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  • EN 4700-002:2016

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section

    Available format(s): 

    Superseded date:  19-05-2021

    Language(s): 

    Published date:  13-04-2016

    Publisher:  Comite Europeen de Normalisation

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    Table of Contents - (Show below) - (Hide below)

    European Foreword
    Introduction
    1 Scope
    2 Normative references
    3 Terms and definitions
    4 Wording of order
    5 Health and safety
    6 Technical requirements

    Abstract - (Show below) - (Hide below)

    This standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat resisting alloy bar and section. It shall be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.

    General Product Information - (Show below) - (Hide below)

    Committee ASD-STAN
    Development Note Supersedes PREN 4700-002. (06/2016)
    Document Type Standard
    Publisher Comite Europeen de Normalisation
    Status Superseded
    Superseded By
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    EN 2306 : 2017 AEROSPACE SERIES - HEAT RESISTING - NICKEL BASE ALLOY NI-CR[20]CO[3]FE[3] - ANNEALED - BARS
    BS EN 2213:2012 Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Bars. De ≤ 16 mm. 980 MPa ≤ Rm ≤ 1 180 MPa
    NF EN 4655 : 2011 AEROSPACE SERIES - STEEL FE-PM 1506 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D < OR = 200 MM - RM > OR = 1400 MPA
    BS EN 4500-005:2012 Aerospace series. Metallic materials. Rules for drafting and presentation of material standards Specific rules for steels
    BS EN 4500-003:2012 Aerospace series. Metallic materials. Rules for drafting and presentation of material standards Specific rules for heat resisting alloys
    BS EN 4631:2013 Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa
    PREN 2278 : 1 AEROSPACE SERIES - STEEL X12CRNIMOV12-3 (1.4933) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 150 MM
    I.S. EN 4720:2014 AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA
    PREN 4721 : DRAFT 2012 AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <=200 MM - 900 MPA <= R[M] <= 1050 MPA
    UNI EN 4500-003 : 2014 AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 003: SPECIFIC RULES FOR HEAT RESISTING ALLOYS
    PREN 4720 : DRAFT 2012 AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA
    I.S. EN 2221:2017 AEROSPACE SERIES - STEEL FE-PL31 - HARDENED AND TEMPERED - HOLLOW BARS - 3,5 MM <= A <= 55 MM
    I.S. EN 2213:2012 AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - BARS - D[E] <= 16 MM - 980 MPA <= R[M] <= 1180 MPA
    BS EN 2135:2017 Aerospace series. Steel FE-PL61. Carburized, hardened and tempered. Bar. De ≤ 40 mm
    I.S. EN 3528:2013 AEROSPACE SERIES - STEEL X2NICOMO18-8-5 (1.6359) - VACUUM INDUCTION MELTED AND VACUUM ARC REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 150 MM - 1750 MPA <= R[M] <= 2000 MPA
    UNI EN 2213 : 2013 AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - BARS - D[E] <= 16 MM - 980 MPA <= R[M] <= 1180 MPA
    I.S. EN 2030:2013 AEROSPACE SERIES - STEEL X105CRMO17 (1.3544) - HARDENED AND TEMPERED - BARS - D[E] <= 150 MM
    UNI EN 4656 : 2011 AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1520 MPA
    BS EN 4657:2010 Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D ≤ 200 mm. Rm ≥ 1650 MPa
    BS EN 4656:2010 Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D ≤ 200 mm. Rm ≥ 1520 MPa
    UNI EN 4631 : 2013 AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA
    I.S. EN 4721:2014 AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA
    16/30337543 DC : 0 BS EN 8.4577 - AEROSPACE SERIES - X5CRNICU15-5 (1.4545) - CONSUMABLE ELECTRODE REMELTED (ESR OR VAR) - SOLUTION TREATED AND PRECIPITATION TREATED (H1025) - BAR FOR MACHINING - A OR D <= 250 MM - 1070 MPA <= R[M] <= 1200 MPA - PREMIUM QUALITY (PQ)
    EN 2221 : 2017 AEROSPACE SERIES - STEEL FE-PL31 - HARDENED AND TEMPERED - HOLLOW BARS - 3,5 MM <= A <= 55 MM
    I.S. EN 4376:2016 AEROSPACE SERIES - HEAT RESISTING ALLOY NICR19FE19NB5MO3 (2.4668) SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION, D[E] <= 200 MM
    I.S. EN 2278:2014 AEROSPACE SERIES - STEEL X12CRNIMOV12-3 (1.4933) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 150 MM
    I.S. EN 4657:2010 AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION REMELTED - BARS - A OR D <= 200 MM - R[M] >= 1650 MPA
    UNI EN 4657 : 2011 AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1650 MPA
    I.S. EN 2119:2017 AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED -WIRES FOR RIVETS - 2 MM <= D <= 10 MM - R[M] >= 960 MPA
    UNI EN 2030 : 2014 AEROSPACE SERIES - STEEL X105CRMO17 (1.3544) - HARDENED AND TEMPERED - BARS - D[E] <= 150 MM
    I.S. EN 2306:2017 AEROSPACE SERIES - HEAT RESISTING - NICKEL BASE ALLOY NI-CR[20]CO[3]FE[3] - ANNEALED - BARS
    BS EN 4721:2014 Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted and electroslag remelted (ESR). Hardened and tempered. Bar. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa
    BS EN 2482:2010 Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1100 MPa ≤ Rm ≤ 1300 MPa. Bars. De ≤ 100 mm
    I.S. EN 2137:2017 AEROSPACE SERIES - STEEL FE-PL75 - 1100 MPA <= R[M] <= 1250 MPA - BARS - DE <= 100 MM
    BS EN 4720:2014 Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted and electroslag remelted (ESR). Hardened and tempered. Bar. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa
    BS EN 4628:2013 Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa
    BS EN 4655:2010 Aerospace series. Steel FEPM1506 (X1CrNiMoAlTi12-10-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D ≤ 200 mm. Rm ≥ 1400 MPa
    12/30263035 DC : 0 BS EN 4825 - AEROSPACE SERIES - STEEL X12CRNIMOV12-3 (1.4933) - AIR MELTED AND CONSUMABLE ELECTRODE REMELTED - HARDENED AND TEMPERED - BAR - D[E] <= 150 MM - 900 MPA <= R[M] <= 1100 MPA
    I.S. EN 2482:2010 AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 100 MM
    I.S. EN 4500-003:2012 AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 003: SPECIFIC RULES FOR HEAT RESISTING ALLOYS
    EN 2135:2017 Aerospace series - Steel FE-PL61 - Carburized, hardened and tempered - Bar - De ≤ 40 mm
    UNI EN 4655 : 2011 AEROSPACE SERIES - STEEL FE-PM1506 (X1CRNIMOAITI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1400 MPA
    EN 2119 : 2017 Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated - Wires for rivets - 2 mm ≤ D ≤ 10 mm - Rm ≥ 960 MPa
    BS EN 3528:2013 Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa
    11/30243869 DC : 0 BS EN 4631 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA
    11/30242528 DC : DRAFT JAN 2011 BS EN 4628 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED - HARDENED AND TEMPERED - BAR D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA
    BS EN 2030:2013 Aerospace series. Steel X105CrMo17 (1.3544). Hardened and tempered. Bars. De ≤ 150 mm
    UNI EN 2482 : 2011 AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 100 MM
    UNI EN 4500-005 : 2014 AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 005: SPECIFIC RULES FOR STEELS
    EN 2482 : 2010 AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 100 MM
    EN 4500-005:2012 Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 005: Specific rules for steels
    EN 4721 : 2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1 050 MPa
    EN 4376:2016 Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section, De ≤ 200 mm
    EN 4631:2013 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1 050 MPa
    EN 4655:2010 Aerospace series - Steel FE-PM1506 (X1CrNiMoAlTi12-10-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ≤ 200 mm - Rm ≥ 1 400 MPa
    EN 2278 : 2014 AEROSPACE SERIES - STEEL X12CRNIMOV12-3 (1.4933) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 150 MM
    EN 2030:2013 Aerospace series - Steel X105CrMo17 (1.3544) - Hardened and tempered - Bars - De ≤ 150 mm
    EN 3528 : 2013 AEROSPACE SERIES - STEEL X2NICOMO18-8-5 (1.6359) - VACUUM INDUCTION MELTED AND VACUUM ARC REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 150 MM - 1750 MPA <= R[M] <= 2000 MPA
    EN 4500-003:2012 Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 003: Specific rules for heat resisting alloys
    EN 2213 : 2012 AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - BARS - D[E] <= 16 MM - 980 MPA <= R[M] <= 1180 MPA
    EN 4628:2013 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ≤ 200 mm — 1 150 MPa ≤ Rm ≤ 1 300 MPa
    EN 4657:2010 Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ≤ 200 mm - Rm ≥ 1 650 MPa
    EN 4656:2010 Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ≤ 200 mm - Rm ≥ 1520 MPa
    EN 4720:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ≤ 200 mm - 1 150 MPa ≤ Rm ≤ 1 300 MPa
    I.S. EN 4500-005:2012 AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 005: SPECIFIC RULES FOR STEELS
    BS EN 4376:2016 Aerospace series. Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated. Bar and section, De ≤ 200 mm
    NF EN 4657 : 2011 AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION REMELTED - BARS - A OR D < OR = 200 MM - R[M] > OR = 1650 MPA
    BS EN 2278:2014 Aerospace series. Steel X12CrNiMoV12-3 (1.4933). 900 MPa ≤ Rm ≤ 1 100 MPa. Bars. De ≤ 150 mm
    UNI EN 4628 : 2013 AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA
    EN 2137:2017 Aerospace series - Steel FE-PL75 - 1 100 MPa ≤ Rm ≤ 1 250 MPa - Bars - De ≤ 100 mm
    PREN 4842 : DRAFT 2016 AEROSPACE SERIES - X5CRNICU15-5 (1.4545) CONSUMABLE ELECTRODE REMELTED (ESR OR VAR) - SOLUTION TREATED AND PRECIPITATION TREATED (H1025) BAR FOR MACHINING A OR D <= 250 MM 1070 MPA <= R[M] <= 1200 MPA PREMIUM QUALITY (PQ)
    PREN 2465 : 200P1 AEROSPACE SERIES - STEEL X2CRNI18-9 (1.4307) - SOFTENED 450 MPA <= R[M] <= 680 MPA BAR FOR MACHINING 4 MM <= D[E] <= 100 MM
    I.S. EN 2135:2017 AEROSPACE SERIES - STEEL FE-PL61 - CARBURIZED, HARDENED AND TEMPERED - BAR - DE <= 40 MM
    I.S. EN 4656:2010 AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1520 MPA
    I.S. EN 4628:2013 AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA
    I.S. EN 4631:2013 AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA
    BS EN 2306:2017 Aerospace series. Heat resisting. Nickel base alloy Ni-Cr20Co3Fe3. Annealed. Bars

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    EN ISO 6892-1:2016 Metallic materials - Tensile testing - Part 1: Method of test at room temperature (ISO 6892-1:2016)
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