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DIN EN 2500-4 |
(DRAFT) Aerospace series - Instructions for the drafting and use of metallic material standards - Part 4: Specific requirements for titanium and titanium alloys; inactive for new design |
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DIN EN 2536 |
Aerospace series - Hard anodizing of aluminium alloys; German version EN 2536:1995 |
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DIN EN 2551 |
(DRAFT) Aerospace series - Rivets, solid, 100° normal countersunk head with dome, in aluminium alloy 2117, inch based series |
|
DIN EN 2557 |
Aerospace series - Carbon fibre preimpregnates - Determination of mass per unit area; German version EN 2557:1997 |
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DIN EN 2558 |
Aerospace series - Carbon fibre preimpregnates - Determination of the volatile content; German version EN 2558:1997 |
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DIN EN 2561 |
Aerospace series - Carbon fibre reinforced plastics - Unidirectional laminates - Tensile test parallel to the fibre direction; German version EN 2561:1995 |
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DIN EN 2564 |
Aerospace series - Carbon fibre laminates - Determination of the fibre-, resin- and void contents; German version EN 2564:1998 |
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DIN EN 2585 |
Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Wide series - Elevated load at ambient temperature - Dimensions and loads; German and English version EN 2585:2001 |
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DIN EN 2591-603 |
Aerospace series - Elements of electrical and optical connection; Test methods - Part 603: Optical elements; Change of power distribution; German version EN 2591-603:2002 |
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DIN EN 2597 |
Aerospace series - Carbon fibre reinforced plastics; unidirectional laminates - Tensile test perpendicular to the fibre direction; German version EN 2597:1998 |
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DIN EN 2632 |
Aerospace series - Aluminium alloy AL-P7075-T73511 - Extruded bar and section - a or D = 150 mm with peripheral coarse grain control; German and English version EN 2632:2005 |
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DIN EN 2635 |
Aerospace series - Aluminium alloy AL-P2014A-T6511 - Extruded bar and section - a or D ≤ 200 mm with peripheral coarse grain control; German and English version EN 2635:2005 |
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DIN EN 2646 |
(DRAFT) Aerospace series - Nipples, lubricating, axial type, in steel, cadmium plated |
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DIN EN 2660 |
(DRAFT) Aerospace series - Heat resisting alloy CO-CH1401 - As cast, remelting stock |
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DIN EN 2713-003 |
Aerospace series - Cables, electrical, single and multicore for general purpose - Operating temperatures between -55 °C and 200 °C - Part 003: Screened (spiral) and jacketed, ink jet printable - Product standard; German and English version EN 2713-003:2005 |
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DIN EN 2713-006 |
(DRAFT) Aerospace series - Cables, electrical, single and multicore for general purpose - Operating temperatures between -55 °C and 200 °C - Part 006: Screened (braided) and jacketed, CO2 laser printable; product standard |
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DIN EN 2714-003 |
Aerospace series - Cables, electrical, single and multicore for general purpose - Operating temperatures between -55 °C and 260 °C - Part 003: Screened (spiral) and jacketed, ink jet printable - Product standard; German and English version EN 2714-003:2005 |
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DIN EN 2755 |
(DRAFT) Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Series elevated loads at ambient temperature; technical specification |
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DIN EN 2763 |
(DRAFT) Aerospace series - Steel FE-PL1504 (33CrMoV12), air melted, hardened and tempered - Bar for machining, De ≤ 80 mm, 1200 MPa ≤ Rm ≤ 1350 MPa |
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DIN EN 2764 |
(DRAFT) Aerospace series - Steel FE-PL1504 (33CrMoV12) air melted, hardened and tempered - Hand and die forgings, De ≤ 80 mm, 1200 MPa ≤ Rm ≤ 1400 MPa |
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DIN EN 2803 |
Aerospace series - Aluminium alloy AL-P7475-T761 - Clad sheet and strip - 1,0 mm ≤ a ≤ 6 mm; German and English version EN 2803:2005 |
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DIN EN 2817 |
(DRAFT) Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) consumable electrode remelted, solution treated and precipitation treated - Bar for machining a or D ≤ 200 mm, Rm ≥ 1070 MPa |
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DIN EN 2821 |
Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D = 200 mm - Rm = 1310 MPa; German and English version EN 2821:2007 |
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DIN EN 2883 |
(DRAFT) Aerospace series - Nuts, hexagonal, self-locking, with counterbore and captive washer, in heat resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C |
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DIN EN 2899 |
(DRAFT) Aerospace series - Vulcanized rubbers - Test on the susceptibility to corrosion in a damp atmosphere of metals in contact with vulcanized rubbers |
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DIN EN 2909 |
Aerospace series - Nuts, bihexagonal, self-locking, deep counterbored, in heat resisting steel FE-PA92HT (A286), silver plated - Classification: 1100 MPa (at ambient temperature)/650 °C; German version EN 2909:1995 |
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DIN EN 2911 |
Aerospace series - Shank nuts, self-locking, in heat resisting steel FE-PA92HT (A286), silver plated - Classification: 1100 MPa (at ambient temperature)/650 °C; German version EN 2911:1995 |
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DIN EN 2912 |
Aerospace series - Washers, flat, large diameter, in aluminium alloy, anodized or chromated; German version EN 2912:1996 |
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DIN EN 2913 |
Aerospace series - Washers, flat, large diameter, in steel, cadmium plated; German version EN 2913:1999 |
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DIN EN 2922 |
(DRAFT) Aerospace series - Nuts, hexagon, plain, reduced height, reduced across flats, in heat resisting steel, passivated, left hand thread; Classification: 600 MPa (at ambient temperature)/650 °C |
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DIN EN 2925 |
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286) - Classification: 900 MPa (at ambient temperature)/650 °C; German version EN 2925:1994 |
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DIN EN 2926 |
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated - Classification: 900 MPa (at ambient temperature)/650 °C; German version EN 2926:1996 |
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DIN EN 2927 |
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718) - Classification: 1275 MPa (at ambient temperature)/650 °C; German version EN 2927:1996 |
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DIN EN 2928 |
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plated - Classification: 1275 MPa (at ambient temperature)/650 °C; German version EN 2928:1996 |
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DIN EN 2929 |
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy) - Classification: 1210 MPa (at ambient temperature)/730 °C; German version EN 2929:1996 |
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DIN EN 2930 |
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated - Classification: 1210 MPa (at ambient temperatur)/730 °C; German version EN 2930:1996 |
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DIN EN 2931 |
Aerospace series - Bolts, T-head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286) - Classification: 900 MPa (at ambient temperature)/650 °C; German version EN 2931:1994 |
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DIN EN 2951 |
(DRAFT) Aerospace series - Metallic materials - Test method; micrographic determination of content of non-metallic inclusions |
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DIN EN 2959 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al), solution treated and cold worked - Bar for forged fasteners 3 mm ≤ D ≤ 30 mm |
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DIN EN 2995-004 |
(DRAFT) Aerospace series - Circuit breakers, single-pole, temperature compensated, rated currents 1 A to 25 A - Part 004: With signal contact and unified mounting hardware, centre-to-centre distance of terminals 18 mm; product standard |
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DIN EN 3019 |
(DRAFT) Aerospace series; self-locking plate nuts, floating, two-lug, in heat resisting steel FE-PA92HT (A286); classification: 1100 MPa (at ambient temperature)/650 °C |
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DIN EN 3038 |
Aerospace series - Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in heat and corrosion resisting steel, passivated - Classification: 1100 MPa (at ambient temperature)/425 °C; German version EN 3038:1996 |
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DIN EN 3048 |
Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Light series - Elevated load at ambient temperature - Dimensions and loads; German and English version EN 3048:2001 |
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DIN EN 3049 |
Aerospace series - O-rings, in fluorocarbon rubber (FKM) low compression set - Hardness 80 IRHD; German version EN 3049:1998 |
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DIN EN 3150 |
Aerospace series - Pins, shoulder, headless, in heat resisting nickel base alloy NI-P100HT (Inconel 718); German version EN 3150:1995 |
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DIN EN 3161 |
(DRAFT) Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, solution treated and precipitation treated - Bar, a or D ≤ 200 mm, Rm ≥ 930 MPa |
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DIN EN 3207 |
Aerospace series - Rubber compounds - Technical specification; German version EN 3207:1998 |
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DIN EN 3219 |
(DRAFT) Aerospace series; heat resisting nickel base alloy (Ni-P100 HT); cold worked and softened; bar and wire for continuous forging or extrusion for fasteners 3 ≤ D ≤ 30 mm |
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DIN EN 3228 |
(DRAFT) Aerospace series; nuts, hexagon, plain, reduced height, normal across flats, in steel, cadmium plated; classification: 900 MPa (at ambient temperature)/235 °C |
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DIN EN 3280 |
Aerospace series; bearings, airframe rolling, rigid or self-aligning; technical specification; German version EN 3280:1994 |
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DIN EN 3284 |
Aerospace series; bearings, airframe rolling - Rigid single row ball bearings in steel - Diameter series 0 and 2; normal clearance category; dimensions and loads; German version EN 3284:1994 |
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DIN EN 3285 |
Aerospace series; bearings, airframe rolling - Rigid single row ball bearings in steel, cadmium plated - Diameter series 0 and 2; normal clearance category; dimensions and loads; German version EN 3285:1994 |
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DIN EN 3289 |
Aerospace series; bearings, airframe rolling - Double row self-aligning ball bearings in corrosion resisting steel - Diameter series 2; dimensions and loads; German version EN 3289:1994 |
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DIN EN 3335 |
Aerospace series - Aluminium alloy AL-P7475-O2 - Sheet for superplastic forming (SPF) - 0,8 mm ≤ a ≤ 6 mm; German and English version EN 3335:2005 |
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DIN EN 3357 |
(DRAFT) Aerospace series - Steel FE-PM1503 (X3CrNiMoAl 13-8-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Bar for machining a or D ≤ 150 mm, 1200 MPa ≤ Rm ≤ 1400 MPa |
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DIN EN 3380 |
Aerospace series - Rings, retaining - Technical specification; German version EN 3380:1996 |
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DIN EN 3382 |
(DRAFT) Aerospace series; rings retaining, internal, axial mounting, steel, phosphated |
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DIN EN 3383 |
(DRAFT) Aerospace series; rings retaining, internal, axial mounting, steel, vacuum cadmium plated |
|
DIN EN 3386 |
(DRAFT) Aerospace series; rings retaining, radial mounting, steel, phosphated |
|
DIN EN 3404 |
(DRAFT) Aerospace series; rivets, solid, universal head, in aluminium alloy 5056A, anodized or chromated; metric series |
|
DIN EN 3464 |
(DRAFT) Aerospace series - Titanium alloy TI-P64001, annealed - Plates 6 mm |
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DIN EN 3507 |
Aerospace series - Steel FE-PL1501 (30CrMo12) - Air melted - Hardened and tempered - Forgings - De = 100 mm - 930 MPa = Rm = 1080 MPa; German and English version EN 3507:2006 |
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DIN EN 3508 |
(DRAFT) Aerospace series - Steel FE-PL1501 (30CrMo12), air melted, hardened and tempered - Bar De ≤ 100 mm, 930 MPa ≤ Rm ≤ 1080 MPa |
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DIN EN 3509 |
(DRAFT) Aerospace series - Steel FE-PL1501 (30CrMo12), air melted, hardened and tempered - Bar De ≤ 40 mm, 1050 MPa ≤ Rm ≤ 1250 MPa |
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DIN EN 3511 |
(DRAFT) Aerospace series - Steel FE-PL1801 (100Cr6), vacuum induction melted and consumable electrode remelted, softened - Bar for the manufacture of machined bearings a or D ≤ 130 mm |
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DIN EN 3518 |
(DRAFT) Aerospace series - Steel FE-PL2105 - Air melted; hardened and tempered; forgings De ≤ 150 mm, 1080 MPa ≤ Rm ≤ 1280 MPa |
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DIN EN 3521 |
(DRAFT) Aerospace series - Steel FE-PL2106 (30CrNiMo8) air melted, hardened and tempered - Bar for machining De ≤ 150 mm, 900 MPa ≤ Rm ≤ 1100 MPa |
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DIN EN 3544-5 |
(DRAFT) Aerospace series - Titanium and titanium alloys; wrought products; technical specification - Part 5: Wire |
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DIN EN 3615 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Determination of the conditions of exposure to humid atmosphere and of moisture absorption |
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DIN EN 3646-003 |
Aerospace series - Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous - Part 003: Receptacle, square flange mounting - Product standard; German and English version EN 3646-003:2006 |
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DIN EN 3661-005 |
(DRAFT) Aerospace series - Circuit breakers, single-pole, temperature compensated, rated current 20 A to 50 A - Part 005: With polarized signal contact and unified mounting hardware, centre-to-centre distance of terminals 21 mm; product standard |
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DIN EN 3665 |
Aerospace series - Test methods for paints and varnishes - Filiform corrosion resistance test on aluminium alloys; German version EN 3665:1997 |
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DIN EN 3680 |
(DRAFT) Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) air melted, solution treated - Seamless tube for pressure applications D ≤ 50 mm; 0,5 mm ≤ a ≤ 5 mm, 500 MPa ≤ Rm ≤ 750 MPa |
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DIN EN 3700 |
(DRAFT) Aerospace series; static inverters for aircraft; technical specification |
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DIN EN 3726 |
Aerospace series - Nuts, self-locking, clip, in heat resisting steel FE-PA2601 (A286), MoS2 coated - Classification: 1100 MPa (at ambient temperature)/425 °C; German and English version EN 3726:2004 |
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DIN EN 3745-306 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 306: Variation of attenuation during temperature cycling; German and English version EN 3745-306:2005 |
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DIN EN 3745-512 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 512: Flexure endurance; German and English version EN 3745-512:2005 |
|
DIN EN 3748 |
Aerospace series - O-ring grooves - Dimensions; German and English version EN 3748:2001 |
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DIN EN 3766 |
(DRAFT) Aerospace series - Rivets, blind, nut plate, universal head, in heat resisting steel, passivated, metric series |
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DIN EN 3771 |
(DRAFT) Aerospace series - Nuts, bihexagonal, plain, in heat resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C |
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DIN EN 3837 |
(DRAFT) Aerospace series - Paints and varnishes - Nature and method for surface preparation of test pieces in aluminium alloys |
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DIN EN 3841-308 |
Aerospace series - Circuit breakers - Test methods - Part 308: Lightning; German and English version EN 3841-308:2004 |
|
DIN EN 3845 |
(DRAFT) Aerospace series - Rings, retaining, radial mounting, in corrosion resisting steel, passivated |
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DIN EN 3859 |
(DRAFT) Aerospace series; titanium alloy TI-P19001; annealed, sheet and strip, hot rolled, a ≤ 6 mm |
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DIN EN 3869 |
(DRAFT) Aerospace series - Pipe couplings, loose flanges and seals - Seals in fluorocarbon rubber and armature in aluminium alloy |
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DIN EN 3954 |
Aerospace series - Silver base alloy AG-B12401 (AgCu40Zn5Ni) - Filler metal for brazing, powder or paste; German version EN 3954:2001 |
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DIN EN 3988 |
(DRAFT) Aerospace series - Test methods for metallic materials - Constant amplitude strain-controlled low cycle fatique testing |
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DIN EN 3990 |
(DRAFT) Aerospace series - Steel FE-PA2801 (X60NiMnCr13-5-3), softened - Bar for machining De ≤ 150 mm, 620 MPa ≤ Rm ≤ 900 MPa |
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DIN EN 4002 |
(DRAFT) Aerospace series - Aluminium alloy AL-P2219-T81 - Sheet and strip; 0,5 mm ≤ (kursiv)a ≤ 6 mm |
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DIN EN 4008-007 |
(DRAFT) Aerospace series - Elements of electrical and optical connection; crimping tools and associated accessories - Part 007: Positioner for crimping tool M22520/2-01; product standard |
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DIN EN 4019 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbows 90°, welded end; German version EN 4019:2001 |
|
DIN EN 4020 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbows 90°, welded end with thrust wire nut; German and English version EN 4020:2001 |
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DIN EN 4050-1 |
(DRAFT) Aerospace series - Test method for metallic materials; ultrasonic inspection of bars, plates, forging stock and forgings - Part 1: General requirements |
|
DIN EN 4050-4 |
(DRAFT) Aerospace series - Test method for metallic materials; ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria |
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DIN EN 4063 |
(DRAFT) Aerospace series - Wire in filler metal for brazing; diameter 0,6 mm ≤ D ≤ 4 mm; dimensions |
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DIN EN 4078 |
(DRAFT) Aerospace series - Inserts, threaded, thin wall, locked and self-locking, in heat resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C |
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DIN EN 4109 |
(DRAFT) Aerospace series - Wrenches, face spanner |
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DIN EN 4123 |
Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread - Classification: 1550 MPa (at ambient temperature)/600 °C; German and English version EN 4123:2004 |
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DIN EN 4168 |
Aerospace series - Clips, spring tension, three parts - Outer clips in heat resisting steel FE-PA2601 (A286); German and English version EN 4168:2004 |
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DIN EN 4185 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees, bulkhead on run, long; German version EN 4185:2001 |
|
DIN EN 4200 |
(DRAFT) Aerospace series - Washers, 100° dimpled, in steel, cadmium plated |
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DIN EN 4330 |
Aerospace series - Steel FE-WA4802 (X8CrNiMn27-22-2) - Filler metal for welding; Wire and rod; German version EN 4330:2002 |
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DIN EN 4340 |
Aerospace series - Magnesium alloy MG-W68001 - Filler metal for welding; Wire and rod; German version EN 4340:2002 |
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DIN EN 4400-1 |
(DRAFT) Aerospace series - Aluminium and aluminium alloy wrought products; technical specification - Part 1: Plate |
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DIN EN 4400-2 |
(DRAFT) Aerospace series - Aluminium and aluminium alloy wrought products; Technical specification - Part 2: Sheet and strip |
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DIN EN 4436 |
(DRAFT) Aerospace series - Steel - Test methods; determination of δ ferrite content |
|
DIN EN 4604-003 |
(DRAFT) Aerospace series - Cable, electrical, for signal transmission - Part 003: Coaxial cable 50 Ohm, 200 °C, type WZ; Product standard |
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DIN EN 6030 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of the mechanical degradation due to chemical paint strippers |
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DIN EN 6033 |
(DRAFT) Aerospace series - Carbon fibre reinforced plastics - Test method; determination of interlaminar fracture toughness energy; mode I, GIC |
|
DIN EN 6036 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of notched, unnotched and filled hole compression strength |
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DIN EN 6040 |
(DRAFT) Aerospace series - Non-metallic materials - Test method; analysis of thermoset systems by High Performance Liquid Chromatography (HPLC) |
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DIN EN 6041 |
(DRAFT) Aerospace series - Non-metallic materials - Test method; analysis of non-metallic (uncured) by differential scanning calorimetry (DSC) |
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DIN EN 6042 |
(DRAFT) Aerospace series - Organic compounds - Test method; analysis by infrared spectroscopy |
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DIN EN 6060 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of the tensile single lap shear strength |
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DIN EN 6061 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of sandwich flexural strength, 4 point bending |
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DIN EN 9104 |
(DRAFT) Aerospace series - Quality management systems - Requirements for Aerospace Quality Management System Certification/Registrations Programs; German and English version EN 9104:2006 |
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DIN EN 9120 |
(DRAFT) Aerospace series - Quality management systems - Requirements for stockist distributors (based on ISO 9001:2000); German and English version EN 9120:2005 |
|
DIN EN 9121 |
Aerospace series - Quality management systems - Assessment applicable to stockist distributors (based on ISO 9001:2000); German and English version EN 9121:2005 |
|
DIN EN 9130 |
(DRAFT) Aerospace series - Quality systems - Record retention |
|
DIN EN 9131 |
(DRAFT) Aerospace series - Quality management systems - Nonconformance documentation |
|
DIN EN ISO 17666 |
Space systems - Risk management (ISO 17666:2003) |
|
DIN ISO 2574 |
Aerospace series - Aircraft electrical cables - Manufacturer's identification marking (ISO 2574:1994) |
|
DIN ISO 6772 |
Aerospace - Fluid systems - Impulse testing of hydraulic hose, tubing and fitting assemblies (ISO 6772:1988) |
|
DIN ISO 7320 |
Aerospace - Couplings, threaded and sealed, for fluid systems - Dimensions (ISO 7320:1992) |
|
DIN V 65900-15 |
Aerospace series - Materials for self-locking nuts, threaded inserts and screw thread inserts of temperature classes ≤ 425 °C (AECMA Technical Report TR 3791:1999) |
|
DIN V 65900-17 |
Aerospace series - O-ring grooves - Design criteria for O-ring grooves, basic calculations (AECMA Technical Report TR 4271:2000) |
|
DIN V 65900-19 |
Aerospace series - Clips, spring tension - Design recommandations (AECMA Technical Report TR 4586:2000) |
|
DIN 29878 |
(DRAFT) Aerospace - Resistance welded metal component parts - Technical specification |
|
DIN 65035 |
Aerospace; steel, nickel- and cobalt-alloy stock, forgings and rings,; technical specification |
|
DIN 65308 |
Aerospace; inserts for composite materials, with MJ thread, open type, screw-locking, corrosion-resisting steel |
|
DIN 65309 |
Aerospace; inserts for composite materials, with MJ thread, closed type, screw-locking, corrosion-resisting steel |
|
DIN 65431 |
(DRAFT) Aerospace - Sleeves, wall thickness 0,5 mm, for fasteners with countersunk head |
|
DIN 65480 |
Aerospace; hexagon nuts with flange and MJ thread, self-locking, corrosion-resisting steel; class: 1100 MPa/315 °C |
|
DIN 65507 |
Aerospace; nuts, hexagon, with MJ thread, captive washer and counterbore, self-locking, steel; class: 1100 MPa/235 °C |
|
DIN 65508 |
Aerospace; nuts, hexagon, with MJ thread, captive washer and counterbore, self-locking, corrosion-resistant steel; class: 1100 MPa/315 °C/425 °C |
|
DIN 65535 |
Aerospace; gang channel nut assembly, with self-locking nuts with MJ thread, nut spacing fixed or optional, in corrosion-resisting steel; class: 1100 MPa/315 °C |
|
DIN EN 12312-1 |
Aircraft ground support equipment - Specific requirements - Part 1: Passenger stairs; English version of DIN EN 12312-1 |
|
DIN EN 12312-10 |
Aircraft ground support equipment - Specific requirements - Part 10: Container/Pallet transfer transporters |
|
DIN EN 12312-11 |
Aircraft ground support equipment - Specific requirements - Part 11: Container/Pallet dollies and loose load trailers |
|
DIN EN 12312-14 |
Aircraft ground support equipment - Specific requirements - Part 14: Disabled/incapacitated passenger boarding vehicles |
|
DIN EN 12312-15 |
Aircraft ground support equipment - Specific requirements - Part 15: Baggage and equipment tractors |
|
DIN EN 12312-16 |
Aircraft ground support equipment - Specific requirements - Part 16: Air start equipment |
|
DIN EN 12312-17 |
Aircraft ground support equipment - Specific requirements - Part 17: Air conditioning equipment |
|
DIN EN 12312-18 |
Aircraft ground support equipment - Specific requirements - Part 18: Nitrogen or Oxygen units |
|
DIN EN 12312-19 |
Aircraft ground support equipment - Specific requirements - Part 19: Aircraft jacks, axle jacks and hydraulic tail stanchions |
|
DIN EN 12312-3 |
Aircraft ground support equipment - Specific requirements - Part 3: Conveyor belt vehicles |
|
DIN EN 12312-4 |
Aircraft ground support equipment - Specific requirements - Part 4: Passenger boarding bridges |
|
DIN EN 12312-5 |
Aircraft ground support equipment - Specific requirements - Part 5: Aircraft fuelling equipment |
|
DIN EN 12312-6 |
Aircraft ground support equipment - Specific requirements - Part 6: Deicers and deicing/antiicing equipment |
|
DIN EN 12312-7 |
Aircraft ground support equipment - Specific requirements - Part 7: Aircraft movement equipment |
|
DIN EN 12312-8 |
Aircraft ground support equipment - Specific requirements - Part 8: Maintenance stairs and platforms |
|
DIN EN 13290-1 |
Aerospace series - Space project management; General requirements - Part 1: Policy and principles; German version EN 13290-1:1999 |
|
DIN EN 13290-2 |
Aerospace - Space project management; General requirements - Part 2: Project breakdown structure; German and English version EN 13290-2:2001 |
|
DIN EN 13290-3 |
Aerospace - Space project management; General requirements - Part 3: Project organisation; German and English version EN 13290-3:2001 |
|
DIN EN 13290-4 |
Aerospace - Space project management; General requirements - Part 4: Project phasing and planning; German and English version EN 13290-4:2001 |
|
DIN EN 13290-6 |
Aerospace - Space project management; General requirements - Part 6: Information/documentation management; German and English version EN 13290-6:2001 |
|
DIN EN 13290-7 |
Aerospace - Space project management; General requirements - Part 7: Cost and schedule management; German and English version EN 13290-7:2001 |
|
DIN EN 13291-1 |
Aerospace series - Space products assurance; General requirements - Part 1: Policy and principles; German version EN 13291-1:1999 |
|
DIN EN 13291-2 |
Space product assurance - General requirements - Part 2: Quality assurance; German and English version EN 13291-2:2003 |
|
DIN EN 13291-3 |
Space product assurance - General requirements - Part 3: Materials, mechanical parts and processes |
|
DIN EN 13292 |
Aerospace series - Space engineering standards; Policy and principles; German version EN 13292:1999 |
|
DIN EN 1361 |
Rubber hoses and hose assemblies for aviation fuel handling - Specification |
|
DIN EN 13701 |
Aerospace - Space systems - Glossary of terms; Trilingual version EN 13701:2001 |
|
DIN EN 14089 |
Aerospace - Space product assurance - The control of limited-life materials; German and English version EN 14089:2002 |
|
DIN EN 14091 |
Aerospace - Space product assurance - Thermal vacuum outgassing test for the screening of space materials; German and English version EN 14091:2002 |
|
DIN EN 14093 |
Aerospace - Space project management - Organization and conduct of reviews; German and English version EN 14093:2002 |
|
DIN EN 14097 |
Aerospace - Space product assurance - Nonconformance control system; German and English version EN 14097:2001 |
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DIN EN 14098 |
Aerospace - Space product assurance - Thermal cycling test for the screening of space materials and processes; German and English version EN 14098:2001 |
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DIN EN 14100 |
Aerospace - Space product assurance - The determination of offgassing products from materials and assembled articles to be used in a manned space vehicle crew compartment; German and English version EN 14100:2001 |
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DIN EN 14101 |
Aerospace - Space product assurance - Material selection for controlling stress-corrosion cracking; German and English version EN 14101:2001 |
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DIN EN 14160 |
Aerospace - Space engineering - Software; German and English version EN 14160:2001 |
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DIN EN 14165 |
Space engineering standards - Fracture control |
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DIN EN 14514 |
Space engineering standards - Functional analysis; German and English version EN 14514:2004 |
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DIN EN 14607-1 |
Space engineering - Mechanical - Part 1: Thermal control; English version EN 14607-1:2004 |
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DIN EN 14607-3 |
(DRAFT) Space engineering - Mechanical - Part 3: Mechanisms; English version prEN 14607-3:2003 |
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DIN EN 14607-5-1 |
Space engineering - Mechanical - Part 5-1: Liquid and electric propulsion for spacecraft; English version EN 14607-5-1:2004 |
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DIN EN 14607-6 |
Space engineering - Mechanical - Part 6: Pyrotechnics; English version EN 14607-6:2004 |
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DIN EN 14607-7 |
Space engineering - Mechanical - Part 7: Mechanical parts; English version EN 14607-7:2004 |
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DIN EN 14607-8 |
Space engineering - Mechanical - Part 8: Materials; English version EN 14607-8:2004 |
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DIN EN 14611 |
(DRAFT) Space product assurance - Determination of the susceptibility of silver plated copper wire and cable to |
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DIN EN 14612 |
Space product assurance - Verification and approval of automatic machine wave soldering |
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DIN EN 14725 |
Space engineering - Verification; German and English version EN 14725:2003 |
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DIN EN 14736 |
Space product assurance - Quality assurance for test centres |
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DIN EN 14737-2 |
Space engineering - Ground systems and operations - Part 2: Documents requirements definitions (DRDs); English version EN 14737-2:2004 |
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DIN EN 14738 |
Space product assurance - Hazard analysis |
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DIN EN 14776 |
Space engineering - Ground systems and operations - Telemetry and telecommand packet utilization; English version EN 14776:2004 |
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DIN EN 14824 |
Space engineering - Testing; English version EN 14824:2003 |
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DIN EN 1915-1 |
Aircraft ground support equipment - General requirements - Part 1: Basic safety requirements; English version of DIN EN 1915-1 |
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DIN EN 1915-3 |
Aircraft ground support equipment - General requirements - Part 3: Vibration measurement methods and reduction |
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DIN EN 1915-4 |
Aircraft ground support equipment - General requirements - Part 4: Noise measurement methods and reduction |
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DIN EN 2000 |
(DRAFT) Aerospace series - Quality assurance - EN aerospace products; approval of the quality system of manufacturers |
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DIN EN 2002-13 |
(DRAFT) Aerospace series - Metallic materials; test methods - Part 13: Reserve torsion testing of wire |
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DIN EN 2002-16 |
(DRAFT) Aerospace series - Metallic materials; test methods - Part 16: Non-destructive testing, penetrant testing |
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DIN EN 2002-20 |
(DRAFT) Aerospace series - Test methods for metallic materials - Part 20: Eddy current testing of circular cross-section tubes |
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DIN EN 2002-21 |
(DRAFT) Aerospace series - Metallic materials; test methods - Part 21: Radiographic testing of castings |
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DIN EN 2002-5 |
(DRAFT) Aerospace series - Test methods for metallic materials - Part 5: Uninterrupted creep and stress-rupture testing |
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DIN EN 2002-6 |
(DRAFT) Aerospace series - Metallic materials; test methods - Part 6: Bend testing |
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DIN EN 2002-7 |
(DRAFT) Aerospace series - Metallic materials; test methods - Part 7: Hardness test |
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DIN EN 2002-8 |
(DRAFT) Aerospace series - Test methods for metallic materials - Part 8: Micrographic determination of grain size |
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DIN EN 2002-9 |
(DRAFT) Aerospace series - Metallic materials; test methods - Part 9: Tube drift expanding test |
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DIN EN 2003-009 |
Aerospace series - Test methods - Titanium and titanium alloys - Part 009: Determination of surface contamination; German and English version EN 2003-009:2007 |
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DIN EN 2003-010 |
Aerospace series - Titanium and titanium alloys - Test methods - Part 010: Sampling for determination of hydrogen content; German and English version EN 2003-010:2007 |
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DIN EN 2003-15 |
(DRAFT) Aerospace series - Test methods for metallic materials; ultrasonic testings - Part 15: Reference blocks |
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DIN EN 2003-2 |
(DRAFT) Aerospace series - Steels; test methods - Part 2: Izod impact test |
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DIN EN 2003-3 |
(DRAFT) Aerospace series - Steel; test methods - Part 3: Calibration of pendulum impact machines |
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DIN EN 2003-9 |
(DRAFT) Aerospace serie - Test methods - Titanium and titanium alloy - Part 9: Determination of surface contamination |
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DIN EN 2004-1 |
Aerospace series; test methods for aluminium and aluminium alloy products; part 1: determination of electrical conductivity of wrought aluminium alloys; German version EN 2004-1:1993 |
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DIN EN 2004-10 |
(DRAFT) Aerospace series; test methods for aluminium and aluminium alloy products; part 10: preparation of micrographic specimens for aluminium alloys |
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DIN EN 2004-5 |
Aerospace series; test methods for aluminium and aluminium alloy products; part 5: determination of cladding thickness and copper diffusion of clad semi-finished products; German version EN 2004-5:1993 |
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DIN EN 2004-7 |
(DRAFT) Aerospace series - Test methods for aluminium and aluminium alloy products - Part 7: Reference blocks for the calibration of measuring equipment used in the determination of electrical conductivity of wrought aluminium and aluminium alloys |
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DIN EN 2007 |
(DRAFT) Aerospace series - Test methods for aluminium and aluminium alloy products - Metallographic determination of cladding thickness and copper diffusion in the cladding for rolled products |
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DIN EN 2021 |
(DRAFT) Aerospace series - Metallic materials - Test methods; shear testing for thin flat product |
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DIN EN 2032-1 |
Aerospace series - Metallic materials - Part 1: Conventional designation; German and English version EN 2032-1:2001 |
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DIN EN 2032-2 |
Aerospace series; metallic materials; part 2: coding of metallurgical condition in delivery condition; German version EN 2032-2:1994 |
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DIN EN 2033 |
(DRAFT) Aerospace series - Strips, cold rolled, in steel - Thickness 0,1 mm ≤ a ≤ 2,5 mm; dimensions |
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DIN EN 2044 |
Aerospace series - Round bars, drawn, in aluminium and aluminium alloys, tolerance class h11, diameter 4 mm≤D≤63 mm - Dimensions; German and English version EN 2044:2001 |
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DIN EN 2046 |
Aerospace series - Hexagonal bars, drawn, in aluminium and aluminium alloys, tolerance class h11, width across flats 7 mm≤a≤50 mm - Dimensions; German and English version EN 2046:2001 |
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DIN EN 2047 |
Aerospace series - Beaded L-section, extruded in aluminium alloys - Dimensions; German and English version EN 2047:2001 |
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DIN EN 2048 |
Aerospace series - Extruded L-section, extruded in aluminium alloys - Dimensions; German and English version EN 2048:2001 |
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DIN EN 2049 |
Aerospace series - Extruded channel section, exruded in aluminium alloys - Dimensions; German and English version EN 2049:2001 |
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DIN EN 2050 |
Aerospace series - Extruded T-section, in aluminium alloys - Dimensions; German and English version EN 2050:2001 |
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DIN EN 2067 |
Aerospace series - Rod ends with self-aligning ball bearings - Technical specification; German version EN 2067:1996 |
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DIN EN 2068 |
Aerospace series - Rod ends with self-lubricating, self-aligning bearings - Technical specification; German version EN 2068:1996 |
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DIN EN 2070-1/A1 |
Aerospace series; aluminium and aluminium alloy wrought products; technical specification; part 1: general requirements; German version EN 2070-1/A1:1993; amendment 1 |
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DIN EN 2071 |
Aerospace series - Sheets in aluminium and aluminium alloys, thickness 0,25 mm≤a≤6 mm - Dimensions; German and English version EN 2071:2001 |
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DIN EN 2072 |
Aerospace series - Aluminium AL-P1050A-H14 - Sheet and strip - 0,4 mm = a = 6 mm; German and English version EN 2072:2005 |
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DIN EN 2082-1/A1 |
Aerospace series; aluminium alloy forging stock and forgings; technical specification; part 1: general requirements; German version EN 2082-1/A1:1993; amendment 1 |
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DIN EN 2083 |
Aerospace series - Copper or copper alloys conductors for electrical cables - Product standard; German version EN 2083:2001 |
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DIN EN 2084 |
Aerospace series - Cables, electric, single-core, general purpose, with conductors in copper or copper alloy - Technical specification; German and English version EN 2084:2005 |
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DIN EN 2085 |
Aerospace series - Aluminium alloy AL-P2618A-T6 - Hand and die forgings - a = 150 mm; German and English version EN 2085:2004 |
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DIN EN 2086 |
Aerospace series - Aluminium alloy AL-P2618A-T851 - Hand and die forgings - a ≤ 150 mm; German and English version EN 2086:2004 |
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DIN EN 2087 |
Aerospace series - Aluminium alloy AL-P2014A - T6 or T62 - Clad sheet and strip - 0,4 mm ≤ a ≤ 6 mm; German and English version EN 2087:2005 |
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DIN EN 2088 |
Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Clad sheet and strip - 0,4 mm = a = 6 mm; German and English version EN 2088:2005 |
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DIN EN 2089 |
Aerospace series - Aluminium alloy AL-P2014A-T6 or T62 - Sheet and strip - 0,4 mm = a = 6 mm; German and English version EN 2089:2005 |
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DIN EN 2090 |
Aerospace series - Aluminium alloy AL-P2024-T3 - Clad sheet and strip 0,3 mm ≤ a ≤ 6 mm; German and English version EN 2090:2005 |
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DIN EN 2094 |
Aerospace series; aluminium alloy AL-P7009-T74; die forgings 3 mm ≤ a ≤ 150 mm; German version EN 2094:1992 |
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DIN EN 2104 |
Aerospace series - Acrylonitrile-butadiene elastomer (NBR) - Hardness 40 IRHD; German version EN 2104:1996 |
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DIN EN 2123 |
(DRAFT) Aerospace series - Aluminium alloy AL-P2618A-T851 - Plate, 6 mm < a ≤ 140 mm |
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DIN EN 2124 |
(DRAFT) Aerospace series - Aluminium alloy AL-P2214-T651 - Plate, 6 mm < a ≤ 140 mm |
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DIN EN 2126 |
Aerospace series; aluminium alloy AL-P7075-T651; plate 6 mm < a ≤ 80 mm; German version EN 2126:1992 |
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DIN EN 2127 |
Aerospace series; aluminium alloy AL-P7075-T73511; extruded bars and sections a or D ≤ 100 mm; German version EN 2127:1992 |
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DIN EN 2128 |
Aerospace series; aluminium alloy AL-P7075-T73511; drawn bars 6 mm ≤ a or D ≤ 75 mm; German version EN 2128:1992 |
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DIN EN 2130 |
Aerospace series - Bearings, precision ball in corrosion resisting steel for instruments and equipment - Technical specification; German version EN 2130:2001 |
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DIN EN 2131 |
Aerospace series - Plates in aluminium alloys, thickness 6 mm |
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DIN EN 2133 |
Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys; German version EN 2133:1997 |
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DIN EN 2134 |
Aerospace series - Round bars, extruded in aluminium and aluminium alloys, diameter 10 mm≤D≤220 mm - Dimensions; German and English version EN 2134:2001 |
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DIN EN 2143 |
Aerospace series; rivets, solid, universal head, in aluminium 1050A, inch based series; german version EN 2143:1992 |
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DIN EN 2144 |
Aerospace series - Rivets, solid, universal head, in aluminium alloy 2117, inch based series; German version EN 2144:1994 |
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DIN EN 2146 |
(DRAFT) Aerospace series - rivets, solid, universal head, in aluminium alloy 2017A - Inch based series |
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DIN EN 2146 |
Aerospace series; rivets, solid, universal head, in aluminium alloy 2017A, inch based series; german version EN 2146:1992 |
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DIN EN 2148 |
(DRAFT) Aerospace series - rivets, solid, universal head, in aluminium alloy 5056A - Inch based series |
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DIN EN 2148 |
Aerospace series; rivets, solid, universal head, in aluminium alloy 5056A, inch based series; german version EN 2148:1992 |
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DIN EN 2149 |
Aerospace series - Rivets, solid, universal head, in aluminium alloy 5056A, anodised or chromated, inch based series; German version EN 2149:1996 |
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DIN EN 2155-12 |
Aerospace series - Test methods for transparent materials for aircraft glazing - Part 12: Determination of linear thermal expansion; German version EN 2155-12:1997 |
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DIN EN 2155-19 |
Aerospace series - Test methods for transparent materials for aircraft glazing - Part 19: Determination of crace resistance; German version EN 2155-19:1996 |
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DIN EN 2155-22 |
(DRAFT) Aerospace series - Test methods for transparent materials for aircraft glazing - Part 22: Determination of thermal relaxation of stretched acrylic sheet |
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DIN EN 2155-4 |
(DRAFT) Aerospace series - Test methods for transparent materials for aircraft glazing - Part 4: Determination of ultraviolet light transmission over the wavelength range 280 nm to 360 nm |
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DIN EN 2155-6 |
(DRAFT) Aerospace series - Test methods for transparent materials for aircraft glazing - Part 6: Determination of optical defects |
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DIN EN 2155-7 |
Aerospace series - Test methods for transparent materials for aircraft glazing - Part 7: Determination of optical deviation; German version EN 2155-7:1997 |
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DIN EN 2157-2 |
Aerospace series; steel; forging stock and forgings; technical specification; part 2: forging stock; German version EN 2157-2:1993 |
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DIN EN 2157-3 |
Aerospace series; steel; forging stock and forgings; technical specification; part 3: pre-production and production forgings; German version EN 2157-3:1993 |
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DIN EN 2161 |
(DRAFT) Aerospace series - Heat resisting alloy CO-CH1401 (CoCr26Ni11W), not heat treated - Precision castings |
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DIN EN 2167 |
(DRAFT) Aerospace series - Heat resisting steel FE-PA 91-HT, solution treated; bars - Inactive for new design |
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DIN EN 2169 |
(DRAFT) Aerospace series - Heat resisting steel FE-PA91-HT, solution treated - Bars and sections for welded rings; inactive for new design |
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DIN EN 2174 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15), solution treated and precipitation treated - Hand and die forgings De ≤ 100 mm, Rm ≥ 850 MPa |
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DIN EN 2175 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15), solution treated and precipitation treated - Sheet, strip and plate 0,5 mm ≤ a ≤ 10 mm, Rm ≥ 850 MPa |
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DIN EN 2177 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2501 (X4NiCrMoTi43-13), solution treated and precipitation treated - Forgings De ≤ 100 mm |
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DIN EN 2183 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9), solution treated - Hand and die forgings, De ≤ 200 mm |
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DIN EN 2184 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9), solution treated - Bar and section, De ≤ 200 mm |
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DIN EN 2185 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9), solution treated - Sheet, strip and plate, 0,2 mm ≤ a ≤ 10 mm |
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DIN EN 2197 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH1701 (NiCr15Co14A15Ti4Mo4), solution treated and precipitation treated - Hand and die forgings De ≤ 200 mm, Rm ≥ 1250 MPa |
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DIN EN 2199 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH1303 (NiCo20Cr20Mo5Ti2A1), solution treated and precipitation treated - Bar and section De ≤ 200 mm |
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DIN EN 2202 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH1303 (NiCo20Cr20Mo5Ti2Al), solution treated - Seamless tubes, D ≤ 50 mm, a ≤ 3 mm |
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DIN EN 2203 |
(DRAFT) Aerospace series - Hest resisting alloy NI-PH1303 (NiCo20Cr20Mo5Ti2A1), solution treated - Sheet, strip and plate 0,2 mm ≤ a ≤ 10 mm |
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DIN EN 2204 |
(DRAFT) Aerospace series - Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al), vacuum melted, solution treated and precipitation treated - Precision casting, De ≤ 50 mm |
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DIN EN 2233 |
(DRAFT) Aerospace series - Heat resisting alloy Ni-CD1701 (NiCo15Cr10Al6Ti5Mo3), vacuum melted, non heat treated - Precision casting, a or D ≤ 50 mm |
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DIN EN 2234 |
(DRAFT) Aerospace series - Cables, electrical, fire-resistant - Technical specification |
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DIN EN 2235 |
Aerospace series - Single and multicore electrical cables, screened and jacketed; German and English version EN 2235:2006 |
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DIN EN 2237 |
(DRAFT) Aerospace series - Heat resisting steel FE-PA91-HT, solution treated and precipitation treated - Bars and sections for welded rings; inactive for new design |
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DIN EN 2238 |
(DRAFT) Aerospace series - Heat resisting steel FE-PA 91-HT, solution treated and precipitation treated; bars - Inactive for new design |
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DIN EN 2240-001 |
(DRAFT) Aerospace series - Lamps incandescent - Part 001: Technical specification |
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DIN EN 2240-003 |
(DRAFT) Aerospace series - Lamps incandescent - Part 003: Lamp, code 44; product standard |
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DIN EN 2240-004 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 004: Lamp, code 47; product standard |
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DIN EN 2240-005 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 005: Lamp, code 73; product standard |
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DIN EN 2240-006 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 006: Lamp, code 73E; product standard |
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DIN EN 2240-007 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 007: Lamp, code 74; product standard |
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DIN EN 2240-008 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 008: Lamp, code 75; product standard |
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DIN EN 2240-009 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 009: Lamp, code 83; product standard |
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DIN EN 2240-010 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 010: Lamp, code 84; product standard |
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DIN EN 2240-011 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 011: Lamp, code 85; product standard |
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DIN EN 2240-012 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 012: Lamp, code 95; product standard |
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DIN EN 2240-013 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 013: Lamp, code 301; product standard |
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DIN EN 2240-014 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 014: Lamp, code 303; product standard |
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DIN EN 2240-015 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 015: Lamp, code 304; product standard |
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DIN EN 2240-017 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 017: Lamp, code 306; product standard |
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DIN EN 2240-018 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 018: Lamp, code 307; product standard |
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DIN EN 2240-019 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 019: Lamp, code 308; product standard |
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DIN EN 2240-020 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 020: Lamp, code 311; product standard |
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DIN EN 2240-021 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 021: Lamp, code 313; product standard |
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DIN EN 2240-022 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 022: Lamp, code 315; product standard |