EN 4500-003:2012
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 003: Specific rules for heat resisting alloys
30-04-2013
10-10-2012
Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Rules for drafting and presentation
Bibliography
This European Standard specifies the specific rules for the drafting and presentation of heat resisting alloy material standards for aerospace applications.It should be used in conjunction with EN 4500-001.
Committee |
ASD-STAN
|
DevelopmentNote |
Supersedes PREN 4500-003. To be read in conjunction with EN 4500-001. (10/2012)
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DocumentType |
Standard
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PublisherName |
Comite Europeen de Normalisation
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Status |
Withdrawn
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Supersedes |
Standards | Relationship |
PN EN 4500-003 : 2013 | Identical |
I.S. EN 4500-003:2012 | Identical |
UNE-EN 4500-003:2012 | Identical |
NS EN 4500-003 : 2012 | Identical |
SN EN 4500-003 : 2013 | Identical |
NF EN 4500-003 : 2013 | Identical |
BS EN 4500-003:2012 | Identical |
UNI EN 4500-003 : 2014 | Identical |
NBN EN 4500-003 : 2012 | Identical |
DIN EN 4500-003:2012-12 | Identical |
NEN EN 4500-003 : 2012 | Identical |
DS EN 4500-003 : 2012 | Identical |
EN 2306:2017 | Aerospace series - Heat resisting - Nickel base alloy Ni-Cr20Co3Fe3 - Annealed - Bars |
BS EN 4262:2013 | Aerospace series. Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20). As forged. Forging stock. a or D ≤ 200 mm - 690 MPa ≤ Rm ≤ 880MPa |
BS EN 4377:2015 | Aerospace series. Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668). Non heat treated. Forging stock. a or D ≤ 300 mm |
I.S. EN 4377:2015 | AEROSPACE SERIES - HEAT RESISTING ALLOY NICR19FE19NB5MO3 (2.4668) - NON HEAT TREATED - FORGING STOCK - A OR D <= 300 MM |
I.S. EN 2402:2014 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NICR20CO3FE3 - ANNEALED - WIRE - D <= 10 MM |
I.S. EN 2030:2013 | AEROSPACE SERIES - STEEL X105CRMO17 (1.3544) - HARDENED AND TEMPERED - BARS - D[E] <= 150 MM |
UNI EN 4263 : 2014 | Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D ≤ 200 mm - 690 MPa ≤ Rm ≤ 960 MPa |
BS EN 4500-001:2012 | Aerospace series. Metallic materials. Rules for drafting and presentation of material standards General rules |
UNI EN 2402 : 2014 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NICR20CO3FE3 - ANNEALED - WIRE - D <= 10 MM |
UNI EN 4500-001 : 2014 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 001: GENERAL RULES |
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 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 2402:2014 | Aerospace series. Heat resisting nickel base alloy NiCr20Co3Fe3. Annealed. Wire. D ≤ 10 mm |
BS EN 2226:2014 | Aerospace series. Steel X105CrMo17 (1.4125). Hardened and tempered. Hand and die forgings. De ≤ 150 mm |
I.S. EN 4262:2013 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - AS FORGED - FORGING STOCK - A OR D <= 200 MM - 690 MPA <= R[M] <= 880 MPA |
I.S. EN 4263:2013 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - AS FORGED - FORGING STOCK - A OR D <= 200 MM - 690 MPA <= R[M] <= 960 MPA |
EN 2174:2017 | Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Solution treated and precipitation treated - Forgings - De ≤ 100 mm - Rm ≥ 850 MPa |
UNI EN 2226 : 2014 | Aerospace series - Steel X105CrMo17 (1.4125) - Hardened and tempered - Hand and die forgings - De ≤ 150 mm |
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 2174:2017 | Aerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Solution treated and precipitation treated. Forgings. De ≤ 100 mm - Rm ≥ 850 MPa |
BS EN 2030:2013 | Aerospace series. Steel X105CrMo17 (1.3544). Hardened and tempered. Bars. De ≤ 150 mm |
I.S. EN 2226:2014 | AEROSPACE SERIES - STEEL X105CRMO17 (1.4125) - HARDENED AND TEMPERED - HAND AND DIE FORGINGS - D[E] <= 150 MM |
EN 4376:2016 | Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section, De ≤ 200 mm |
EN 2226:2014 | Aerospace series - Steel X105CrMo17 (1.4125) - Hardened and tempered - Hand and die forgings - De ≤ 150 mm |
EN 2030:2013 | Aerospace series - Steel X105CrMo17 (1.3544) - Hardened and tempered - Bars - De ≤ 150 mm |
EN 4263:2013 | Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D ≤ 200 mm - 690 MPa ≤ Rm ≤ 960MPa |
EN 4500-001:2012 | Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 001: General rules |
EN 2402:2014 | Aerospace series - Heat resisting nickel base alloy NiCr20Co3Fe3 - Annealed - Wire - D ≤ 10 mm |
EN 4377:2015 | Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) - Non heat treated - Forging stock - a or D ≤ 300 mm |
EN 4262:2013 | Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D ≤ 200 mm - 690 MPa ≤ Rm ≤ 880MPa |
BS EN 4263:2013 | Aerospace series. Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20). As forged. Forging stock. a or D ≤ 200 mm - 690 MPa ≤ Rm ≤ 960MPa |
BS EN 4376:2016 | Aerospace series. Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated. Bar and section, De ≤ 200 mm |
I.S. EN 2174:2017 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2602 (X4NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED -FORGINGS - DE <= 100 MM R[M] => 850 MPA |
BS EN 2306:2017 | Aerospace series. Heat resisting. Nickel base alloy Ni-Cr20Co3Fe3. Annealed. Bars |
UNI EN 4262 : 2014 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - AS FORGED - FORGING STOCK - A OR D <= 200 MM - 690 MPA <= R[M] <= 880 MPA |
I.S. EN 4500-001:2012 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 001: GENERAL RULES |
ASD-STAN prEN 4500-004 P3:2023 | Aerospace series Metallic materials — Rules for drafting and presentation of material standards — Part 004: Specific rules for titanium and titanium alloys |
PREN 2957 : 200P1 | AEROSPACE SERIES - METHOD OF PREPARATION OF FORGED SAMPLES |
EN 2950:2008 | Aerospace series - Test method - Wrought heat resisting alloys Semi-finished products and parts - Conditions for macrographic and micrographic examination - Atlas of structures and defects |
EN 4700-002:2016 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section |
EN ISO 643:2012 | Steels - Micrographic determination of the apparent grain size (ISO 643:2012) |
EN 4700-004:2010 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 004: Wire |
PREN 2043 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - GENERAL REQUIREMENTS FOR SEMI-FINISHED PRODUCT QUALIFICATION (EXCLUDING FORGINGS AND CASTINGS) |
EN 2032-1:2001 | Aerospace series - Metallic materials - Part 1: Conventional designation |
ISO 643:2012 | Steels Micrographic determination of the apparent grain size |
EN 4500-001:2012 | Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 001: General rules |
PREN 6018 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - DETERMINATION OF DENSITY ACCORDING TO DISPLACEMENT METHOD |
EN 4700-003:2010 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 003: Tube |
EN 4258:1998 | Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use |
EN 2002-001:2005 | Aerospace series - Metallic materials - Test methods - Part 1: Tensile testing at ambient temperature |
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