EN European Norm Tests Part 54

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 4659 : 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 1650 MPa.
• EN 4660-001: 2011; Aviation series. Modular and open avionics architectures. Architectural
• EN 4660-002: 2011; Aviation series. Modular and open avionics architectures. Common functional modules
• EN 4660-003: 2011; Aviation series. Modular and open avionics architectures. Communication/Network
• EN 4660-004: 2011; Aviation series. Modular and open avionics architectures. Packaging
• EN 4660-005: 2011; Aviation series. Modular and open avionics architectures. Software
• EN 4662: 2010; Aviation series. Test specifications for vibration control components.
• EN 4670 : 2010 ; Aviation series. Steel FEPM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Softened. Tattoo stock. a or D 3L 300 mm.
• EN 4671 : 2010 ; Aviation series. Steel FE-PM1506 (X1CrNiMoAlTi12-10-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Tattoos. a or D 3L 200 mm. 3 million dollars 1400 MPa.
• EN 4672: 2011; Aviation series. Steel FE-PM1504 (X1CrNiMoAlTi12-10-2). Vacuum induction melted and consumable electrode remelted. Softened. Tattoo stock. a or D 3L 300 mm.
• EN 4673-001: 2010; Aviation series. Bits, UNJ threads, with self-locking, self-opening keys. Installation and uninstallation procedure
• EN 4673-002 : 2010 ; Aviation series. Bits, UNJ threads, with self-locking, self-opening keys. design standard
• EN 4673-003: 2010; Aviation series. Bits, UNJ threads, with self-locking, self-opening keys. Technical specification
• EN 4673-004 : 2010 ; Aviation series. Bits, UNJ threads, with self-locking, self-opening keys. Heat resistant nickel base alloy NI-P100HT (Inconel 718), silver plated
• EN 4673-005 : 2010 ; Aviation series. Bits, UNJ threads, with self-locking, self-opening keys. Heat resistant nickel base alloy NI-P101HT (WASPALOY), silver plated
• EN 4673-006 : 2010 ; Aviation series. Bits, UNJ threads, with self-locking, self-opening keys. Made of heat resistant steel FE-PA2601 (A286), MoS2 coated
• EN 4674-001: 2015; Aviation series. Electrical wiring, installation. Self wrapping shielding (EMI) protective sheath. Technical specification
• EN 4674-002 : 2015 ; Aviation series. Electrical wiring, installation. Self-enveloping shielding (EMI) protective sheath. General and product standard list
• EN 4674-003: 2015; Aviation series. Electrical wiring, installation. Self-enveloping shielding (EMI) protective sheath. open arm. In the pressurized area. EMI shielding 5 kA . temperature range. 65^DC to 200^DC. product standard
• EN 4674-004 : 2015 ; Aviation series. Electrical wiring, installation. Self-enveloping shielding (EMI) protective sheath. open arm. outside the pressure area. EMI shielding 10 kA. Temperature range -65 ^DC to 200 ^DC. product standard
• EN 4675 : 2011 ; Aviation series. Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0;4Fe). Rm $3M 1 300 MPa. bars. At 0L 110mm.
• EN 4677-001: 2012; Aviation series. Welded and brazed assemblies for aerospace construction. Combinations of metallic materials with electron beam welding. Quality of weldments
• EN 4678 : 2011 ; Aviation series. Welded joints and solders for aerospace structures. Combinations of metallic materials with laser beam welding. Quality of resources.
• EN 4681-001: 2012; Aviation series. General purpose electrical cables with aluminum or copper-clad aluminum conductors. Technical specification
• EN 4681-002 : 2012 ; Aviation series. General purpose electrical cables with aluminum or copper-clad aluminum conductors. general
• EN 4681-005 : 2015 ; Aviation series. Electrical, general purpose cables with aluminum or copper-clad aluminum conductors. The AZ family is for use in a single, low pressure atmosphere. product standard
• EN 4681-006: 2015; Aviation series. General purpose electrical cables with aluminum or copper-clad aluminum conductors. AZA family, single and multi-core assembly for use in low pressure atmosphere. product standard
• EN 4683: 2011; Aviation series. Steel FE-WM 3504 (X4CrNiMo16-5-1). The air has melted. Filler metal for welding. Wire and rod.
• EN 4685: 2011; Aviation series. Titanium Ti10V2Fe3Al. bars. D $0L 110mm. $3 million 1240 MPa.
• EN 4686: 2014; Aviation series. Titanium alloy pipe coupling 8$0D30′. Equipped blind ferrules.
• EN 4687: 2012; Aviation series. Paints and varnishes. Chromate-free, anti-corrosion, two-component cold curing primer for military applications.
• EN 4688 : 2012 ; Aviation series. Paints and varnishes. Two-component anti-corrosion cold curing primer for military applications.
• EN 4689: 2012; Aviation series. Paints and varnishes. Two component cold curing polyurethane coating. High flexibility and chemical resistance for military applications.
• EN 4697 : 2012 ; Aviation series. General and installation requirements for passenger seat equipment.
• EN 4697 : 2016 ; Aviation series. General and installation requirements for passenger seat equipment.
• EN 4700-001: 2010; Aviation series. Steel and heat resistant alloys. Forged products. Technical specification. Plate, sheet and strip
• EN 4700-002: 2010; Aviation series. Steel and heat resistant alloys. Forged products. Technical specification. Bar and section
• EN 4700-002: 2016; Aviation series. Steel and heat resistant alloys. Forged products. Technical specification. Bar and section
• EN 4700-003: 2010; Aviation series. Steel and heat resistant alloys. Forged products. Technical specification. Tube
• EN 4700-004: 2010; Aviation series. Steel and heat resistant alloys. Forged products. Technical specification. Phone
• EN 4700-005 : 2010 ; Aviation series. Steel and heat resistant alloys. Forged products. Technical specification. tattoo stock
• EN 4700-006: 2010; Aviation series. Steel and heat resistant alloys. Forged products. Technical specification. Pre-production and production forgings
• EN 4700-007: 2010; Aviation series. Steel and heat resistant alloys. Forged products. Technical specification. remelt stock
• EN 4701-001: 2013; Aviation series. Connectors, optical, rectangular, modular, operating temperature 125^DC, for EN 4531-101 contacts. Technical specification
• EN 4701-001: 2014; Aviation series. Connectors, optical, rectangular, modular, operating temperature 125 ^DC, for EN 4531-101 contacts. Technical specification
• EN 4701-002 : 2013 ; Aviation series. Connectors, optical, rectangular, modular, operating temperature 125 ^DC, for EN 4531-101 contacts. Material
• EN 4701-002: 2016; Aviation series. Connectors, optical, rectangular, modular, operating temperature 125 ^DC, for EN 4531-101 contacts. Features of performance
• EN 4701-003: 2013; Aviation series. Connectors, optical, rectangular, modular, operating temperature 125^DC, for EN 4531-101 contacts. Module series 2 ; product standard
• EN 4704: 2012; Aviation series. Tartaric-Sulfuric-Acid anodization of aluminum and aluminum wrought alloys for corrosion protection and paint pretreatment (TSA).
• EN 4707: 2014; Aviation series. Acid cleaning of hexavalent chromium-free aluminum and aluminum alloy.
• EN 4708-001: 2014; Aviation series. Sheath, heat shrink, for bonding, sealing and identification. Technical specification
• EN 4710-01: 2015; Aviation series. Quick-release fastening systems for non-structural applications. Technical specification
• EN 4710-02: 2015; Aviation series. Quick-release fastening systems for non-structural applications. Spring clamp stud combination
• EN 4710-03: 2015; Aviation series. Quick-release fastening systems for non-structural applications. spring clamp
• EN 4710-04: 2015; Aviation series. Quick-release fastening systems for non-structural applications. Spring clamp. One-way tolerance compensation
• EN 4710-05 : 2015 ; Aviation series. Quick-release fastening systems for non-structural applications. Spring clamp. Two way tolerance compensation
• EN 4710-06: 2015; Aviation series. Quick-release fastening systems for non-structural applications. Stud. Quick release and locking
• EN 4710-07 : 2015 ; Aviation series. Quick-release fastening systems for non-structural applications. retaining washer
• EN 4720: 2014; Aviation series. Steel X4CrNiMo16-5-1 (1;4418). Melted air and electroslag were remelted (ESR). Hardened and tempered. Rod. 3L 200mm. 1 150 MPa 3L Rm 3L 1 300 MPa.
• EN 4721: 2014; Aviation series. Steel X4CrNiMo16-5-1 (1;4418). Melted air and electroslag were remelted (ESR). Hardened and tempered. Rod. 3L 200mm. 900 MPa $3L Rm $3L 1 050 MPa.
• EN 4723 : 2015 ; Aviation series. Standardized measurement methods for comfort and living space criteria for aircraft passenger seats.
• EN 4725: 2014; Aviation series. Aluminum alloy AL-P2024- Al Cu4Mg1 ; T351 ; Plate. 6mm 2J and 3L 150mm.
• EN 4726: 2015; Aviation series. Acceptance of cosmetic changes to the appearance of aircraft cabin parts.
• EN 4800-001: 2010; Aviation series. Titanium and titanium alloys. Technical specification. Plate, sheet and strip
• EN 4800-002: 2010; Aviation series. Titanium and titanium alloys. Technical specification. Bar and section
• EN 4800-003: 2010; Aviation series. Titanium and titanium alloys. Technical specification. Tube
• EN 4800-004: 2010; Aviation series. Titanium and titanium alloys. Technical specification. Phone
• EN 4800-005 : 2010 ; Aviation series. Titanium and titanium alloys. Technical specification. tattoo stock
• EN 4800-006: 2010; Aviation series. Titanium and titanium alloys. Technical specification. Pre-production and production forgings
• EN 4800-007 : 2010 ; Aviation series. Titanium and titanium alloys. remelt stock
• EN 4800-008: 2010; Aviation series. Titanium and titanium alloys. Technical specification. Pre-production and production castings
• EN 4817: 2012; Aviation series. Passive UHF RFID tags for aircraft use.
• EN 4818 : 2012 ; Aviation series. Passive HF RFID tags for aircraft use.
• EN 4819 : 2012 ; Aviation series. Communication Memory Button (CMB) tags designed for use in aircraft.
• EN 4826: 2014; Aviation series. Coating of steels with specified tensile strength 3L 1 450 MPa, copper alloys, nickel alloys and aluminum alloys with Zinc-Nickel (12-16% Ni) for parts and fasteners.
• EN 6031: 2015; Aviation series. Fiber reinforced plastics. Test method. Determination of in-plane shear properties (±45$0D tensile test).
• EN 6032: 2015; Aviation series. Fiber reinforced plastics. Test method. Determination of glass transition temperatures.
• EN 6033: 2015; Aviation series. Carbon fiber reinforced plastics. Test method. Determination of fracture toughness energy between layers. Mode I. GIC.
• EN 6034: 2015; Aviation series. Carbon fiber reinforced plastics. Test method. Determination of fracture toughness energy between layers. Mode II. GIIC.
• EN 6035: 2015; Aviation series. Fiber reinforced plastics. Test method. Determination of notched and unnotched tensile strength.
• EN 6036: 2015; Aviation series. Fiber reinforced plastics. Test method. Determination of notched, unnotched and filled hole compression strength.
• EN 6037 : 2015 ; Aviation series. Fiber reinforced plastics. Test method. Determination of bearing strength.
• EN 6038: 2015; Aviation series. Fiber reinforced plastics. Test method. Determination of compression strength after impact.
• EN 6049-001: 2015; Aviation series. Electrical wiring, installation. Protection sheath in meta-aramid fibres. Technical specification
• EN 6049-002 : 2010 ; Aviation series. Electrical wiring, installation. Protection sheath in meta-aramid fibres. List of general and product standards
• EN 6049-003: 2009; Aviation series. Electrical wiring, installation. Protection sheath in meta-aramid fibres. Braided, tubular, expandable. product standard
• EN 6049-005: 2014; Aviation series. Electrical wiring, installation. Protection sheath in meta-aramid fibres. The arm is flexible, post-installation. product standard
• EN 6049-006: 2012; Aviation series. Electrical wiring, installation. Protection sheath in meta-aramid fibres. Self-wrapping protective sleeve, flexible post-installation. product standard
• EN 6049-007: 2012; Aviation series. Electrical wiring, installation. Protection sheath in meta-aramid fibres. Self-wrapping mechanical and electrical protective jacket, flexible post-installation operating temperature from -55^DC to 260^DC. product standard
• EN 6049-008: 2013; Aviation series. Electrical wiring, installation. Protective covers made of meta-aramid fiber. Nickel copper braid, self-winding shield (EMI) shielding sheath, flexible post-installation operating temperature from -55^DC to 200^DC. product standard
• EN 6049-009: 2016; Aviation series. Electrical wiring, installation. Protection sheath in meta-aramid fibres. Self-closing fire protection sleeve, flexible, post-installation, operating temperature -55 ^DC to 260 ^DC. product standard
• EN 6059-100 : 2011 ; Aviation series. Electrical wiring, installation. Protection arms. Test methods. general
• EN 6059-100 : 2015 ; Aviation series. Electrical wiring, installation. Protection arms. Test methods. general
• EN 6059-308: 2014; Aviation series. Electrical wiring, installation. Protection arms. Test methods. rapid temperature change
• EN 6059-406: 2014; Aviation series. Electrical wiring, installation. Protection arms. Test methods. Vibration
• EN 6059-501 : 2010 ; Aviation series. Electrical wiring, installation. Protection arms. Test methods. voltage proof test
• EN 6059-502: 2009; Aviation series. Electrical wiring, installation. Protection arms. Test methods. Resistance to electric arcs
• EN 6059-502: 2014; Aviation series. Electrical wiring, installation. Protection arms. Test methods. Resistance to electric arcs
• EN 6059-503: 2012; Aviation series. Electrical wiring, installation. Protection arms. Test methods. Temperature rise due to rated current injected into the sleeve
• EN 6059-504: 2014; Aviation series. Electrical wiring, installation. Protection arms. Test methods. Temperature rise inside the loom due to self-heating when protected by a sleeve

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.