PREN 7010 - AEROSPACE SERIES - USER GUIDE FOR CREATION AND DESIGNATION OF BOLTS

Available format(s)

Hardcopy , PDF

Language(s)

English

Publisher

British Standards Institution

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) - ANNEALED - BAR AND WIRE - D[E] <= 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 <= R[M] <= 1100 MPA - FORGINGS - D[E] <= 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) - 1100 MPA <= R[M] <= 1300 MPA - FORGINGS - D[E] <= 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) - 1250 MPA <= R[M] <= 1400 MPA - FORGINGS - D[E] <= 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) - R[M] >= 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) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 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) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 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) - 1250 MPA <= R[M] <= 1400 MPA - BARS - D[E] <= 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