting hole, class A, C and E. product standard
• EN 4644-023: 2015; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175^DC (or 125^DC) continuous. Plug, size 2, with earth block, class B and F. product standard
• EN 4644-024: 2015; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Socket size 2, class A, C and E. Product standard
• EN 4644-025: 2015; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Socket, size 2, flanged, class A, C and E. product standard
• EN 4644-026: 2015; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Slot size with grounding block, class B and F 2. Product standard
• EN 4644-131: 2011; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Size 3 plug for rack and panel applications. product standard
• EN 4644-131 : 2015 ; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Size 3 plugs, class C and D for rack and panel applications. product standard
• EN 4644-133: 2011; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. 3D slot for rack and panel application. product standard
• EN 4644-133: 2016; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. 3D slot for rack and panel application, class C and D. Product Standard
• EN 4644-141 : 2011 ; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. No. 4 plug for rack and panel applications. product standard
• EN 4644-141 : 2016 ; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Size 4 plugs, class C and D for rack and panel applications. product standard
• EN 4644-142: 2012; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175^DC (or 125^DC) continuous. Size 4 slots for rack and panel application. product standard
• EN 4644-201 : 2015 ; Aviation series. Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 ^DC (or 125 ^DC) continuous. Locking and polarization hardware. product standard
• EN 4645-002: 2009; Aviation series. Connectors, optical, circular, single and multi-pin, coupled with threaded ring, self-locking 1,25 mm diameter ring with removable alignment sleeve retainer. Features of performance and communication arrangements
• EN 4645-003: 2009; Aviation series. Connectors, optical, circular, single and multi-pin, coupled with threaded ring, self-locking 1,25 mm diameter ring with removable alignment sleeve retainer. Square flange seat. product standard
• EN 4645-004: 2009; Aviation series. Connectors, optical, circular, single and multi-pin, coupled with threaded ring, self-locking 1,25 mm diameter ring with removable alignment sleeve retainer. Jam nut slot. product standard
• EN 4645-005 : 2009 ; Aviation series. Connectors, optical, circular, single and multi-pin, coupled with threaded ring, self-locking 1,25 mm diameter ring with removable alignment sleeve retainer. Receipt. product standard
• EN 4649 : 2009 ; Aviation series. Handheld fire extinguishers with syngas for aircraft use. Technical specification and qualification conditions.
• EN 4650 : 2010 ; Aviation series. Wire and cable marking process, UV Laser.
• EN 4651: 2014; Aviation series. Copper-clad aluminum alloy conductors for electrical wiring. Product standard.
• EN 4652-001: 2015; Aviation series. Connectors, coaxial, radio frequency. Technical specification
• EN 4652-110 : 2015 ; Aviation series. Connectors, coaxial, radio frequency. Type 1, BNC interface. Clamp nut mounting version. Straight plug. product standard
• EN 4652-111 : 2015 ; Aviation series. Connectors, coaxial, radio frequency. Type 1, BNC interface. Clamp nut mounting version. Right angle plug. product standard
• EN 4652-112 : 2015 ; Aviation series. Connectors, coaxial, radio frequency. Type 1, BNC interface. Clamp nut mounting version. Square flange seat. product standard
• EN 4652-113 : 2015 ; Aviation series. Connectors, coaxial, radio frequency. Type 1, BNC interface. Clamp nut mounting version. Partition slot. product standard
• EN 4652-211 : 2015 ; Aviation series. Connectors, coaxial, radio frequency. Type 2, TNC interface. Clamp nut mounting version. Right angle plug. product standard
• EN 4652-212 : 2015 ; Aviation series. Connectors, coaxial, radio frequency. Type 2, TNC interface. Clamp nut mounting version. Square flange seat. product standard
• EN 4652-310: 2015; Aviation series. Connectors, coaxial, radio frequency. Type 3, N interface. Clamp nut mounting version. Straight plug. product standard
• EN 4655 : 2010 ; Aviation series. Steel FEPM1506 (X1CrNiMoAlTi12-10-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. bars. a or D 3L 200 mm. 3 million dollars 1400 MPa.
• EN 4656: 2010; Aviation series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. bars. a or D 3L 200 mm. $3 million, 1520 MPa.
• EN 4657: 2010; Aviation series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. bars. a or D 3L 200 mm. $3 million, 1650 MPa.
• EN 4658 : 2010 ; Aviation series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Tattoos. a or D 3L 200 mm. R$dm 3 million 1520 MPa.

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.