|
DIN EN 4261 |
(DRAFT) Aerospace series - Metallic materials - Rules for drafting and presentation of test method standards |
|
DIN EN 4262 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20), as forged - Forging stock, a or D ≤ 200 mm, 690 MPa ≤ Rm ≤ 880 MPa |
|
DIN EN 4263 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20), as forged - Forging stock, a or D ≤ 200 mm, 690 MPa ≤ Rm ≤ 960 MPa |
|
DIN EN 4264 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2501 (X4NiCrMoTi43-13), as forged - Forging stock, a or D ≤ 200 mm |
|
DIN EN 4265 |
(DRAFT) Aerospace series - Bearings, spherical plain, in corrosion resisting steel; wide series - Dimensions and loads; inch series |
|
DIN EN 4266 |
(DRAFT) Aerospace series - Bearings, spherical plain, in corrosion resisting steel, cadmium plated; wide series - Dimensions and loads; inch series |
|
DIN EN 4267 |
Aerospace series - Round bars in titanium and titanium alloys - Diameter 6 mm ≤ D ≤ 160 mm; Dimensions; German and English version EN 4267:2001 |
|
DIN EN 4269 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, floating, two lug, reduced series, with counterbore, in steel, cadmium plated, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4272 |
(DRAFT) Aerospace series - Aluminium alloy AL-P2219-T854 - Die forgings a ≤ 200 mm |
|
DIN EN 4273 |
(DRAFT) Aerospace series - Aluminium alloy AL-P6082-T6511 - Extruded bars and sections a or D ≤ 200 mm |
|
DIN EN 4274 |
(DRAFT) Aerospace series - Aluminium alloy AL-P6082-T6511 - Extruded bars and sections a or D ≤ 200 mm with peripheral coarse grain control |
|
DIN EN 4275 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7075-T76511 - Extruded bars and sections a or D ≤ 100 mm with peripheral coarse grain control |
|
DIN EN 4276 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7175-T7351 - Hand forgings a ≤ 150 mm |
|
DIN EN 4277 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7175-T73 - Hand and die forgings a ≤ 125 mm |
|
DIN EN 4278 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7175-T7352 - Hand and die forgings a ≤ 150 mm |
|
DIN EN 4282 |
(DRAFT) Aerospace series - Aluminium alloy AL-P2219-T37 - Plate 6 mm < a ≤ 40 mm |
|
DIN EN 4283 |
Aerospace series - Aluminium alloy AL-P2219-T87 - Plate - 6 mm < a ≤ 40 mm; German and English version EN 4283:2005 |
|
DIN EN 4284 |
(DRAFT) Aerospace series - Aluminium alloy AL-P2219-T852 - Forgings a ≤ 400 mm |
|
DIN EN 4285 |
(DRAFT) Aerospace series - Aluminium alloy AL-P2219-T851 - Forgings a ≤ 400 mm |
|
DIN EN 4286 |
Aerospace series - Aluminium alloy AL-P8090-T89 - Die forgings - a ≤ 125 mm; German and English version EN 4286:2005 |
|
DIN EN 4287 |
Aerospace series - Aluminium alloy AL-P7010 - Forging stock; German and English version EN 4287:2005 |
|
DIN EN 4288 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7050 - Forging stock |
|
DIN EN 4289 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7175 - Forging stock |
|
DIN EN 4290 |
(DRAFT) Aerospace series - Aluminium alloy AL-P2219 - Forging stock |
|
DIN EN 4291 |
Aerospace series - Aluminium alloy AL-P8090 - Forging stock; German and English version EN 4291:2005 |
|
DIN EN 4292 |
Aerospace series - Aluminium alloy AL-R39002 - Forging stock; German and English version EN 4292:2005 |
|
DIN EN 4293 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7175-T73511 - Extruded bars and sections a or D ≤ 150 mm |
|
DIN EN 4294 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7175-T7354 - Die forgings a ≤ 150 mm |
|
DIN EN 4297 |
(DRAFT) Aerospace series - Nuts, hexagonal, self-locking by plastic ring, normal height, normal across flats, in corrosion resisting steel, passivated; classification: 900 MPa (at ambient temperature)/120 °C |
|
DIN EN 4300 |
(DRAFT) Aerospace series - Identification marking of engine items - Design standard |
|
DIN EN 4301 |
(DRAFT) Aerospace series - Identification marking methods for engine items - Engineering requirements |
|
DIN EN 4302 |
(DRAFT) Aerospace series - Open ring insert tool, square drive |
|
DIN EN 4303 |
Aerospace series - Sleeves, tubular, for tension screws with flush head, in corrosion resisting steel, passivated, (0,25 mm wall thickness); German and English version EN 4303:2005 |
|
DIN EN 4304 |
(DRAFT) Aerospace series - Sleeves, tubular, for shear screws with flush head, in corrosion resisting steel, passivated (0,25 mm wall thickness) |
|
DIN EN 4304 |
Aerospace series - Sleeves, tubular, for shear screws with flush head, in corrosion resisting steel, passivated, (0,25 mm wall thickness); German and English version EN 4304:2005 |
|
DIN EN 4306 |
(DRAFT) Aerospace series - Sleeves, tubular, for tension screws with flush head, in corrosion resisting steel, passivated (0,50 mm wall thickness) |
|
DIN EN 4306 |
Aerospace series - Sleeves, tubular, for tension screws with flush head, in corrosion resisting steel, passivated, (0,50 mm wall thickness); German and English version EN 4306:2005 |
|
DIN EN 4307 |
(DRAFT) Aerospace series - Sleeves, tubular, for shear screws with flush head, in corrosion resisting steel, passivated (0,50 mm wall thickness) |
|
DIN EN 4307 |
Aerospace series - Sleeves, tubular, for shear screws with flush head, in corrosion resisting steel, passivated, (0,50 mm wall thickness); German and English version EN 4307:2005 |
|
DIN EN 4309 |
(DRAFT) Aerospace series - Nuts, hexagon, self-locking by plastic ring, normal height, normal across flats, in alloy steel, cadmium plated; classification: 900 MPa (at ambient temperature)/120 °C |
|
DIN EN 4311 |
Aerospace series - Studs, coarse tolerance reduced shank, medium length threads, in heat and corrosion resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature) / 315 °C; German and English version EN 4311:2006 |
|
DIN EN 4312 |
(DRAFT) Aerospace series - Studs, coarse tolerance reduced shank, medium length threads, in heat and corrosion resisting steel, with aluminium pigmented coating - Classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 4312 |
Aerospace series - Studs, coarse tolerance reduced shank, medium length thread, in heat and corrosion resisting steel, with aluminium pigmented coating - Classification: 1 100 MPa (at ambient temperature)/315 °C; German and English version EN 4312:2006 |
|
DIN EN 4313 |
Aerospace series - Aluminium alloy AL-P6013-T6 - Sheet and strip - 0,5 mm ≤ a ≤ 6 mm; German and English version EN 4313:2005 |
|
DIN EN 4314 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15), non heat treated - Forging stock, a or D ≤ 250 mm |
|
DIN EN 4315 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15), solution treated and precipitation treated - Bar and section a or D ≤ 100 mm, Rm ≥ 900 MPa |
|
DIN EN 4317 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15), non heat treated - Forging stock, a or D ≤ 200 mm |
|
DIN EN 4318 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) solution treated and precipitation treated - Bar and section De ≤ 100 mm, Rm ≥ 960 MPa |
|
DIN EN 4321 |
Aerospace series - Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1550 MPa (at ambient temperature)/650 °C; German and English version EN 4321:2004 |
|
DIN EN 4322 |
Aerospace series - Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated - Strength class: 1100 MPa (at ambient temperature): German and English version EN 4322:2004 |
|
DIN EN 4323 |
Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature)/350 °C; German and English version EN 4323:2004 |
|
DIN EN 4324 |
Aerospace series - Aluminium alloy AL-W42201 - Filler metal for welding; Rod; German and English version EN 4324:2001 |
|
DIN EN 4325 |
Aerospace series - Heat resisting alloy NI-WH1302 (NiCr20Co13Mo4Ti3Al) - Filler metal for welding; Wire and rod; German version EN 4325:2001 |
|
DIN EN 4326 |
Aerospace series - Heat resisting alloy CO-WH4102 (CoCr28W20Ni5V1) - Filler metal for welding; Wire and rod; German version EN 4326:2001 |
|
DIN EN 4327 |
Aerospace series - Heat resisting alloy CO-WH1401 (CoCr26Ni11W8) - Filler metal for welding; Wire and rod; German version EN 4327:2001 |
|
DIN EN 4328 |
Aerospace series - Steel FE-WM1601 (X18CrWNi13-3-2) - Filler metal for welding; Wire and rod; German version EN 4328:2002 |
|
DIN EN 4329 |
Aerospace series - Heat resisting alloy NI-WH0001 (NiCr20) - Filler metal for welding; Wire and rod; German version EN 4329:2001 |
|
DIN EN 4331 |
Aerospace series - Steel FE-WL1804 (25CrMnMo4-2-2) - Filler metal for welding; Wire and rod; German version EN 4331:2002 |
|
DIN EN 4332 |
Aerospace series - Steel FE-WL1805 (8CrMnMo12-4-9) - Filler metal for welding; Wire and rod; German version EN 4332:2002 |
|
DIN EN 4333 |
Aerospace series - Steel FE-WA4902 (X5CrNiCoMoWMn21-20-20-3-3-2) - Filler metal for welding; Wire and rod; German version EN 4333:2002 |
|
DIN EN 4334 |
Aerospace series - Steel FE-WL1806 (15CrMnMoV5-4-9-3) - Filler metal for welding; Wire and rod; German version EN 4334:2002 |
|
DIN EN 4335 |
Aerospace series - Steel FE-WA2602 (X4NiCrTiMoV26-15) - Filler metal for welding; Wire and rod; German version EN 4335:2002 |
|
DIN EN 4336 |
Aerospace series - Steel FE-WA3801 (X4CrNiMn20-10-2) - Filler metal for welding; Wire and rod; German version EN 4336:2002 |
|
DIN EN 4337 |
Aerospace series - Heat resisting alloy NI-WH8901 (NiCr16Ti3Mn2) - Filler metal for welding; Wire and rod; German version EN 4337:2001 |
|
DIN EN 4338 |
Aerospace series - Heat resisting alloy NI-WH3902 (NiCr25Mo10C) - Filler metal for welding; Wire and rod; German version EN 4338:2001 |
|
DIN EN 4339 |
Aerospace series - Heat resisting alloy CO-WH4002 (CoCr29W9) - Filler metal for welding; Wire and rod; German version EN 4339:2001 |
|
DIN EN 4341 |
Aerospace series - Aluminium alloy AL-W46431 - Filler metal for welding; Wire and rod; German version EN 4341:2001 |
|
DIN EN 4342 |
Aerospace series - Titanium TI-W99001 - Filler metal for welding; Wire and rod; German version EN 4342:2001 |
|
DIN EN 4343 |
Aerospace series - Steel FE-WM1001 (X13Cr12) - Filler metal for welding; Wire and rod; German version EN 4343:2002 |
|
DIN EN 4344 |
Aerospace series - Steel FE-WM1002 (X13Cr13) - Filler metal for welding; Wire and rod; German version EN 4344:2001 |
|
DIN EN 4346 |
(DRAFT) Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted, softened - Forging stock a or D ≤ 300 mm |
|
DIN EN 4347 |
(DRAFT) Aerospace series - Steel FE-PM1506 (X3CrNiMoAl13-8-2) vacuum induction melted and consumable electrode remelted, softened - Forgings stock a or D ≤ 300 mm |
|
DIN EN 4351 |
(DRAFT) Aerospace series - Rod ends, with self-aligning double row ball bearings and threaded shank in corrosion resisting steel - Dimensions and loads; inch series |
|
DIN EN 4352 |
Aerospace series - Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated - Classification: 1550 MPa (at ambient temperature) /425 °C; German and English version EN 4352:2004 |
|
DIN EN 4354 |
(DRAFT) Aerospace series - Six lobe recess - Drivers, relieved |
|
DIN EN 4355 |
(DRAFT) Aerospace series - Six lobe recess - Drivers, socket |
|
DIN EN 4356 |
(DRAFT) Aerospace series - Six lobe recess - Drivers, short |
|
DIN EN 4357 |
(DRAFT) Aerospace series - Six lobe recess - Drivers, handle |
|
DIN EN 4358 |
(DRAFT) Aerospace series - Six lobe recess - Drivers, double ended, 90° |
|
DIN EN 4359 |
(DRAFT) Aerospace series - Six lobe recess - Drivers; technical specification |
|
DIN EN 4360 |
(DRAFT) Aerospace series - Rivets, solid, 100° countersunk reduced head with dome, in aluminium alloy 7050, anodized or chromated - Metric series |
|
DIN EN 4361 |
(DRAFT) Aerospace series - Rivets, solid, 100° countersunk reduced head with dome, in aluminium alloy 5056A, anodized or chromated - Metric series |
|
DIN EN 4362 |
(DRAFT) Aerospace series - Rivets solid, 100° countersunk reduced head, in titanium alloy Ti 44,5 Cb, metric series |
|
DIN EN 4363 |
(DRAFT) Aerospace series - Rivets solid, 100° countersunk reduced head, in titanium alloy Ti 44,5 Cb, with aluminium pigmented coating, metric series |
|
DIN EN 4364 |
(DRAFT) Aerospace series - Cast acrylic - Properties |
|
DIN EN 4365 |
(DRAFT) Aerospace series - Heat and crazing resistant cast acrylic, crosslinked, and low moisture absorption - Properties |
|
DIN EN 4366 |
(DRAFT) Aerospace series - Heat and crazing resistant cast acrylic, crosslinked, multi-axially stretched, and low moisture absorption - Properties |
|
DIN EN 4367 |
(DRAFT) Aerospace series - Cast acrylic sheets - Dimensions |
|
DIN EN 4368 |
(DRAFT) Aerospace series - Heat resisting alloy NI-CD1701 (NiCo15Cr10Al6Ti5Mo3) non heat treated - Remelting stock |
|
DIN EN 4369 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH1701 (NiCr15Co14Al5Ti4Mo4) solution treated and precipitation treated - Bar and section, De ≤ 100 mm |
|
DIN EN 4370 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH1701 (NiCr15Co14Al5Ti4Mo4) non heat treated - Forging stock, a or D ≤ 100 mm |
|
DIN EN 4371 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PD9001 (NiCu31) non heat treated - Bar for rivets, D ≤ 10 mm |
|
DIN EN 4372 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PD9001 (NiCu31) non heat treated - Wire for rivets, D ≤ 10 mm |
|
DIN EN 4373 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PD9001 (NiCu31) annealed - Seamless tube, D ≤ 75 mm, a ≤ 3 mm |
|
DIN EN 4374 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3) solution treated and precipitation treated - Bar and section, De ≤ 200 mm |
|
DIN EN 4375 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3) non heat treated - Forging stock, a or D ≤ 250 mm |
|
DIN EN 4376 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) solution treated and precipitation treated - Bar and section, De ≤ 200 mm |
|
DIN EN 4377 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) non heat treated - Forging stock, a or D ≤ 300 mm |
|
DIN EN 4378 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) solution treated and precipitation treated - Wire for rivets, D ≤ 1,6 mm |
|
DIN EN 4379 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) solution treated - Forging, De ≤ 200 mm |
|
DIN EN 4380 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) solution treated - Bar and section, De ≤ 200 mm |
|
DIN EN 4381 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) solution treated - Seamless tubes for structured application, D ≤ 50 mm, a ≤ 3 mm |
|
DIN EN 4382 |
Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated - Seamless tubes - For hydraulic application - D =50 mm, a =3 mm; German and English version EN 4382:2006 |
|
DIN EN 4383 |
Aerospace series - Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3) - Non heat treated - Remelting stock; German and English version EN 4383:2006 |
|
DIN EN 4384 |
(DRAFT) Aerospace series - Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al) non heat treated - Remelting stock |
|
DIN EN 4385 |
(DRAFT) Aerospace series - Non-metallic materials - General organisation of standardization; Links between types of standards |
|
DIN EN 4386 |
(DRAFT) Aerospace series - Non-metallic materials - Rules for the drafting and presentation of test method standards |
|
DIN EN 4387 |
(DRAFT) Aerospace series - Non-metallic materials - Rules for drafting and presentation of technical specifications |
|
DIN EN 4390 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, floating, self-aligning, two lug, in heat resisting steel, silver plated - Classification: 900 MPa (at ambient temperature)/425 °C |
|
DIN EN 4396 |
(DRAFT) Aerospace series - Shaft-nuts, self-locking, in heat resisting steel FE-PA92HT (A286), silver plated |
|
DIN EN 4399 |
(DRAFT) Aerospace series - Rings, threaded, self-locking, in heat resisting steel FE-PA92HT (A286), silver plated |
|
DIN EN 4401 |
Aerospace series - Lockbolts, protruding head, sheartype, close tolerance, in titanium alloy TI-P64001, with aluminium pigmented coating, metric series - Classification: 1100 MPa (at ambient temperature) / 315 °C; German and English version EN 4401:2006 |
|
DIN EN 4402 |
(DRAFT) Aerospace series - Lockbolts, 100° countersunk normal head, sheartype, close tolerance, in titanium alloy TI-P64001, with aluminium pigmented coating, metric series - Classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 4402 |
Aerospace series - Lockbolts, 100° countersunk normal head, sheartype, close tolerance, in titanium alloy TI-P64001, with aluminium pigmented coating, metric series - Classification: 1100 MPa (at ambient temperature)/315 °C; German and English version EN 4402:2006 |
|
DIN EN 4403 |
(DRAFT) Aerospace series - Rivets, solid, 100° countersunk normal head, in titanium alloy Ti 44,5 Cb, with aluminium pigmented coating, metric series |
|
DIN EN 4404 |
(DRAFT) Aerospace series - Rivets, solid, universal head, in titanium alloy Ti 44,5 Cb, with aluminium pigmented coating, metric series |
|
DIN EN 4406 |
Aerospace series - Paints and varnishes - Two component cold curing polyurethane coating - Abrasion resistant; German and English version EN 4406:2006 |
|
DIN EN 4407 |
(DRAFT) Aerospace series - Bolts, normal hexagonal head, threaded to head, in titanium alloy, aluminium IVD coated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4408-001 |
Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 1: General rules; German and English version EN 4408-001:2005 |
|
DIN EN 4408-002 |
Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 2: Laminated parts; German and English version EN 4408-002:2005 |
|
DIN EN 4408-003 |
Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 3: Parts including core materials; German and English version EN 4408-003:2005 |
|
DIN EN 4408-004 |
Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 4: Items obtained by winding; German and English version EN 4408-004:2005 |
|
DIN EN 4408-005 |
Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 5: Seams; German and English version EN 4408-005:2005 |
|
DIN EN 4408-006 |
Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 6: Preforms; German and English version EN 4408-006:2005 |
|
DIN EN 4409 |
(DRAFT) Aerospace series - Square bars, extruded in aluminium and aluminium alloys - Thickness 6 mm ≤ a ≤ 200 mm; dimensions |
|
DIN EN 4410 |
(DRAFT) Aerospace series - Rectangular bars, extruded in aluminium and aluminium alloys - Thickness 6 mm ≤ a ≤ 160 mm; dimensions |
|
DIN EN 4411 |
(DRAFT) Aerospace series - Sheets, cold rolled, in steel - Thickness 0,5 mm ≤ a ≤ 3,0 mm; dimensions |
|
DIN EN 4419 |
(DRAFT) Aerospace series - Washers, chamfered, with counterbore, in alloy steel, cadmium plated |
|
DIN EN 4420 |
Aerospace series - Clips, spring tension, in alloy steel FE-PA3903; German and English version EN 4420:2003 |
|
DIN EN 4421 |
(DRAFT) Aerospace series - Studs in titanum alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel; strength class: 1100 MPa (at ambient temperature) |
|
DIN EN 4424 |
Aerospace series - Rod-ends, adjustable, single fork and threaded shank with engagement: 1,5 × thread diameter in titanium alloys - Dimensions and loads; German and English version EN 4424:2006 |
|
DIN EN 4425 |
Aerospace series - Washers, tab in corrosion resisting steel for flight control rods - Dimensions; German and English version EN 4425:2006 |
|
DIN EN 4434 |
Aerospace series - Copper or copper alloy lightweight conductors for electrical cables - Product standard (Normal and tight tolerances); German and English version EN 4434:2005 |
|
DIN EN 4435 |
(DRAFT) Aerospace series - Rivets, solid, 100° countersunk normal head, in heat resisting nickel base alloy NI-PH2301 (Hastelloy X), inch based series |
|
DIN EN 4437 |
(DRAFT) Aerospace series - Metallic materials - Test method; salt spray testing |
|
DIN EN 4438 |
(DRAFT) Aerospace series - Metallic materials - Test methods; linear thermal expansion of solid materials with a vitreous silica dilatometer |
|
DIN EN 4443 |
(DRAFT) Aerospace series - Nuts, elliptical clinch, self-locking, MJ threads; in heat resisting steel FE-PA2601 (A286), MoS2 coated; Classification: 900 MPa (at ambient temperature)/425 °C |
|
DIN EN 4444 |
(DRAFT) Aerospace series - Nuts, elliptical clinch, self-locking, in heat resisting steel FE-PA2601 (A286), MoS2 coated; Classification: 900 MPa (at ambient temperature)/425 °C - Technical specification |
|
DIN EN 4445 |
(DRAFT) Aerospace series - Nuts, elliptical clinch, self-locking - Design standard |
|
DIN EN 4446 |
(DRAFT) Aerospace series - Nuts, elliptical clinch, self-locking - Installation and removal procedure |
|
DIN EN 4447 |
(DRAFT) Aerospace series - Nuts, elliptical clinch, self-locking - UNJ threads, in heat resisting steel FE-PA2601 (A286), MoS2 coated; Classification: 900 MPa (at ambient temperature)/425 °C |
|
DIN EN 4448 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7050-T7452 - Die forgings a ≤ 150 mm |
|
DIN EN 4449 |
Aerospace series - Aluminium alloy AL-P7050-T76 - Sheet - 0,8 mm ≤ a ≤ 6 mm; German and English version EN 4449:2005 |
|
DIN EN 4450 |
Aerospace series - Aluminium alloy AL-P7050-T762 - Sheet - 0,8 mm ≤ a ≤ 6 mm; German and English version EN 4450:2005 |
|
DIN EN 4457 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7475-T7351 - Plate 6 mm < a ≤ 100 mm |
|
DIN EN 4458 |
Aerospace series - Studs, MJ threads, in titanium alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel - Strength class: 1100 MPa (at ambient temperature) - Technical specification; German and English version EN 4458:2005 |
|
DIN EN 4459 |
Aerospace series - Studs, in titanium alloy TI-P64001, with serrated locking ring in corrosion resisting steel - Design standard; German and English version EN 4459:2005 |
|
DIN EN 4460 |
Aerospace series - Studs, in titanium alloy TI-P64001, with serrated locking ring in corrosion resisting steel - Installation and removal procedure; German and English version EN 4460:2005 |
|
DIN EN 4461 |
(DRAFT) Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Bar a or D ≤ 150 mm, Rm ≥ 1200 MPa |
|
DIN EN 4462 |
(DRAFT) Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Bar a or D ≤ 150 mm, Rm ≥ 1300 MPa |
|
DIN EN 4463 |
(DRAFT) Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Bar a or D ≤ 150 mm, Rm ≥ 1400 MPa |
|
DIN EN 4464 |
(DRAFT) Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Forgings a or D ≤ 150 mm, Rm ≥ 1200 MPa |
|
DIN EN 4465 |
(DRAFT) Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Forgings a or D ≤ 150 mm, Rm ≥ 1300 MPa |
|
DIN EN 4466 |
(DRAFT) Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Forgings a or D ≤ 150 mm, Rm ≥ 1400 MPa |
|
DIN EN 4467 |
(DRAFT) Aerospace series - Steel FE-PM1505 (X1CrNiMoAl1Ti12-9-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Bar a or D ≤ 150 mm, Rm ≥ 1200 MPa |
|
DIN EN 4468 |
(DRAFT) Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Bar a or D ≤ 150 mm, Rm ≥ 1300 MPa |
|
DIN EN 4469 |
(DRAFT) Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Bar a or D ≤ 150 mm, Rm ≥ 1400 MPa |
|
DIN EN 4470 |
(DRAFT) Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Forgings a or D ≤ 150 mm, Rm ≥ 1200 MPa |
|
DIN EN 4471 |
(DRAFT) Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Forgings a or D ≤ 150 mm, Rm ≥ 1300 MPa |
|
DIN EN 4472 |
(DRAFT) Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Forgings a or D ≤ 150 mm, Rm ≥ 1400 MPa |
|
DIN EN 4473 |
(DRAFT) Aerospace series - Aluminium pigmented coatings - Technical specification |
|
DIN EN 4474 |
(DRAFT) Aerospace series - Aluminium pigmented coatings - Coating methods |
|
DIN EN 4486 |
(DRAFT) Aerospace series - Steel balls |
|
DIN EN 4493 |
(DRAFT) Aerospace series - Inserts, screw thread, helical coil, self-locking, in heat resisting nickel base alloy NI-PH1801 (NI-P96HT, Nimonic 90), silver plated |
|
DIN EN 4494 |
Aerospace series - Rings, split, in stainless steel; German and English version EN 4494:2006 |
|
DIN EN 4495 |
Aerospace series - Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating, metric series - Classification: 1 100 MPa (at ambient temperature)/315 °C; German and English version EN 4495:2006 |
|
DIN EN 4496 |
Aerospace series - Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating - Classification: 1100 MPa (at ambient temperature)/315 °C; German and English version EN 4496:2005 |
|
DIN EN 4496 Berichtigung 1 |
Aerospace series - Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating - Classification: 1100 MPa (at ambient temperature)/315 °C; German and English version EN 4496:2005, Corrigenda to DIN EN 4496:2006-08; German and English version EN 4496:2005/AC:2006 |
|
DIN EN 4497 |
(DRAFT) Aerospace series - Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating, Classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 4497 |
Aerospace series - Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating - Classification: 1 100 MPa (at ambient temperature)/315 °C; German and English version EN 4497:2005 |
|
DIN EN 4498 |
(DRAFT) Aerospace series - Bolts, large hexagonal head, close tolerance normal shank, medium length thread, in heat resisting nickel base alloy, passivated, with aluminium pigmented coating, Classification: 1550 MPa (at ambient temperature)/315 °C |
|
DIN EN 4498 |
Aerospace series - Bolts, large bihexagonal head, close tolerance normal shank, medium length thread, in heat resisting nickel base alloy, passivated, with aluminium pigmented coating, Classification: 1 550 MPa (at ambient temperature)/315 °C; German and English version EN 4498:2005 |
|
DIN EN 4499 |
(DRAFT) Aerospace series - Screws, 100° countersunk reduced head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating, Classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 4500-1 |
(DRAFT) Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 1: General rules |
|
DIN EN 4500-2 |
(DRAFT) Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 2: Specific rules for aluminium, aluminium alloys and magnesium alloys |
|
DIN EN 4500-3 |
(DRAFT) Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 3: Specific rules for heat resisting alloys |
|
DIN EN 4500-3/A1 |
(DRAFT) Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 3: Specific rules for heat resisting alloys |
|
DIN EN 4500-4 |
(DRAFT) Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 4: Specific rules for titanium and titanium alloys |
|
DIN EN 4500-5 |
(DRAFT) Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 5: Specific rules for steels |
|
DIN EN 4500-5/A1 |
(DRAFT) Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 5: Specific rules for steels |
|
DIN EN 4500-6 |
(DRAFT) Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 6: Specific rules for filler metals for brazing |
|
DIN EN 4501 |
Aerospace series - Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating, metric series - Classification: 1 100 MPa (at ambient temperature) / 315 °C; German and English version EN 4501:2006 |
|
DIN EN 4502 |
(DRAFT) Aerospace series - Washers, flat, for riveting in heat resisting steel FE-PA4901 (Multimet) - Inch based series |
|
DIN EN 4508 |
Aerospace series - Paints and varnishes - Test method for anti slip coatings - Determination of the sliding friction behaviour; German and English version EN 4508:2006 |
|
DIN EN 4509 |
Aerospace series - Screws, 100° countersunk normal head, offset cruciform recess, threaded to head, in titanium alloy, anodized, with aluminium pigmented coating, metric series - Classification: 1 100 MPa (at ambient temperature) / 315 °C; German and English version EN 4509:2006 |
|
DIN EN 4511 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH2301 (NiCr22FeMo), solution treated and cold worked - Wire for rivets 1,6 mm ≤ D ≤ 10 mm |
|
DIN EN 4522 |
(DRAFT) Aerospace series - Metallic materials - Test methods, pin-type bearing test of yield strength |
|
DIN EN 4523 |
(DRAFT) Aerospace series - Metallic materials - Test methods: compression testing |
|
DIN EN 4524 |
(DRAFT) Aerospace series - Metallic materials - Test methods; measurement of fatigue crack growth rates |
|
DIN EN 4525 |
(DRAFT) Aerospace series - Aluminium and aluminium alloys - Test methods; shear testing |
|
DIN EN 4526 |
(DRAFT) Aerospace series - Metallic materials - Test methods; sharp edge-notch tensile testing for sheet and strip |
|
DIN EN 4527 |
(DRAFT) Aerospace series - Aluminium and aluminium alloys; test methods - Determination susceptibility to stress-corrosion cracking |
|
DIN EN 4529-001 |
Aerospace series - Elements of electrical and optical connection - Sealing plugs - Part 001: Technical specification; German and English version EN 4529-001:2006 |
|
DIN EN 4529-002 |
Aerospace series - Elements of electrical and optical connection - Sealing plugs - Part 002: Index of product standards; German and English version EN 4529-002:2006 |
|
DIN EN 4545 |
(DRAFT) Aerospace series - Steel FE-PL1505 (15CrMoV6) air melted, hardened and tempered - Plate 20 mm ≤ a ≤ 50 mm, 1080 MPa ≤ Rm ≤ 1280 MPa |
|
DIN EN 4549 |
Aerospace series - Pipe coupling, in heat resisting steel or in heat resisting nickel alloy - Coupling end, welded - Design configuration - Inch series; German and English version EN 4549:2003 |
|
DIN EN 4550-1 |
Aerospace series - Pipe coupling 37° - Design configuration - Inch series - Part 1: Male sealing ends, spherical; German and English version EN 4550-1:2003 |
|
DIN EN 4550-2 |
Aerospace series - Pipe coupling 37° - Design confirguration - Inch series - Part 2: Port ends; German and English version EN 4550-2:2003 |
|
DIN EN 4550-3 |
Aerospace series - Pipe coupling 37° - Design configuration - Inch series - Part 3: Port connections; German and English version EN 4550-3:2003 |
|
DIN EN 4550-4 |
Aerospace series - Pipe coupling 37° - Design configuration - Inch series - Part 4: Female sealing ends; German and English version EN 4550-4:2003 |
|
DIN EN 4551 |
Aerospace series - Pipe couplings, 37°, in heat resisting steel - Swivel nuts - Inch series; German and English version EN 4551:2003 |
|
DIN EN 4552 |
Aerospace series - Pipe coupling, 37°, spherical, in heat resisting steel - Straight nipples, welded end - Inch series; German and English version EN 4552:2003 |
|
DIN EN 4553 |
Aerospace series - Pipe coupling 37°, spherical, in heat resisting steel - Elbow 90° nipples, welded end - Inch series; German and English version EN 4553:2003 |
|
DIN EN 4554 |
Aerospace series - Pipe coupling 37°, spherical, in heat resisting steel - Straight unions, threaded - Inch series; German and English version EN 4554:2003 |
|
DIN EN 4555 |
Aerospace series - Pipe coupling 37°, in heat resisting steel - Ferrules, welded end - Inch series; German and English version EN 4555:2003 |
|
DIN EN 4556 |
Aerospace series - Pipe coupling 37°, in heat resisting steel - Cap assemblies - Inch series; German and English version EN 4556:2003 |
|
DIN EN 4557 |
Aerospace series - Pipe couplings, 37°, spherical, in heat resisting steel - Tees nipples, welded end - Inch series; German and English version EN 4557:2003 |
|
DIN EN 4560 |
Aerospace series - Pipe coupling 37° spherical, up to 21000 kPa - Inch series - Technical specification; German and English version EN 4560:2003 |
|
DIN EN 4561 |
Aerospace series - Pipe coupling, welded, in heat resisting steel - Elbow 90° - Inch series; German and English version EN 4561:2003 |
|
DIN EN 4562 |
Aerospace series - Pipe coupling, welded, in heat resisting steel - Reductors - Inch series; German and English version EN 4562:2003 |
|
DIN EN 4563 |
Aerospace series - Pipe coupling, welded, in heat resisting steel - Tees - Inch series; German and English version EN 4563:2003 |
|
DIN EN 4566 |
(DRAFT) Aerospace series - Heat resisting alloy CO-PH4101 (CoCr20W15Ni), vacuum melted, solution treated - Forgings De ≤ 100 mm |
|
DIN EN 4567 |
(DRAFT) Aerospace series - Heat resisting alloy CO-PH4101 (CoCr20W15Ni), vacuum melted, solution treated - Bar and section a or D ≤ 100 mm |
|
DIN EN 4568 |
(DRAFT) Aerospace series - Heat resisting alloy CO-PH4101 (CoCr20W15Ni), vacuum melted, solution treated - Sheet and strip a ≤ 6 mm |
|
DIN EN 4569 |
(DRAFT) Aerospace series - Heat resisting alloy CO-PH4101 (CoCr20W15Ni), vacuum melted, solution treated - Wire D ≤ 4 mm |
|
DIN EN 4570 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20), solution treated - Forgings De ≤ 100 mm |
|
DIN EN 4571 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20), solution treated - Bar and section De ≤ 100 mm |
|
DIN EN 4572 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20), solution treated - Sheet and strip a ≤ 3 mm |
|
DIN EN 4573 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20), solution treated and precipitation treated - Bar and section De ≤ 100 mm |
|
DIN EN 4574 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20), solution treated and precipitation treated - Forgings De ≤ 100 mm |
|
DIN EN 4575 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20), solution treated and descaled - Sheet and plate 3 mm < a ≤ 50 mm |
|
DIN EN 4585 |
Aerospace series - Clips, spring tension - Technical specification; German and English version EN 4585:2003 |
|
DIN EN 4590 |
(DRAFT) Aerospace series - Retainers, spring, sheet metal, for self-locking barrel nuts, in corrosion resisting steel, passivated |
|
DIN EN 4590 |
Aerospace series - Retainers, spring, sheet metal, for self-locking barrel nuts, in corrosion resisting steel, passivated; German and English version EN 4590:2005 |
|
DIN EN 4591 |
(DRAFT) Aerospace series - Nuts, barrel, self-locking, floating, self-aligning, in heat resisting nickel base alloy, MoS2 lubricated; classification: 1550 MPa (at ambient temperature)/315 °C |
|
DIN EN 4591 |
Aerospace series - Nuts, barrel, self-locking, floating, self-aligning, in heat resisting nickel base alloy, MoS2 lubricated - Classification: 1550 MPa (at ambient temperature)/315 °C; German and English version EN 4591:2005 |
|
DIN EN 4603 |
(DRAFT) Aerospace series - Molybdenum disulphide coatings of fasteners - Technical specification |
|
DIN EN 4604-001 |
(DRAFT) Aerospace series - Cable, electrical, for signal transmission - Part 001: Technical specification |
|
DIN EN 4604-002 |
(DRAFT) Aerospace series - Cable, electrical, for signal transmission - Part 002: General |
|
DIN EN 4615 |
Aerospace series - Magnesium alloy MG-C18002 - T4 - Sand casting; German and English version EN 4615:2005 |
|
DIN EN 4616 |
Aerospace series - Magnesium alloy MG-C18002 - T4 - Chill casting; German and English version EN 4616:2005 |
|
DIN EN 6000 |
(DRAFT) Aerospace series - Auminium alloys AL-P2024-T351 - Plate 6,0 mm < a ≤ 55 mm, close-tolerance flatness |
|
DIN EN 6024 |
(DRAFT) Aerospace series - Screws 100° countersunk reduced head, offset cruciform recess, close tolerance shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C; inch series |
|
DIN EN 6025 |
(DRAFT) Aerospace series - Plates - Aluminium alloys 2024, tolerance flatness, thickness 6 mm < a ≤ 55 mm; dimensions |
|
DIN EN 6029 |
(DRAFT) Aerospace series - Rod-ends, adjustable, single fork with UNJ threaded shank, min. engagement: 1,5 × diamter in corrosion resisting steel - Dimensions and loads; inch series |
|
DIN EN 6039 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of the exothermic reaction during curing of prepreg material |
|
DIN EN 6044-1 |
(DRAFT) Aerospace series - Carbon fibre reinforced epoxy prepreg; technical specification - Part 1: General requirements |
|
DIN EN 6044-2 |
(DRAFT) Aerospace series - Carbon fibre reinforced epoxy prepreg; technical specification - Part 2: Qualification program/batch release testing; unidirectional tape, 180 °C curing class |
|
DIN EN 6046 |
(DRAFT) Aerospace series - bearings, spherical plain, in corrosion resisting steel; narrow series - Dimensions and loads; inch series |
|
DIN EN 6047-001 |
(DRAFT) Aerospace series - Connectors, electrical, circular, coupled by threaded ring, for high current, operating temperature + 200 °C continuous and fire resistant - Part 001: Technical specification |
|
DIN EN 6047-002 |
(DRAFT) Aerospace series - Connectors, electrical, circular, coupled by threaded ring, for high current, operating temperature + 200 °C continuous, and fire resistant - Part 002: Specification of performance and contact arrangements |
|
DIN EN 6047-003 |
(DRAFT) Aerospace series - Connectors, electrical, circular, coupled by threaded ring, for high current, operating temperature + 200 °C continuous, and fire resistant - Part 003: Square flange receptacle; Product standard |
|
DIN EN 6047-004 |
(DRAFT) Aerospace series - Connectors, electrical, circular, coupled by threaded ring, for high current, operating temperature + 200 °C continuous and fire resistant - Part 004: Plug; product standard |
|
DIN EN 6049-001 |
(DRAFT) Aerospace series - Electrical cables, installation; Protection sleeve in meta-aramid fibres - Part 001: Technical specification |
|
DIN EN 6049-003 |
(DRAFT) Aerospace series - Electrical cables, installation; protection sleeve in meta-aramid fibres - Part 003: Braided, tubular, expandable; product standard |
|
DIN EN 6049-004 |
(DRAFT) Aerospace series - Electrical cables, installation; protection sleeve in meta-aramid fibres - Part 004: Braided, tubular, high expandable; product standard |
|
DIN EN 6049-005 |
(DRAFT) Aerospace series - Electrical cables, installation; protection sleeve in meta-aramid fibres - Part 005: Sleeve flexible, post installation; product standard |
|
DIN EN 6049-006 |
(DRAFT) Aerospace series - Electrical cables, installation; Protection sleeve in meta-aramid fibres - Part 006: Self-wrapping protective sleeve, flexible post installation; Product standard |
|
DIN EN 6050 |
(DRAFT) Aerospace series - Pins, close tolerance, swage locking, 100° countersunk head reduced, shear type, in aluminium alloy 7050, chemical film - Inch series |
|
DIN EN 6051 |
(DRAFT) Aerospace series - Collars, swage locking, shear type, in aluminium alloy 3003, chemical film - Inch series |
|
DIN EN 6052 |
(DRAFT) Aerospace series - Rivets-Collar-System in aluminium alloy, shear type, inch series - Technical specification |
|
DIN EN 6054 |
(DRAFT) Aerospace series - Collars, swage locking, shear type, in aluminium alloy 6061, chemical film - Inch series |
|
DIN EN 6059-100 |
(DRAFT) Aerospace series - Electrical cables, installation; Protection sleeves; Test methods - Part 100: General |
|
DIN EN 6059-201 |
(DRAFT) Aerospace series - Electrical cables, installation, protection sleeves; test methods - Part 201: Visual inspection |
|
DIN EN 6059-202 |
(DRAFT) Aerospace series - Electrical cables, installation, protection sleeves; test methods - Part 202: Dimensions and mass |
|
DIN EN 6059-203 |
(DRAFT) Aerospace series - Electrical cables, installation, protection sleeves; test methods - Part 203: Coverage |
|
DIN EN 6059-301 |
(DRAFT) Aerospace series - Electrical cables, installation, protection sleeves; test methods - Part 301: Sun light exposure |
|
DIN EN 6059-302 |
(DRAFT) Aerospace series - Electrical cables, installation, protection sleeves; test methods - Part 302: High temperature exposure |
|
DIN EN 6059-303 |
(DRAFT) Aerospace series - Electrical cables, installation; Protection sleeves; Test methods - Part 303: Resistance to fluids |
|
DIN EN 6059-305 |
(DRAFT) Aerospace series - Electrical cables, installation, protection sleeves; test methods - Part 305: Fluid absorption |
|
DIN EN 6059-306 |
(DRAFT) Aerospace series - Electrical cables, installation, protection sleeves; test methods - Part 306: Mould growth |
|
DIN EN 6059-401 |
(DRAFT) Aerospace series - Electrical cables; installation; protection sleeves; test methods - Part 401: Expansion range |
|
DIN EN 6059-402 |
(DRAFT) Aerospace series - Electrical cables; installation; protection sleeves; test methods - Part 402: Bending properties |
|
DIN EN 6059-403 |
(DRAFT) Aerospace series - Electrical cables; installation; protection sleeves; test methods - Part 403: Scrape abrasion |
|
DIN EN 6059-404 |
(DRAFT) Aerospace series - Electrical cables; installation; protection sleeves; test methods - Part 404: Tensile strength |
|
DIN EN 6059-405 |
(DRAFT) Aerospace series - Electrical cables; installation; protection sleeves; test methods - Part 405: Dynamic cut-through |
|
DIN EN 6059-406 |
(DRAFT) Aerospace series - Electrical cables, installation; Protection sleeves; Test methods - Part 406: Vibration |
|
DIN EN 6063 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of material degradation due to chemical products |
|
DIN EN 6064 |
(DRAFT) Aerospace series - Non-metallic materials - Analysis of non-metallic materials (cured) for the determination of the extent of cure by Differential Scanning Calorimetry (DSC) |
|
DIN EN 6066 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of tensile strength of tapered and stepped joints |
|
DIN EN 6067 |
(DRAFT) Aerospace series - Pin, quick release, self-retaining, positive locking, double acting - Button handle |
|
DIN EN 6068 |
(DRAFT) Aerospace series - Pin, quick-release, self-retaining, positive locking, single acting - Button handle |
|
DIN EN 6070 |
(DRAFT) Aerospace series - Aluminium and aluminium alloy wrought products - Technical specification; general requirements |
|
DIN EN 6071 |
(DRAFT) Aerospace series - Aluminium and aluminium alloy wrought products - Technical specification; plate |
|
DIN EN 6073 |
(DRAFT) Aerospace series - Metallic materials; aluminium and aluminium alloys - Test methods, drop test |
|
DIN EN 6074 |
(DRAFT) Aerospace series - Metallic materials - Test methods; statistical data for material qualification |
|
DIN EN 6080 |
(DRAFT) Aerospace series - Rivet, 100° normal flush head, close tolerance - Inch series |
|
DIN EN 6081 |
(DRAFT) Aerospace series - Rivets, universal head - Inch based series |
|
DIN EN 6084 |
(DRAFT) Aerospace series - Non-metallic materials - Surfacing films; technical specification; general requirements |
|
DIN EN 6085 |
(DRAFT) Aerospace series - Non-metallic materials - Epoxy surfacing films |
|
DIN EN 6100 |
(DRAFT) Aerospace series - Pins, close tolerance, swage locking, 100° countersunk head, shear type, in aluminium alloy 7050, chemical film - Inch series |
|
DIN EN 6104 |
(DRAFT) Aerospace series - Rivets, solid, in aluminium or aluminium alloy; Inch series - Technical specification |
|
DIN EN 6110 |
(DRAFT) Aerospace series - Bolts, blind, 100° flush head, stainless steel |
|
DIN EN 7000-1 |
(DRAFT) Aerospace series - Non-metallic materials; rules for the drafting and presentation of material standards - Part 1: General rules |
|
DIN EN 7000-10 |
(DRAFT) Aerospace series - Non-metallic materials; rules for the drafting and presentation of material standards - Part 10: Reinforcement fibres |
|
DIN EN 7000-11 |
(DRAFT) Aerospace series - Non-metallic materials; rules for drafting and presentation of material standards - Part 11: Preimpregnates |
|
DIN EN 7000-6 |
(DRAFT) Aerospace series - Non-metallic materials; rules for the drafting and presentation of material standards - Part 6: Structural adhesive systems |
|
DIN EN 7000-8 |
(DRAFT) Aerospace series - Non-metallic materials - Rules for drafting and presentation of material standards - Part 8: Lightweight cores |
|
DIN EN 7000-9 |
(DRAFT) Aerospace series - Non-metallic materials; rules for the drafting and presentation of material standards - Part 9: Paints and varnishes |
|
DIN EN 7001 |
(DRAFT) Aerospace series - Process standards - Rules for the drafting and presentation of surface treatment standards |
|
DIN EN 9103 |
(DRAFT) Aerospace series - Quality management systems - Variation management of key characteristics |
|
DIN EN 9110 |
(DRAFT) Aerospace series - Quality systems - Model for quality assurance applicable to maintenance organizations; German and English version EN 9110:2005 |
|
DIN EN 9111 |
(DRAFT) Aerospace series - Quality systems - Quality system assessment applicable to maintenance organizations |
|
DIN EN 9121 |
(DRAFT) Aerospace series - Quality systems - Quality system assessment applicable to stockist distributors |
|
DIN EN 9133 |
Aerospace series - Quality management systems - Qualification procedure for aerospace standard parts; German and English version EN 9133:2004 |
|
DIN EN ISO 14620-1 |
Space systems - Safety requirements - Part 1: System safety (ISO 14620-1:2002); German and English version EN ISO 14620-1:2002 |
|
DIN EN ISO 16091 |
Space systems - Integrated logistic support (ISO 16091:2002); German and English version EN ISO 16091:2002 |
|
DIN EN ISO 21351 |
Space systems - Functional and technical specifications (ISO 21351:2005); German and English version EN ISO 21351:2005 |
|
DIN IEC 62239 |
(DRAFT) Process Management for Avionics - Technical specification for preparing an electronic components management plan (IEC 107/18/CD:2002) |
|
DIN IEC 62396 |
(DRAFT) Process management for avionics industry - Standard for the accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment (IEC 107/29/CD:2004) |