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TS EN 2070-3 Aerospace-Aluminum and aluminum alloys machined products-Technical specifications; Section 3: Rod and cross section
TS EN 2103-2 Aerospace series - Re-melting drafts and castings made of steel, nickel-based and cobalt-based alloys - Technical specifications - Part 2: Re-melting drafts
TS EN 2103-3 Aerospace series-Steel, nickel-based and cobalt-based alloy remelting drafts and castings-Technical specifications-Part 3: Pre-production and production castings
TS EN 4344 Aviation series - Steel fe-Wm1002 (x13cr13) - Filler metal for welding- Wire and rod
TS EN 2083 Aviation series - Copper and copper alloy conductors for electrical cables - Product standard
TS EN 3889 Aviation series - Fe-Wm 3801 (x5 crnicu17-4) steel - Filler metal for welding
TS EN 3890 Aviation series -Fe-Wm1502 (x11crnimovn12-3) -Filling metal for welding
TS EN 3896 Aviation series-Steel fe-Wm 1501 (x13-12-3-2-2-XNUMX) -Filling metal for welding
TS EN 3897 Aviation series-Fe-Wa4801 (x6crnimnnb18-10) filler metal for welding
TS EN 4328 Aviation series - Steel fe-Wm1601 (x18crwni13-3-2) - Filler metal for welding: Wire and rod
TS EN 4330 Aviation series - Steel fe-Wa 4802 (w8crnimn 27-22-2) -Fill metal for welding: Wire and rod
TS EN 4331 Aviation series-Steel fe-Wl 1804 (25 crmnmo 4-2-2) filler metal for welding-Wire and rod
TS EN 4332 Aerospace series - Steel fe-Wl1805 (8crmnmo12-4-9) - Filler metal for welding; Wire and rod
TS EN 4333 Aviation series - Steel fe-Wa 4902 (x5crnicomowmn 21-20-20-3-3-2) -Fill metal for welding-Wire and rod
TS EN 4335 Aviation series - Steel fe-Wa2602 (x4nicrtimov26-15) - Filler metal for welding, wire and rod
TS EN 4336 Aviation series-Steel fe-Wa 3801 (xNUMX-4-20-10-2) - Full metal, wire and rod for welding
TS EN 4343 Aviation series - Steel fe-Wm 1001 (x13cr12) - Welding filler metal - Wire and rod
TS EN 2821 Aerospace series - Steel fe-Pm18021 (x5crnicu15-5) - Re-melted consumable electrodes - Chemically treated and precipitated - Rod to remove sawdust - Diameter or thickness of 200 mm or greater - Rm 1310 mpa or bigger
TS EN 3490 Aviation series - Steel fe-Pm3901 (x15crni17-3) - Air melted - Hardened and tempered - Rod for chip removal - De? 200 mm - 900 MPa? Rm? 1 100 is MPa
TS EN 3638 Aerospace series - Heat-resistant alloy FE-PA2601 (X6NiCrTiMoV26-15) - Re-melted consumable electrode - Chemical and precipitated - Plate, strip and plate - 0,5 mm? a? 10 mm
TS EN 3677 Aerospace series - Steel fe-Pm3801 (x5crnicu17-4) - Chemical and precipitated - Melted in air - Forged materials - a or D? 200 mm - Rm? 1 310 MPa
TS EN 3678 Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Melted in air - Chemical and precipitated - Forged materials - Thickness or diameter equal to or greater than 200 mm and Rm equal to or greater than 930 MPa one
TS EN 2467 Aviation series - FE-PA3901 Steel (X2CrNi18-9) - Air-melted - Softened - Sheets, sheets and strip - 0,4 mm? a? 20 mm - 520 MPa? Rm? 670 MPa
TS EN 2573 Aviation series - Steel fe-Pa3901 (x6crniti18-10) - Soft - Tensile stress -Rm? 780 is MPa - Diameter of 0,25 mm? Also ? Wires with 3 mm
TS EN 3162 Aviation series - Steel fe-Pm3801 (x5crnicu17-4) - Air-melted, chemically treated and precipitated sheet and strip - a? 6 mm, Rm? 930 is MPa
TS EN 3365 Aviation series - Steel fe-Pm3901 (x15CrNi17-3) - Reinforced, softened, forged block, thickness or diameter a or D? 300 is mm
TS EN 3488 Aviation series - Steel fe-Pa3601 (X6CrNiTi18-10) - Air melted - Softened - Sheet and strip - Thickness a? 6 mm - 500 MPa? Rm? 700 MPa
TS EN 4098 Aviation series - Steel fe-Pl1507 (40CrMoV12) - Re-melted, hardened and tempered, forging - Diameter De? 50 mm, 1250 MPa? Rm? 1400 MPa
TS EN 4216 Aviation series - Steel fe-Cm3801 (gx5crnicunb16-4) - Homogenized, treated with chemical solution and hardened with precipitation, precision casting - Diameter <50 mm and rm <900 mpa
TS EN 4346 Aviation series - Çelikfe-Pm1505 (x1crnimoalti12-9-2) - Melted with vacuum induction and remelted using consumable electrode, softened, thickness or diameter a or d <300 mm
TS EN 4461 Aviation series - Steel fe-Pm1506 (x1crnimoalti13-8-2) - Melted by vacuum induction and remelted using consumable electrode - Treated with chemical solution and treated with precipitation - Rods - Thickness or diameter a or d < 150 mm - Rm <1200 MPa
TS EN 4465 Aviation series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Melted with vacuum induction and remelted using consumable electrodes - Treated with chemical solution and treated with precipitation - Forgings - Thickness or diameter a or D < 150 mm - Rm <1300 MPa
TS EN 4467 Aviation series - Steel fe-Pm1505 (x1crnimoalti12-9-2) - Melted with vacuum induction and remelted using consumable electrode - Treated with chemical solution and treated with precipitation - Rods - Thickness or diameter a or d < 150 mm - Rm <1200 mpa
TS EN 4468 Aviation series - Steel fe-Pm1505 (X1CrNiMoAlTi12-9-2) - Melted by vacuum induction and remelted using consumable electrode - Treated with chemical solution and treated with precipitation - Rods - Thickness or diameter a or D < 150 mm - Rm <1300 MPa
TS EN 4470 Aviation series - Steel fe-Pm1505 (x1crnimoalti12-9-2) - Melted by vacuum induction and re-melted using consumable electrot - Treated with chemical solution and treated with precipitate - Tattoos - Thickness or diameter a or D? 150 mm - Rm? 1 200 is MPa
TS EN 4471 Aerospace series - Steel fe-Pm1505 (X1CrNiMoAlTi12-9-2) - Melted by vacuum induction and re-melted using consumable electrot - Treated with chemical solution and treated with precipitate - Tattoos - Thickness or diameter a or D? 150 mm - Rm? 1 300 is MPa
TS EN 2465 Aviation series -Steel fe-Pa3901 (x2crni18-9) -Soft - With tensile stress 450 mpa <rm <680 mpa - Diameter 0,4 mm <d <100 mm
TS EN 2460 Aviation series - Steel fe-Pm1901 (x12crni13) - 600 MPa? Rm? 800 MPa - Bars - De? 70 mm
TS EN 2461 Aviation series - Steel fe-Pm1901 (x12crni13) - 600 mpa <rm <800 mpa - Forgings - De <70 mm
TS EN 2466 Aviation series - Steel fe-Pa3901 (x2crni19-11) - Softened - Forging - De? 100 mm
TS EN 2818 Aviation series - Steel fe-Pm1802 (x5crnicu15-5) - Re-melted using consumable electrodes - Treated with chemical solution and treated with precipitate - Forging - A or D? 200 mm - Rm? 1 070 MPa
TS EN 3330 Aviation series - Steel fe-Pl1503 (35crmo4) - Annealed - Rod and wire - De? 40 mm - for the largest torque nuts
TS EN 4528 Aviation series - Steel fe-Pa3903 (x10crni18-8) - Cold rolled - Strips for springs - A <3 mm - 1250 mpa <rm <1640 mpa
TS EN 4642 Aviation series - Steel fe-Pm 3504 (x4CrNiMo16-5-1) - Melted using air - Hardened and tempered - Sheet and plate - 0,6 mm? a? 50 mm - 900 mpa? Rm? 1050 mpa
TS EN 3529 Aerospace series - Steel fe-Pm2701 (x2nicomo18-8-5) - Melted in vacuum and re-melted with vacuum arc- Forged with chemical solution and precipitate- A or d? 150 mm - 750 mpa? rm? 2000 mpa
TS EN 4700-007 Aerospace series - Steel and heat resistant alloys - Formed products - Technical specifications - Part 004: Wire
TS EN 4700-004 Aerospace series - Steel and heat resistant alloys - Formed products - Technical specifications - Part 007: Re-melted draft
TS EN 4657 Aviation series - Steel fe-Pm1507 (x1crnimoalti12-11-2) - Melted in vacuum and remelted using consumable electrode - Chemically treated and precipitation - Rods - A or <200 mm - Rm> 1650 mpa
TS EN 4700-002: 2010 Aerospace series - Steel and heat resistant alloys - Formed products - Technical specifications - Part 002: Rod and profile
TS EN 4655 Aviation series - Steel fe-Pm1506 (x1crnimoalti12-10-2) - Melted in vacuum and re-melted using consumable eletrot- Chemically treated and precipitated - Rods - A or d = 200 mm - Rm = 1 400 m
TS EN 4700-001 Aerospace series - Steel and heat resistant alloys - Formed products - Technical specifications - Part 001: Sheet, sheet and strip
TS EN 4656 Aerospace series - Steel fe-Pm1507 (x1crnimoalti12-11-2) -Melted in vacuum and re-melted using a consumable electrode- Chemical and precipitated rods - A or d = 200 mm - Rm = 1520 mpa
TS EN 4659 Aerospace series - Steel fe-Pm1507 (x1crnimoalti12-11-2) -Melted in vacuum and re-melted using consumable eletrot- Chemical and precipitated process- Forging - a or D = 200 mm - Rm = 1650 mpa
TS EN 4672 Aviation series - Steel fe-Pm1504 (x1crnimoalti12-10-2) - Melted by vacuum induction and re-melted using consumable electrot- Softened-Forged draft - A or d? 300 mm
TS EN 4683 Aviation series-Steel fe-Wm 3504 (x4crnimo16-5-1) -High-softened -Filling metal for welding-Wire and rod
TS EN 2252 Aviation series - Steel fe-PL1505 (15crmov6) - 1 080 mpa? 1250 mpa - Pounded - De? 100 mm
TS EN 3351 Aviation series - Titanium alloy ti-4al-4mo-2sn - Solution treated and aged - Forgings - D e <= 150 mm
TS EN 4268 Aviation series - Metallic materials - Heat treatment plants - General rules
TS EN 4500-001 Aerospace series - Metallic materials - Rules for the preparation and presentation of material standards - Part 001: General rules
TS EN 4500-003 Aerospace series - Metallic materials - Rules for the preparation and presentation of material standards - Part 003: Particular requirements for heat-resistant alloys
TS EN 4500-004 Aerospace series - Metallic materials - Rules for the preparation and presentation of material standards - Part 004: Particular requirements for titanium and titanium alloys
TS EN 4500-005 Aerospace series - Metallic materials - Rules for the preparation and presentation of material standards - Part 005: Particular requirements for steels
TS EN 3528 Aviation series - Steel X2NiCoMo18-8-5 (1,6359) - Melted vacuum induction melted and vacuum arc - Solution treatment and precipitation treatment - Bar - One or D? 150 mm - 1 750 MPa? Rm? 2 000 MPa
TS EN 4628 Aviation series - Steel fe-Pm 3504 (x4crnimo16-5-1) - Air melted - Hardened and tempered - Rod - De <150 mm - 1100 mpa <rm <1300 mpa
TS EN 4629 Aviation series - Steel fe-Pm 3504 (x4crnimo16-5-1) - Air melted - Hardened and tempered - Forged block - De <300 mm
TS EN 4631 Aviation series - Steel fe-Pm 3504 (x4crnimo16-5-1) - Air melted - Hardened and tempered - Rod - De <200 mm - 900 mpa <rm <1050 mpa
TS EN 2030 Aviation series - Steel X105CrMo17 (1.3544) - Hardened and annealed - Busbars - De? 150 mm
TS EN 4720: 2014 Air-Space series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electric remelting (ESR) - Hardened and tempered - Bar - De? 200 mm - 1 150 MPa? Rm? 1 300 MPa
TS EN 4721: 2014 Air-Space series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electric remelting (ESR) - Hardened and tempered - Bar - De? 200 mm - 900 MPa? Rm? 1 050 MPa
TS EN 2278: 2014 Aviation Series-Space series-Steel X12CrNiMoV12-3 (1.4933) - 900 MPa? Rm? 1 100 MPa - Bars - De? 150 mm
TS EN 4630: 2014 Aviation series - Steel fe-Pm 3504 (x4crnimo16-5-1) - Air melted - Hardened and tempered - Forgings - De <200 mm - 900 mpa <rm <1050 mpa
TS EN 4627: 2014 Aviation series - Steel fe-Pm 3504 (x4crnimo16-5-1) - Air melted - Hardened and tempered - Forgings - De <150 mm - 1100 mpa <rm <1300 mpa
TS EN 2226 Aviation series - Steel X105CrMo17 (1.4125) - Hardened and tempered - Forging by hand and die - De? 150 mm
TS EN 2589 Aviation series - Steel - Sheet and strip, cold rolled - Thickness 0,1 mm? a? 3 mm - Dimensions
TS EN 2590 Aerospace series - Steel - Hot rolled sheets and sheets
TS EN 2033 Aviation series - Cold rolled steel, Thickness 0,1 mm? a? 2,5 mm - Dimensions
TS EN 2002-005 Aerospace series - Metallic materials-Test methods-Part 005: Continuous drift and tension -Completion test
TS EN 2103-1 Aerospace series - Re-melting drafts and castings made of steel, nickel-based and cobalt-based alloys - Technical specifications - Part 1: General rules
TS EN 2104 Aviation-Acrylonitrile-Butadiene rubber (nbr) -40 hardness armor
TS EN 2157-1 Aviation series-Steel-Forging draft and forging-Technical specifications; Section 1: General rules
TS EN 2157-2 Aviation series - Steel - Forging draft and forging - Technical specifications - Part 2: Forging draft
TS EN 2157-3 Aviation series - Steel - Forging draft and forging - Technical specifications - Part 3: Semi-finished and finished forging
TS EN 2205 Aviation series - Steel fe-Pl1502 (25crmo4) - 900 mpa <rm> <1100 mpa - Rod - De> 40 mm
TS EN 2209 Aviation series- Steel fe-Pl1502 (25crmo4) - 900 mpa <rm <1100 mpa - Plate, strip and sheet - 0 mm <a <5 mm
TS EN 2398 Aviation series - Heat resistant steel fe-Pa2601 (x6nicrtimov26-15) - Rm? 900 mpa - Rods for machined bolts - D? 25 is mm
TS EN 2399 Aviation series - Heat resistant steel fe-Pa2601 (x4nicrtimov26-15) - Rm? 900 mpa - Rods for forged bolts - D? 25 is mm
TS EN 2438 Aviation series - Steel fe-Pl2102 (35nicr6) - 900 mpa <rm <1100 mpa - Rod - De <40 mm
TS EN 2439 Aviation series - Steel fe-Pl2102 (35nicr6) - 900 mpa <rm <1100 mpa - Forgings - De <40 mm
TS EN 2446 Aviation series - Steel fe-Pl1503 (35crmo4) - 1100 mpa <rm <1300 mpa - Rods - De <25 mm
TS EN 2448 Aviation series - Steel fe-Pl1503 (35crmo4) - 900 mpa <rm <1100 mpa - Rods - De <40 mm
TS EN 2469 Aerospace series - Steel fe-Pa3901 (x1crni18-10) - Melted with air - Softened - Wires - Diameter 0, 4 mm to 12, 5 mm - Rm 450 mpa to 650 mpa
TS EN 2478 Aviation series - Steel fe-Pl2107 (30nicrmo16) - 1220 mpa <rm <1370 mpa - Rods - De <40 mm
TS EN 2480 Aviation series - Steel fe-Pl2108 (36nicrmo16) - 1250 mpa <rm <1400 mpa - Rods - De <75 mm
TS EN 2481: 2010 Aviation series- Steel steel fe-Pl2108 (35nicrmo16) -1250 mpa = rm = 1 400 mpa - Forging - De = 75 mm
TS EN 2482: 2010 Aviation series - Steel steel fe-Pl2108 (35nicrmo16) -1100 mpa = rm = 1 300 mpa - Rods - De = 100 mm
TS EN 2483: 2010 Aviation series- Steel steel fe-Pl2108 (35nicrmo16) -1100 mpa = rm = 1 300 mpa - Forging - De = 100 mm
TS EN 2542 Aviation series - Steel fe-Pl1502 (25crmo4) - Annealed - Rod and wire - De <40 mm - For the largest torque nuts
TS EN 2543 Aviation series - Steel fe-Pl1502 (25crmo4) - Annealed - Plate and strip - 0 mm <a <3 mm - For the largest torque nuts
TS EN 2815 Aviation series - Steel fe-Pm1802 (x5crnicu15-5) - Re-melted using consumable electrodes - Treated with chemical solution and treated with precipitate - Rods for machining - A or d? 200 mm - Rm? 965 mpa
TS EN 2817 Aviation series - Steel fe-Pm1802 (x5crnicu15-5) - Re-melted consumable electrode - Chemically treated and precipitated - Rod to remove sawdust - A or d? 200 mm - Rm? 1070 mpa
TS EN 2831 Aviation series-Hydrogen brittleness in steel-Slow bending test
TS EN 2832 Aviation series-Hydrogen brittleness in steel-Notched sample test
TS EN 2947 Aviation series - Steel fe-Pa3901 (x2crni18-9) - Melted with air - No heat treatment - Cold drawn steel wire - A or d 2, 3 mm
TS EN 3114-001 Aerospace series - Test method - Microstructure of processed titanium alloy (+) products - Part 001: General specifications
TS EN 3145 Aviation series - Round bars, steel, hot rolled - Normal tolerances - Diameter 6 mm d 250 mm dimensions
TS EN 3146 Aviation series-Round bars, hot-rolled, steel, with threaded diameter-Diameter 6 mm d 250 mm-Dimensions
TS EN 3160 Aerospace series - Steel fe-Pm3801 (x5crnicu17-4) - Air melted, chemical solution treated and settled rod - Diameter d <200 mm and rupture stress rm <1310 mpa
TS EN 3161 Aerospace series - Steel fe-Pm3801 (x5crnicu17-4) - Air melted, chemical solution treated and settled rod - Diameter d <200 mm and rupture stress rm <930 mpa
TS EN 3163 Aviation series - Steel fe-Pm3801 (x5crnicu17-4) - Air melted, soft, forged - Diameter d <300 mm
TS EN 3329 Aviation series - Steel fe-Pl1503 (35crmo4) - Annealed - Sheet and strip - 0, 3 mm? a? 2 mm - for the largest torque nuts
TS EN 3359 Aviation series - Steel fe-Pm1503 (x3crnimoal13-8-2) - Melted and melted in vacuum using consumables, soft, forged, thickness a and diameter less than 300 mm
TS EN 3361 Aviation series - Steel fe-Pm1802 (x5crnicu15-5) - Remelted using consumable electrode, treated with chemical solution and treated with precipitate, plate and strip, thickness a <6 mm, 1070 mpa <rm < Which is 1220 mpa
TS EN 3364 Aviation series - Steel fe-Pm1802 (x5crnicu15-5) - Remelted, softened, forging block, thickness or diameter a or d <300 mm using consumable electrode
TS EN 3469 Aviation series - Steel fe-Pm1802 (x5crnicu15-5) - Re-melted using consumable electrode - Treated with chemical solution and treated with precipitate - Forging - A or d? 200 mm - Rm? 1310 mpa
TS EN 3476 Aviation series - Steel fe-Pl1501 (30crmo12) - Air-melted - Softened - Forging - Thickness or diameter of 300 mm
TS EN 3479 Aerospace series - Steel fe-Pm1802 (x5crnicu15-5) - Re-melted consumable electrode - Chemically treated and precipitated - Plate 6 - Thickness 6 mm to 20 mm - Rn 1070 mpa to 1220 mpa
TS EN 3480 Aviation series - Steel fe-Pa3601 (x6crniti18-10) - Melted with air - Softened - Plate - Thickness 6 mm <a <50 mm - 500 mpa <rm <700 mpa
TS EN 3487 Aviation series - Steel fe-Pa3601 (x6crniti18-10) - Melted with air - Soft - Processing rod - With A or d <250 mm - With 500 mpa <rm <700 mpa
TS EN 3491 Aviation series - Steel fe-Pm3901 (x15crni17-3) - Air melted - Hardened and tempered - Forgings - De> 100 mm - 900 mpa
TS EN 3507 Aviation series - Steel fe-Pl1501 (30crmo12) - Air melted - Hardened and tempered - Forgings - De> 100 mm - 930 mpa
TS EN 3527 Hearing protectors - Safety rules and testing - Part 7: Hearing-leveled ear plugs
TS EN 3816 Aviation series - Steel fe-Pa3601 (x6crniti18-10) - Melted by air - Softened and cold rolled - Plate and strip with a thickness of 3 mm - Rm> 800 mpa
TS EN 3889 Aviation series - Steel fe-Wm3801 (x5crnicu17-4) - Filler metal for welding
TS EN 3890 Aviation series - Steel fe-Wm1502 (x11crnimovn12-3) - Filler metal for welding
TS EN 3896 Aviation series - Steel fe-Wm1501 (x13crnimoco 12-3-2-2) - filler metal for welding
TS EN 3897 Aviation series - Steel fe-Wa4801 (x6crnimnnb18-10) - Filler metal for welding
TS EN 3971 Aerospace series - Steel fe-Pl1507 (40crmov12) - Melted with disposable electrode - Annealed - Forging - Length or diameter 350 mm
TS EN 3972 Aviation series - Steel fe-Pl1507 (40crmov12) - Melted with a disposable electrode - Hardened and tempered - Processing rod - Also> 50 mm in diameter, strength 1250 mpa <rm <1400 mpa
TS EN 3973 Aviation series - Steel fe-Cm3801 (x5crnicunb16-4) - Homogenized, chemically treated and precipitated hardened - Cast into waxed mold - Diameter is> 50 mm lan - Rm> 1030 mpa
TS EN 4059 Aviation series - Fillers and wires for welding in steel - diameter 0,5 mm? D ? 5,0 mm - Dimensions
TS EN 4328 Aviation series - Steel fe-Wm1601 (x18crwni13-3-2) - Filler metal for welding - Wire and rod
TS EN 4330 Aviation series - Steel fe-Wa4802 (x8crnimn27-22-2) - Filler metal for welding - Wire and rod
TS EN 4331 Aviation series - Steel fe-Wl1804 (25crmnmo4-2-2) - Filler metal for welding - Wire and rod
TS EN 4332 Aviation series - Steel fe-Wl1805 (8crmnmo12-4-9) - Filler metal for welding - Wire and rod
TS EN 4333 Aviation series - Steel fe-Wa4902 (x5crnicomowmn21-20-20-3-3-2) - Filler metal for welding - Wire and rod
TS EN 4334 Aerospace series - Steel Fe w 806 (15crmnmov5-4-9-3) filler metal for welding; Wire and rod
TS EN 4335 Aviation series - Steel fe-Wa2602 (x4nicrtimov26-15) - Filler metal for welding - Wire and rod
TS EN 4336 Aviation series - Steel fe-Wa3801 (x4crnimn20-10-2) - Filler metal for welding - Wire and rod
TS EN 4343 Aviation series - Steel fe-Wm1001 (x13cr12) - Filler metal for welding - Wire and rod
TS EN 4344 Aviation series - Steel fe-Wm1002 (x13cr13) - Filler metal for welding - Wire and rod
TS EN 4347 Aviation series - Steel fe-Pm1506 (x1crnimoalti13-8-2) - Melted with vacuum induction and remelted using consumable electrode, softened, thickness or diameter a or d <300 mm
TS EN 4462 Aviation series - Steel fe-Pm1506 (x1crnimoalti13-8-2) - Melted with vacuum induction and remelted using consumable electrode - Treated with chemical solution and treated with precipitation - Rods - Thickness or diameter a or d < 150 mm - Rm <1300 mpa
TS EN 4463 Aviation series - Steel fe-Pm1506 (x1crnimoalti13-8-2) - Melted with vacuum induction and remelted using consumable electrode - Treated with chemical solution and treated with sediment - Rods - Thickness or diameter a or d < 150 mm - Rm <1400 mpa
TS EN 4464 Aviation series - Steel fe-Pm1506 (x1crnimoalti13-8-2) - Melted by vacuum induction and remelted using consumable electrot - Treated with chemical solution and treated with precipitation - Forgings - Thickness or diameter a or d < 150 mm - Rm <1200 mpa
TS EN 4466 Aviation series - Steel fe-Pm1506 (x1crnimoalti13-8-2) - Melted with vacuum induction and remelted using consumable electrode - Treated with chemical solution and treated with precipitation - Forgings - Thickness or diameter a or d < 150 mm - Rm <1400 mpa
TS EN 4469 Aviation series - Steel fe-Pm1505 (x1crnimoalti12-9-2) - Melted with vacuum induction and remelted using consumable electrode - Treated with chemical solution and treated with sediment - Rods - Thickness or diameter a or d < 150 mm - Rm <1400 mpa
TS EN 4472 Aviation series - Steel fe-Pm1505 (x1crnimoalti12-9-2) - Melted with vacuum induction and remelted using consumable electrode - Treated with chemical solution and treated with precipitation - Forgings - Thickness or diameter a or d < 150 mm - Rm <1400 mpa
TS EN 4658: 2010 Aerospace series - Steel fe-Pm1507 (x1crnimoalti12-11-2) -Melted in vacuum and re-melted using a consumable eletrot- Chemical and precipitated process- Tattoos - A or d = 200 mm - Rpa = Mpa X
TS EN 4671: 2010 Aerospace series - Steel fe-Pm1507 (x1crnimoalti12-11-2) - Re-melted in vacuum media and re-melted using consumables - Forged - A or d = 200 mm - Rpa X
TS EN 4700-003: 2010 Aerospace series - Steel and heat resistant alloys - Formed products - Technical specifications - Part 003: Pipe
TS EN 4700-005: 2010 Aerospace series - Steel and heat resistant alloys - Formed products - Technical specifications - Part 005: Forging draft
TS EN 4700-006: 2010 Aerospace series - Steel and heat resistant alloys - Formed products - Technical specifications - Part 006: Pre-production and forging