17/30369678 DC : 0
NA
NA
Status of Standard is Unknown
PREN 7010 - AEROSPACE SERIES - USER GUIDE FOR CREATION AND DESIGNATION OF BOLTS
Available format(s)
Hardcopy , PDF
Language(s)
English
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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 : 2016 | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu<br> |
| SAE AMS 5726 : 2015 | STEEL, CORROSION AND HEAT-RESISTANT, BARS AND WIRE, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED AND WORK-STRENGTHENED, CONSUMABLE ELECTRODE REMELTED, 200 KSI (1379 MPA) TENSILE STRENGTH CAPABILITY |
| SAE AMS 5645 : 2016 | STEEL, CORROSION AND HEAT RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS, 18CR - 10NI - 0.40TI (321), SOLUTION HEAT TREATED |
| SAE AMS 5663 : 2016 | 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 DEGREES F (968 DEGREES 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 AMS 5937 : 2012 | 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 AMS 5662 : 2016 | 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 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE |
| SAE AMS 6346 : 2013 | 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 AMS 6348 : 2013 | 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 AMS 6322 : 2014 | 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 AMS 5643 : 2016 | STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 16CR - 4.0NI - 0.30CB (NB) - 4.0CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| SAE AMS 4971 : 2014 | 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 AMS 6940 : 2011 | 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 AMS 5845 : 2014 | 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 AMS 6358 : 2016 | STEEL SHEET, STRIP, AND PLATE, 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740) |
| SAE AMS 6528 : 2012 | STEEL, BARS, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), SPECIAL AIRCRAFT QUALITY CLEANLINESS, NORMALIZED |
| SAE AMS 5853 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS AND WIRE, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C) SOLUTION TREATED AND WORK-STRENGTHENED, 160 KSI (1103 MPA) TENSILE STRENGTH |
| SAE AMS 5647 : 2017 | STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 19CR - 9.5NI, SOLUTION HEAT TREATED |
| SAE AMS 5648 : 2016 | 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 AMS 6484 : 2016 | 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 AMS 4965 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 6415 : 2016 | STEEL, BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) |
| SAE AMS 5629H : 2016 | 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 AMS 5683:2012(S2017) | ALLOY WELDING WIRE, CORROSION AND HEAT RESISTANT, 75NI - 15.5CR - 8.0FE |
| SAE AMS 5734 : 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 HEAT TREATED |
| 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 AMS 5637 : 2012 | 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 AMS 5646 : 2014 | 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 AMS QQ S 763D : 2013(S2015) | 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 AMS 5719 : 2012 | 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 AMS 6325 : 2015 | 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 AMS 6414 : 2016 | 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 AMS 5622 : 2013 | 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 AMS 5844 : 2014 | 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 AMS 2700E : 2011 | PASSIVATION OF CORROSION RESISTANT STEELS |
| SAE AMS 5706 : 2015 | 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 DEGREES 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 AMS 5639 : 2017 | 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 AMS 6370 : 2016 | 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 AMS 6360 : 2013 | 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 AMS 5708 : 2015 | 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 DEGREES F (1079 DEGREES C) SOLUTION HEAT TREATED |
| PREN 6118 : DRAFT 2016 | AEROSPACE SERIES - PROCESS SPECIFICATION - ALUMINIUM BASE PROTECTION FOR FASTENERS |
| SAE AMS 6487 : 2016 | 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 AMS 5636 : 2006 | 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 AMS 4967 : 2014 | 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 AMS 4928 : 2016 | 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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