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PREN 7010 - AEROSPACE SERIES - USER GUIDE FOR CREATION AND DESIGNATION OF BOLTS
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English
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1. Foreword
2. Bolt
Annex A
Bibliography
prEN 7010.
| Committee |
ACE/12
|
| DocumentType |
Draft
|
| Pages |
36
|
| PublisherName |
British Standards Institution
|
| Status |
NA
|
| EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
| EN 4473:2010 | Aerospace series - Aluminium pigmented coatings for fasteners - Technical specification |
| SAE AMS5659S | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu |
| SAE AMS5726E | Steel, Corrosion and Heat-Resistant, Bars and Wire 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V 1800 °F (982 °C) Solution Heat Treated and Work-Strengthened Consumable Electrode Remelted 200 ksi (1379 MPa) Tensile Strength Capability |
| SAE AMS5645S | Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, Tubing, and Rings 18Cr - 10Ni - 0.40Ti (321) Solution Heat Treated |
| SAE AMS5663N | Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution and Precipitation Heat Treated |
| ISO 5855-2:1999 | Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts |
| SAE AMS 5737 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
| PREN 3513 : 200P1 | AEROSPACE SERIES - STEEL FE-PL711 - HARDENED AND TEMPERED - 900 <= R[M] <= 1100 MPA - BAR AND WIRE - D[E] <= 45 MM |
| ISO 5855-1:1999 | Aerospace MJ threads Part 1: General requirements |
| PREN 2475 : 200P1 | |
| ISO 7689:2008 | Aerospace Bolts, with MJ threads, made of alloy steel, strength class 1 100 MPa Procurement specification |
| SAE AMS5937 | Steel, Corrosion-Resistant, Bars, Wire, and Forgings 12Cr - 11Ni - 2Mo 1.5Al 0.3Ti Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated, Precipitation Hardenable |
| PREN 2959 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1302 (NICR20CO13MO4TI3AL) - SOLUTION TREATED AND COLD WORKED - BAR FOR FORGED FASTENERS - 3 MM <= D <= 30 MM |
| SAE AMS5662N | Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50AI - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Heat Treated, Precipitation-Hardenable |
| SAE AMS6346B | Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength |
| PREN 2304 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 100 MM - R[M] >= 960 MPA |
| SAE AMS6348D | Steel, Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Normalized |
| EN 3330:2009 | Aerospace series - Steel FE-PL1503 (35CrMo4) - Annealead - Bar and wire - De ≤ 40 mm - For prevailing torque nuts |
| SAE AMS6322P | Steel Bars, Forgings, and Rings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) |
| PREN 2448 : 1 | AEROSPACE SERIES - STEEL FE-PL62 - 900 MPA <= R[M] <= 1100 MPA - BARS D[E] <= 40 MM |
| EN 2516:1997 | Aerospace series - Passivation of corrosion resisting steels and decontamination of nickel base alloys |
| EN 2438:2008 | Aerospace series - Steel FE-PL2102 (35NiCr6) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm |
| PREN 3813 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - D[E] <= 50 MM |
| EN 2439:2009 | Aerospace series - Steel FE-PL2102 (34NiCr6) - 900 MPa ≤ Rm ≤ 1 100 MPa - Forgings - De ≤ 40 mm |
| WL 1.4944-3 : 1984 | HIGH TEMPERATURE PRECIPITATION-HARDENING NICKEL-CHROMIUM-TITANIUM STEEL WITH ABOUT 0,06C-25NI-15CR-2,1TI-1,2MO; RODS AND WIRE FOR SCREWS AND NUTS |
| EN 4315:2007 | 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 |
| EN 4317:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D ≤ 200 mm |
| SAE AMS5643U | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb (Nb) - 4.0Cu Solution Heat Treated, Precipitation Hardenable |
| SAE AMS4971K | Titanium Alloy, Bars, Wire, Forgings, and Rings 6Al - 6V - 2Sn Annealed, Heat Treatable |
| PREN 3833 : 200P2 | AEROSPACE SERIES - BOLTS, MJ THREADS, IN HEAT RESISTING NICKEL BASE ALLOY NI-PH2601 (INCONEL 718), PASSIVATED - CLASSIFICATION: 1550 MPA (AT AMBIENT TEMPERATURE)/650 DEGREES C - TECHNICAL SPECIFICATION |
| EN 2491:2011 | Aerospace series - Molybdenum disulphide dry lubricants - Coating methods |
| ISO 8168:2016 | Aerospace — Bolts, with MJ threads, made of heat and corrosion resisting steel, strength class 1 100 MPa — Procurement specification |
| SAE AMS6940A | Titanium Alloy Bars, Forgings and Forging Stock 3.0Al - 2.5V Annealed |
| EN 2398:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X6NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for machined bolts - D ≤ 25 mm |
| WL 3.7164-2 : 1990 | AEROSPACE - TITANIUM ALLOY WITH APPROX. 6AL-4V - BARS AND FORGINGS |
| TR 4609 : 2015 | AEROSPACE SERIES - SPIRAL DRIVE RECESSES FOR THREADED FASTENERS - GEOMETRICAL DEFINITION AND TECHNICAL REQUIREMENTS |
| SAE AMS5845J | Alloy, Corrosion-Resistant, Round Bars 20Cr - 35Ni - 35Co - 10Mo Vacuum Induction Plus Consumable Electrode Vacuum Remelted Solution Heat Treated, Work Strengthened, and Aged |
| EN 4826:2014 | Aerospace series - Zinc-Nickel (12 %-16 % Ni) plating of steels with specified tensile strength ≤ 1 450 MPa, copper alloys, nickel alloys and aluminium alloys for parts and fasteners |
| SAE AMS6358K | Steel Sheet, Strip, and Plate 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) |
| SAE AMS6528C | Steel, Bars 0.95Cr - 0.20Mo (0.28 – 0.33C) (SAE 4130) Special Aircraft Quality Cleanliness Normalized |
| SAE AMS5853C | Steel, Corrosion and Heat-Resistant, Bars and Wire 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Consumable Electrode Melted 1800 °F (982 °C) Solution Treated and Work-Strengthened 160 ksi (1103 MPa) Tensile Strength |
| SAE AMS5647K | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 19Cr - 9.5Ni Solution Heat Treated |
| SAE AMS5648M | Steel, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Tubing, and Rings, 17Cr - 12Ni - 2.5Mo (316) Solution Heat Treated |
| EN 2205:2009 | Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm |
| EN 2483:2010 | Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Forgings - De ≤ 100 mm |
| AIR 9169 : 1990 | CONDITIONS D'HOMOLOGATION ET DE RECEPTION DES VIS EN ACIER A TRES HAUTE RESISTANCE (CLASSE 1 550 MPA ET 1 800 MPA) |
| AIR 9160 : 1992 | CONDITIONS GENERALES DE RECETTE ET D'EMPLOI DES ACIERS CORROYES UTILISES DANS LES CONSTRUCTIONS AERONAUTIQUES |
| AIR 9185 : 1982 | CONDITIONS D'HOMOLOGATION ET DE CONTROLE DES VIS EN ALLIAGE DE TITANE T-A 6 V (CLASSE DE RESISTANCE 1 100 MPA) |
| EN 2133:2010 | Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys |
| EN 2481:2010 | Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 250 MPa ≤ Rm ≤ 1 400 MPa - Forgings - De ≤ 75 mm |
| WL 1.6604-1 : 1982 | HEAT-TREATABLE CHROMIUM-NICKEL-MOLYBDENUM STEEL WITH ABOUT 0.3C-2CR-2NI-0.4MO; RODS AND FORGINGS |
| SAE AMS6484E | Steel, Bars, Forgings, and Tubing 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340) Normalized and Tempered |
| EN 2478:2008 | Aerospace series - Steel FE-PL2107 (30NiCrMo16) - 1 220 MPa ≤ Rm ≤ 1 370 MPa - Bars - De ≤ 40 mm |
| WL 1.7224-1 : 1992 | AEROSPACE; HARDENED AND TEMPERED CHROMIUM-MOLYBDENUM STEEL WITH APPROX. 0,35C-1CR-2MO; BARS AND WIRE FOR BOLTS AND NUTS TO BE COLD OR HOT FORMED |
| ISO 8080:1985 | Aerospace Anodic treatment of titanium and titanium alloys Sulfuric acid process |
| ISO 14276:2002 | Aerospace — Drives, internal, offset cruciform — Metric series |
| SAE AMS4965L | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged |
| SAE AMS6415U | Steel, Bars, Forgings, and Tubing 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340) |
| SAE AMS5629H | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 13Cr - 8.0Ni - 2.2Mo - 1.1Al Vacuum Induction Plus Consumable Electrode Melted Solution Heat Treated, Precipitation Hardenable |
| SAE AMS5683G | Alloy Welding Wire, Corrosion and Heat Resistant 75Ni - 15.5Cr - 8.0Fe |
| EN 2786:2008 | Aerospace series - Electrolytic silver plating of fasteners |
| PREN 3220 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY (NI-P101HT) - COLD WORKED AND SOFTENED - BAR AND WIRE FOR CONTINUOUS FORGING OR EXTRUSION FOR FASTENERS - 3 <= D <= 30 MM |
| PREN 2137 : 1 | AEROSPACE SERIES - STEEL FE-PL75 - 1100 MPA <= R[M] <= 1250 MPA - BARS D[E] <= 100 MM |
| SAE AMS5637H | Steel, Corrosion Resistant, Bars and Wire 18Cr - 9.0Ni (SAE 30302) Solution Heat Treated, Cold Drawn and Stress Relieved 125 ksi (862 MPa) Tensile Strength |
| SAE AMS5646P | Steel, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Tubing, and Rings 18Cr - 11Ni - 0.60Cb(Nb) (347) Solution Heat Treated |
| PREN 2961 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 - SOLUTION TREATED - BAR FOR MACHINED FASTENERS - D <= 50 MM - R[M] >= 1270 MPA |
| SAE AMSQQS763D | Steel, Corrosion Resistant, Bars, Wire, Shapes, and Forgings |
| AIR 9173 : 1980 | |
| SAE AMS 5732 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS5719D | Steel Bars, Wire, Forgings, Tubing, Rings, and Extrusions, Corrosion-Resistant 11.8Cr - 2.5Ni - 1.8Mo - 0.33V (0.08 - 0.15C) Annealed, Vacuum Arc or Electroslag Remelted |
| EN 2399:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for forged bolts - D ≤ 25 mm |
| ISO 68-1:1998 | ISO general purpose screw threads — Basic profile — Part 1: Metric screw threads |
| EN 4377:2015 | Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) - Non heat treated - Forging stock - a or D ≤ 300 mm |
| SAE AMS6325K | Steel, Bars, and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength |
| AIR 9184 : 1965 | |
| SAE AMS6414M | Steel, Bars, Forgings, and Tubing 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340) Vacuum Consumable Electrode Remelted |
| ISO 9152:1998 | Aerospace Bolts, with MJ threads, in titanium alloys, strength class 1 100 MPa Procurement specification |
| PREN 3666 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 - SOLUTION TREATED AND COLD WORKED - BAR FOR FORGED FASTENERS - D <= 50 MM - 1550 MPA <= R[M] <= 1830 MPA |
| EN 2482:2010 | Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Bars - De ≤ 100 mm |
| SAE AMS 5731 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED |
| AIR 9165 : 1992 | CONDITIONS GENERALES DE RECETTE ET D'EMPLOI DES ACIERS ET ALLIAGES CORROYES RESISTANT A CHAUD, UTILISES DANS LES CONSTRUCTIONS AERONAUTIQUES |
| LN 65010-1:1968-03 | Specification for screws and bolts of low alloyed steel with minimum tensile strength up to 90 kg/mm |
| WL 1.4534-1 : 2012 | AEROSPACE SERIES - HIGH-STRENGTH PRECIPITATION-HARDENING STAINLESS CHROMIUM-NICKEL-MOLYBDENUM-ALUMINIUM STEEL WITH APPROX. 0,04 C - 13 CR - 8 NI - 2,2 MO - 1 AL - PART 1: BARS AND FORGINGS |
| EN 2808:1997 | Aerospace series - Anodizing of titanium and titanium alloys |
| WL 2.4668-2 : 1984 | HIGH TEMPERATURE NICKEL ALLOY WITH ABOUT 0,05C-19CR-18FE-5NB-3MO; RODS AND FORGINGS |
| SAE AMS5622F | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb - 4.0Cu Solution Heat Treated, Precipitation Hardenable Consumable Electrode Remelted |
| AIR 9167 : 1979 | CONDITIONS D'HOMOLOGATION ET DE CONTROLE DES VIS RESISTANT A CHAUD |
| SAE AMS5844H | Alloy, Corrosion-Resistant, Round Bars 20Cr - 35Ni - 35Co - 10Mo Vacuum Induction Plus Consumable Electrode Vacuum Remelted Solution Heat Treated and Work Strengthened |
| PREN 6117 : 200P1 | AEROSPACE SERIES - SPECIFICATION FOR LUBRICATION OF FASTENERS WITH CETYL ALCOHOL |
| AIR 9183 : 1966 | |
| PREN 3761 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 - SOFTENED AND COLD WORKED - BAR FOR FORGED FASTENERS - D <= 50 MM - 1100 MPA <= R[M] <= 1300 MPA |
| SAE AMS2700E | Passivation of Corrosion Resistant Steels |
| SAE AMS5706M | Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 57Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.006B - 0.05Zr Consumable Electrode or Vacuum Induction Melted 1825 to 1900 °F Solution Heat Treated |
| PREN 3514 : 200P1 | AEROSPACE SERIES - STEEL FE-PL711 - HARDENED AND TEMPERED - 1100 <= R[M] <= 1300 MPA - BAR AND WIRE FOR BOLTS - D[E] <= 25 MM |
| LN 65010-2:1968-03 | Specification for screws and bolts of low alloyed steel with minimum tensile strength up to 90 kg/mm; minimum tensile breaking loads, proof loads |
| SAE AMS5639J | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 19Cr - 10Ni Solution Heat Treated |
| NFL 05 224 : 1990 | AIRCRAFT AND AEROSPACE - ISO M THREAD - LIMITING PROFILES AND ISO TOLERANCES FOR BOLTS AND NUTS |
| PREN 3219 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY (NI-P100HT) - COLD WORKED AND SOFTENED - BAR AND WIRE FOR CONTINUOUS FORGING OR EXTRUSION FOR FASTENERS - 3 <= D <= 30 MM |
| WL 1.7784-3 : 2012 | AEROSPACE SERIES - ULTRAHIGH-STRENGTH CHROMIUM-MOLYBDENUM-VANADIUM STEEL WITH APPROX. 0,4 C - 5 CR - 1,3 MO - 0,5 V - PART 3: BAR AND WIRE FOR COLD-OR-HOT-FORMED BOLTS AND NUTS |
| EN 2446:2008 | Aerospace series - Steel FE-PL1503 (35CrMo4) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Bars - De ≤ 25 mm |
| SAE AMS6370P | Steel, Bars, Forgings, and Rings 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) |
| ISO 3353-1:2002 | Aerospace Lead and runout threads Part 1: Rolled external threads |
| PREN 2952 : 200P3 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 - SOLUTION TREATED AND COLD WORKED - BAR FOR FORGED FASTENERS - D <= 50 MM - 1270 MPA <= R[M] <= 1550 MPA |
| SAE AMS6360M | Steel Tubing, Seamless 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) Normalized or Stress Relieved |
| EN 4318:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De ≤ 100 mm, Rm ≥ 960 MPa |
| ISO 10664:2014 | Hexalobular internal driving feature for bolts and screws |
| SAE AMS5708L | Nickel Alloy, Corrosion and Heat-Resistant, Bars, Wire Forgings, and Rings 58Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B Consumable Electrode or Vacuum Induction Melted 1975 °F (1079 °C) Solution Heat Treated |
| PREN 6118 : DRAFT 2016 | AEROSPACE SERIES - PROCESS SPECIFICATION - ALUMINIUM BASE PROTECTION FOR FASTENERS |
| SAE AMS6487L | Steel, Bars, and Forgings 5.0Cr - 1.3Mo - 0.50V (0.38 - 0.43C) (H-11) Consumable Electrode Vacuum Melted |
| ISO 4757:1983 | Cross recesses for screws |
| EN 2480:2008 | Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 250 MPa ≤ Rm ≤ 1 400 MPa - Bars - De ≤ 75 mm |
| SAE AMS5636F | Steel, Corrosion-Resistant, Bars and Wire 18Cr - 9.0Ni (SAE 30302) Solution Heat Treated and Cold Drawn 100 ksi (689 MPa) Tensile Strength |
| DTD 5638 : JUL 85 | HEAT RESISTING NICKEL BASED ALLOY FE-52.5 NI-19 CR-3 MO-5 (N6+TA)-0.9 TI-0.5 AL (VACUUM MELTED) BAR AND WIRE FOR FASTENERS MAXIMUM DIAMETER OR SECTIONAL DIMENSION 50 MM |
| SAE AMS4967L | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable |
| EN 2448:2008 | Aerospace series - Steel FE-PL1503 (35CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm |
| ISO 7913:1994 | Aerospace Bolts and screws, metric Tolerances of form and position |
| ISO 3161:1999 | Aerospace — UNJ threads — General requirements and limit dimensions |
| PREN 2960 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY (NI-P101HT) - COLD WORKED AND SOLUTION TREATED - BAR FOR MACHINING FOR FASTENERS - 3 <= D <= 50 MM |
| PREN 3639 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 - SOFTENED AND COLD WORKED - WIRE FOR FORGED FASTENERS - D <= 15 MM - 900 MPA <= R[M] <= 1100 MPA |
| SAE AMS4928V | Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6Al - 4V Annealed |
| EN 4376:2016 | Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section, De ≤ 200 mm |
| SAE AMS 5962 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, ROUND BARS AND WIRE, 52.5NI - 19CR - 3.0MO - 5.1CB - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION TREATED AND WORK STRENGTHENED, PRECIPITATION HARDENABLE |
| ISO 1891:2009 | Fasteners — Terminology |
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