PREN 4500-003 : 200P2
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 003: SPECIFIC RULES FOR HEAT RESISTING SLLOYS
Available format(s)
Hardcopy , PDF
Superseded date
04-01-2024
Language(s)
English
Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Rules for drafting and presentation
Bibliography
Describes the general rules for the drafting and presentation of heat resisting alloy material standards for aerospace applications.
| DevelopmentNote |
Supersedes PREN 2500/3. (10/2002) To be used in conjunction with PREN 4500-001. (08/2003)
|
| DocumentType |
Draft
|
| Pages |
21
|
| ProductNote |
Superseded by EN 4500-003:2012
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| DIN EN 4500-003:2012-12 | Identical |
| 10/30239357 DC : 0 | Identical |
| PREN 2187 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1301 (NICR19CO18MO4TI3AL3) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 200 MM - R[M] >= 1 300 MPA |
| PREN 2203 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1303 (NICO20CR20MO5TI2AL) - SOLUTION TREATED - SHEET, STRIP AND PLATE - 0,2 MM <= A <= 10 MM |
| PREN 2407 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NI-PH2601 (NICR19FE19NB5MO3) - SOLUTION TREATED AND PRECIPITATION TREATED - SHEET, STRIP AND PLATE - 0,2 MM <= A <= 10 MM |
| PREN 3671 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - NON HEAT TREATED - FORGING STOCK - A OR D <= 250 MM |
| PREN 3638 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - CONSUMABLE ELECTRODE REMELTED - SOLUTION AND PRECIPITATION TREATED - SHEET, STRIP AND PLATE - 0,5 MM <= A <= 10 MM |
| PREN 2402 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NICR20CO3FE3 - ANNEALED - WIRE - D <= 10 MM |
| PREN 4318 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 100 MM - R[M] >= 960 MPA |
| PREN 4369 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1701 (NICR15CO14AL5TI4MO4) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 100 MM |
| PREN 4338 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-WH3902 (NICR25MO10C) - FILLER METAL FOR WELDING - WIRE AND ROD |
| PREN 4095 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY - NI-CH1305 (NICR16CO10MO8A14TI4) - VACUUM MELTED - NON HEAT TREATED - PRECISION CASTINGS |
| PREN 4372 : 200P2 | AEROSPACE SERIES - HEAT RESISTING NICKEL ALLOY WITH COPPER NI-PD9001 (NICU31) - WIRE FOR SOLID RIVETS - D <= 10 MM |
| PREN 4263 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - AS FORGED - FORGING STOCK - A OR D <= 200 MM - 690 MPA <= R[M] <= 960 MPA |
| PREN 2174 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2602 (X4NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 100 MM - R[M] >= 850 MPA |
| PREN 4325 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-WH1302 (NICR20CO13MO4TI3AI) - FILLER METAL FOR WELDING - WIRE AND ROD |
| PREN 4377 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) - NON HEAT TREATED - FORGING STOCK - A OR D <= 300 MM |
| PREN 4383 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH2601 (NICR19FE19NB5MO3) - NON HEAT TREATED - REMELTING STOCK |
| PREN 4568 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-PH4101 (COCR20W15NI) - VACUUM MELTED - SOLUTION TREATED - SHEET AND STRIP - A <= 6 MM |
| PREN 4373 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PD9001 (NICU31) - ANNEALED - SEAMLESS TUBE - D <= 75 MM, A <= 3 MM |
| PREN 4087 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PD2101 (NICO14NB5TI2) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 75 MM R[M] >= 1210 MPA |
| PREN 4094 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH1305 (NICR16CO10MO8A14TI4) - VACUUM MELTED - NON HEAT TREATED - REMELTING |
| PREN 4570 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED - FORGINGS - D[E] <= 100 MM |
| 09/30201781 DC : 0 | BS 2HR 53 - SPECIFICATION FOR NICKEL-IRON-CHROMIUM-MOLYBDENUM-TITANIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NI/CO 42.5, CR 12.5, MO 5.8, TI 3.0, FE REMAINDER) |
| BS 2HR 204:2009 | Specification for nickel-chromium-iron-molybdenum-cobalt-tungsten heat-resisting alloy plate, sheet and strip (nickel base, Cr 21.7, Fe 18.5, Mo 9, Co 1.5, W 0.6) |
| BS EN 4382:2006 | Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb). Solution treated. Seamless tubes. For hydraulic application. D ≤ 50 mm, a ≤ 3 mm |
| BS EN 4671:2010 | Aerospace series. Steel FE-PM1506 (X1CrNiMoAlTi12-10-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 200 mm. Rm ≥ 1400 MPa |
| BS 3HR1(2010) : 2010 | SPECIFICATION FOR NICKEL-CHROMIUM-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CR 19.5, TI 2.2, AL 1.4) |
| BS 2HR 208:2009 | Specification for nickel-chromium-iron alloy plate, sheet and strip: annealed (nickel base, Cr 15.5, Fe 8) |
| BS 2HR 209:2011 | Specification for nickel-chromium-cobalt-molybdenum- titanium-aluminium heat-resisting alloy plate, sheet and strip (Nickel base, Cr 18, Co 14, Mo 7, Ti 2.2, Al 2.1) |
| BS 2HR 404:2011 | Specification for nickel-cobalt-chromium-molybdenum- titanium-aluminium heat-resisting alloy seamless tubes (Nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5) |
| 09/30199924 DC : 0 | BS 3HR 2 - SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CR 19.5, CO 18.0, TI 2.5, AL 1.5) |
| BS 2HR 403:2011 | Specification for nickel-chromium-titanium heat-resisting alloy seamless tubes (Nickel base, Cr 19.5, Ti 0.4) |
| BS 2HR 5:2010 | Specification for nickel-chromium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Ti 0.4) |
| BS 2HR 506:2010 | Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy wire: softened (nickel base, Cr 19.5, Co 1.8, Ti 2.5, Al 1.5) |
| BS 3HR 502:2011 | Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn and solution treated wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) |
| BS EN 4383:2006 | Aerospace series. Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3). Non heat treated. Remelting stock |
| 09/30201218 DC : DRAFT MAY 2009 | BS 2HR 208 - SPECIFICATION FOR NICKEL-CHROMIUM-IRON ALLOY PLATE, SHEET AND STRIP: ANNEALED (NICKEL BASE, CR 15.5, FE 8) |
| BS EN 3671:2007 | Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb). Non heat treated. Forging stock. a or D ≤ 250 mm |
| 09/30199929 DC : 0 | BS 2HR 3 - SPECIFICATION FOR NICKEL-COBALT-CHROMIUM-MOLYBDENUM-ALUMINIUM-TITANIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CO 20, CR 14.8, MO 5, AL 4.8, TI 1.2) |
| BS EN 4379:2007 | Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb).Solution treated, forging De ≤ 200 mm |
| BS EN 3668:2006 | Aerospace series. Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9). Non heat treated. Forging stock. a or D ≤ 250 mm |
| BS EN 4373:2007 | Aerospace series. Heat resisting alloy NI-PD9001 (NiCu31). Annealed, seamless tube D ? 75 mm, a ? 3 mm |
| BS EN 2398:2008 | Aerospace series. Heat resisting steel FE-PA2601(X6NiCrTiMoV26-15). Rm ≥ 900 MPa. Bars for machined bolts. D ≤ 25 mm |
| BS 2HR 3:2010 | Specification for nickel-cobalt-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 14.8, Mo 5, Al 4.8, Ti 1.2) |
| BS 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 |
| 09/30199935 DC : 0 | BS 2HR 6 - SPECIFICATION FOR NICKEL-CHROMIUM-IRON-MOLYBDENUM-COBALT-TUNGSTEN HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CR 21.7, F E 18.5, MO 9, CO 1.5, W 0.6) |
| 09/30201774 DC : 0 | BS 2HR 51 - SPECIFICATION FOR HIGH EXPANSION HEAT-RESISTING STEEL BILLETS, BARS, FORGINGS AND PARTS (NI 25.5, CR 15, TI 2, MN 1.5, MO 1.25, SI 0.7, V 0.3) (SOLUTION TREATED AT 980 DEGREE C) |
| 10/30239356 DC : 0 | BS EN 4500-1 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 1: GENERAL RULES |
| BS 2HR 240:2011 | Specification for cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy plate, sheet and strip (Cobalt base, Cr 20, W 15, Ni 10, Mn 1.5) |
| I.S. EN 4672:2011 | AEROSPACE SERIES - STEEL FE-PM1504 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| PREN 2202 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1303 (NICO20CR20MO5TI2AL) - SOLUTION TREATED - SEAMLESS TUBE - D <= 50 MM, A <= 3 MM |
| PREN 2199 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1303 (NICO20CR20MO5TI2AL) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 200 MM |
| PREN 2233 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CD1701 (NICO15CR10AL6TI5MO3) - VACUUM MELTED - NON HEAT TREATED - PRECISION CASTING - A OR D <= 50 MM |
| PREN 4262 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - AS FORGED - FORGING STOCK - A OR D <= 200 MM - 690 MPA <= R[M] <= 880 MPA |
| PREN 4314 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2602 (X4NICRTIMOV26-15) - NON HEAT TREATED - FORGING STOCK - A OR D <= 250 MM |
| PREN 4569 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-PH4101 (COCR20W15NI) - VACUUM MELTED - SOLUTION TREATED - WIRE - D <= 4 MM |
| PREN 4375 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1301 (NICR19CO18MO4TI3AL3) - NON HEAT TREATED - FORGING STOCK - A OR D <= 250 MM |
| PREN 4566 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-PH4101 (COCR20W15NI) - VACUUM MELTED - SOLUTION TREATED - FORGINGS - D[E] <= 100 MM |
| PREN 4575 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED AND DESCALED - SHEET AND PLATE - 3 MM < A <= 50 MM |
| 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 |
| PREN 2226 : 200P1 | AEROSPACE SERIES - STEEL FE-PM 3501 (X105CRMO17) - HARDENED AND TEMPERED - HAND AND DIE FORGINGS D[E] <= 150 MM |
| PREN 2403 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NI-CH2601 (NICR19FE19NB5MO3) - VACUUM MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - PRECISION CASTING - A OR D <= 50 MM |
| I.S. EN 4384:2007 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH1303 (NICO20CR20MO5TI2AL) - NON HEAT TREATED - REMELTING STOCK |
| PREN 4671 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1506 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION REMELTED - FORGINGS - A OR D <= 200 MM - R[M] >= 1400 MPA |
| PREN 4264 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2501 (X4NICRMOTI43-13) - AS FORGED - FORGING STOCK - A OR D <= 200 MM |
| PREN 4329 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-WH0001 (NICR20) - FILLER METAL FOR WELDING - WIRE AND ROD |
| PREN 4337 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-WH8901 (NICR16TI3MN2) - FILLER METAL FOR WELDING - WIRE AND ROD |
| PREN 4370 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1701 (NICR15CO14AL5TI4MO4) - NON HEAT TREATED - FORGING STOCK - A OR D <= 100 MM |
| PREN 4378 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) - SOLUTION TREATED AND PRECIPITATION TREATED - WIRE FOR RIVETS - D <= 1,6 MM |
| PREN 4376 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 200 MM |
| PREN 4382 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - SOLUTION TREATED - SEAMLESS TUBES - FOR HYDRAULIC APPLICATION - D <= 50 MM, A <= 3 MM |
| PREN 4511 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2301 (NICR22FEMO) - SOLUTION TREATED AND COLD WORKED - WIRE FOR RIVETS - 1,6 MM <= D <= 10 MM |
| PREN 4567 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-PH4101 (COCR20W15NI) - VACUUM MELTED - SOLUTION TREATED - BAR AND SECTION - A OR D <= 100 MM |
| PREN 4571 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED - BAR AND SECTION - D[E] <= 100 MM |
| PREN 4097 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY - NI-CD1401 (NICO10W10CR9AI6TA3) - VACUUM MELTED - PRECIPITATION TREATED - PRECISION CASTINGS |
| PREN 4093 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3901 (NICR25MO10) - AIR MELTED AND VACUUM REFINED - ANNEALED - SHEET, STRIP AND PLATE - A > 3 MM |
| BS 3HR 401:2011 | Specification for nickel-chromium-titanium-aluminium heat-resisting alloy seamless tubes (Nickel base, Cr 19.5, Ti 2.2, Al 1.4) |
| 09/30199937 DC : 0 | BS 2HR 10 - SPECIFICATION FOR NICKEL-COBALT-CHROMIUM-MOLYBDENUM-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CO 20, CR 20, MO 5.9, TI 2.1, AL 0.5) |
| 09/30201215 DC : DRAFT MAY 2009 | BS 2HR 207 - SPECIFICATION FOR NICKEL-IRON-CHROMIUM-MOLYBDENUM-ALUMINIUM-TITANIUM HEAT-RESISTING ALLOY PLATE, SHEET AND STRIP (NI/CO 43.5, CR 16.5, MO 3.3, AL 1.2, TI 1.2, FE REMAINDER) |
| PREN 2184 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2301 (NICR21FE18MO9) - SOLUTION TREATED - BAR AND SECTION - D[E] <= 200 MM |
| 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 |
| PREN 3018 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2801 (NICR16FE7TI3NB1AI1) - CONSUMABLE ELECTRODE REMELTED - COLD DRAWN WIRE FOR THE MANUFACTURE OF THREAD INSERTS - D <= 3 MM |
| PREN 4326 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-WH4102 (COCR28W20NI5V1) - FILLER METAL FOR WELDING - WIRE AND ROD |
| PREN 3668 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2301 (NICR21FE18MO9) - NON HEAT TREATED - FORGING STOCK - A OR D <= 250 MM |
| PREN 4086 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PD2101 (NICO14B5TI2) - NON HEAT TREATED - FORGING STOCK A OR D <= 360 MM |
| I.S. EN 2399:2008 | AEROSPACE SERIES - HEAT RESISTING STEEL FE-PA2601 (X4NICRTIMOV26-15) - R[M] >= 900 MPA - BARS FOR FORGED BOLTS - D <= 25 MM |
| DIN EN 3018:1997-12 (Draft) | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2801 (NICR16FE7TI3NBAL1) CONSUMABLE ELECTRODE REMELTED - COLD DRAWN WIREFOR THE MANUFACTURE OF THREAD INSERTS D <= 3 MM |
| 09/30201205 DC : DRAFT MAY 2009 | BS 2HR 203 - SPECIFICATION FOR NICKEL-CHROMIUM-TITANIUM HEAT-RESISTING ALLOY PLATE, SHEET AND STRIP (NICKEL BASE, CR 19.5, TI 0.4) |
| BS 4HR 601:2010 | Specification for nickel-chromium-titanium-aluminium heat-resisting alloy bar and wire (maximum diameter or minor sectional dimension of 30 mm) for the manufacture of fasteners (nickel base, Cr 19.5, Ti 2.2, Al 1.4) |
| UNI EN 4671 : 2011 | AEROSPACE SERIES - STEEL FE-PM1506 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1400 MPA |
| UNI EN 4670 : 2011 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| UNI EN 4382 : 2008 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - SOLUTION TREATED - SEAMLESS TUBES - FOR HYDRAULIC APPLICATION - D <= 50 MM, A <= 3 MM |
| UNI EN 4672 : 2012 | AEROSPACE SERIES - STEEL FE-PM1504 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| I.S. EN 4379:2007 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - SOLUTION TREATED, FORGING D[E] <= 200 MM |
| I.S. EN 2398:2008 | AEROSPACE SERIES - HEAT RESISTING STEEL FE-PA2601 (X6NICRTIMOV26-15) - R[M] >= 900 MPA - BARS FOR MACHINED BOLTS - D <= 25 MM |
| I.S. EN 4671:2010 | AEROSPACE SERIES - STEEL FE-PM1506 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1400 MPA |
| PREN 2183 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2301 (NICR21FE18MO9) - SOLUTION TREATED - FORGINGS - D[E] <= 200 MM |
| PREN 2197 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1701 (NICR15CO14AL5TI4MO4) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 200 MM - R[M] >= 1 250 MPA |
| PREN 2204 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH1303 (NICO20CR20MO5TI2AL) - VACUUM MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - PRECISION CASTING - D[E] <= 50 MM |
| PREN 4317 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - NON HEAT TREATED - FORGING STOCK - A OR D <= 200 MM |
| PREN 4222 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1305 (NICR22CO13MO9AI1) - AIR MELTED AND VACUUM REFINED - ANNEALED - SHEET AND STRIP - 0,25 MM <= A <= 3 MM |
| PREN 2119 : 200P1 | 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 |
| PREN 2178 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2501 (X4NICRMOTI43-13) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 200 MM |
| PREN 4371 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PD9001 (NICU31) - NON HEAT TREATED - BAR FOR RIVETS - D <= 10 MM |
| PREN 4380 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - SOLUTION TREATED - BAR AND SECTION - D[E] <= 200 MM |
| DIN EN 2959:2000-03 (Draft) | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1302 (NICR20CO13MO4TI3AL), SOLUTION TREATED AND COLD WORKED - BAR FOR FORGED FASTENERS 3 MM = D = 30 MM |
| I.S. EN 4670:2010 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| BS 2HR 650:2011 | Specification for high expansion heat-resisting steel bar and wire for the manufacture of bolts, studs, set screws and nuts (Ni 25.5, Cr 15, Ti 2, Mn 1.5, Mo 1.25, Si 0.7, V 0.3) (limiting ruling section 50 mm) |
| 09/30199931 DC : 0 | BS 2HR 4 - SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-ALUMINIUM-MOLYBDENUM-TITANIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CO 15, CR 14.2, AL 5, MO 4, TI 4) |
| BS EN 2399:2008 | Aerospace series. Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15). Rm ≥ 900 MPa. Bars for forged bolts. D ≤ 25 mm |
| BS 2HR 207:2009 | Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy plate, sheet and strip (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder) |
| 09/30201787 DC : 0 | BS 2HR 55 - SPECIFICATION FOR NICKEL-IRON-CHROMIUM-MOLYBDENUM-ALUMINIUM-TITANIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NI/CO 43.5, CR 16.5, MO 3.3, AL 1.2, TI 1.2, FE REMAINDER) |
| 09/30201210 DC : DRAFT MAY 2009 | BS 2HR 205 - SPECIFICATION FOR NICKEL-COPPER ALLOY SHEET AND STRIP: ANNEALED (NICKEL BASE, CU 31) |
| 09/30201778 DC : 0 | BS 2HR 52 - SPECIFICATION FOR HEAT-RESISTING STEEL BILLETS, BARS, FORGINGS AND PARTS (NI 25.5, CR 14.7, TI 1.8, MN 1.5, MO 1.2, V 0.3) |
| BS 3HR 202:2009 | Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy sheet and strip (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) |
| BS 2HR 205:2009 | Specification for nickel-copper alloy sheet and strip: annealed (nickel base, Cu 31) |
| BS 3HR2(2010) : 2010 : INC : AMD 2 : 2012 | AEROSPACE SERIES - SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CR 19.5, CO 18.0,TI 2.5, AL 1.5) |
| BS 2HR 402:2011 | Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy seamless tubes (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) |
| 09/30201213 DC : DRAFT MAY 2009 | BS 2HR 206 - SPECIFICATION FOR NICKEL-COBALT-CHROMIUM-MOLYBDENUM-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY PLATE, SHEET AND STRIP (NICKEL BASE, CO 20, CR 20, MO 5.9, TI 2.1, AL 0.5) |
| BS EN 4314:2007 | Aerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Non heat treated, forging stock a or D ? 250 mm |
| BS 2HR 6:2010 | Specification for nickel-chromium- iron-molybdenum-cobalt-tungsten heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 21.7, Fe 18.5, Mo 9, Co 1.5, W 0.6) |
| BS 3HR 504:2011 | Specification for nickel-chromium-titanium heat-resisting alloy bar and wire for rivets and rivets (Maximum diameter or minor sectional dimension 20 mm) (Nickel base, Cr 19.5, Ti 0.4) |
| BS 2HR 206:2009 | Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5) |
| 09/30199922 DC : 0 | BS 3HR 1 - SPECIFICATION FOR NICKEL-CHROMIUM-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CR 19.5, TI 2.2, AL 1.4) |
| 10/30230586 DC : 0 | BS 2HR 505 - SPECIFICATION FOR NICKEL-CHROMIUM-IRON-TITANIUM-NIOBIUM -ALUMINIUM HEAT RESISTING ALLOY ROUND WIRE FOR THREAD INSERTS WITH A MAXIMUM DIAMETER OF 2 MM (NICKEL BASE CR 15.5, FE 7.0, TI 2.5, NB/TA 0.95, AL 0.70) |
| BS 3HR 201:2009 | Specification for nickel-chromium- titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 2.2, Al 1.4) |
| BS 2HR 52:2010 | Specification for heat-resisting steel billets, bars, forgings and parts (Ni 25.5, Cr 14.7, Ti 1.8, Mn 1.5, Mo 1.2, V 0.3) |
| BS 2HR 55:2010 | Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder) |
| BS 3HR 503:2011 | Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy wire for thread inserts (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) (0.45 mm to 2 mm diameter) |
| 10/30230588 DC : 0 | BS 2HR 506 - SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-TITANIUM-ALUMINIUM HEAT RESISTING ALLOY WIRE: SOFTENED (NICKEL BASE, CR 19.5, CO 1.8, TI 2.5, AL 1.5) |
| 10/30230593 DC : 0 | BS 4HR 601 - SPECIFICATION FOR NICKEL-CHROMIUM-TITANIUM-ALUMINIUM HEAT RESISTING ALLOY BAR AND WIRE (MAXIMUM DIAMETER OR MINOR SECTIONAL DIMENSION 30 MM) FOR THE MANUFACTURE OF FASTENERS (NICKEL BASE, CR 19.5, TI 2.2, AL 1.4) |
| 09/30201200 DC : DRAFT MAY 2009 | BS 3HR 201 - SPECIFICATION FOR NICKEL-CHROMIUM-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY PLATE, SHEET AND STRIP (NICKEL BASE, CR 19.5, TI 2.2, AL 1.4) |
| BS 2HR 53:2010 | Specification for nickel-iron-chromium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (Ni/Co 42.5, Cr 12.5, Mo 5.8, Ti 3.0, Fe remainder) |
| BS 3HR2(2010) : 2010 : INC : AMD 1 : 2011 | AEROSPACE SERIES - SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CR 19.5, CO 18.0,TI 2.5, AL 1.5) |
| 09/30199933 DC : 0 | BS 2HR 5 - SPECIFICATION FOR NICKEL-CHROMIUM-TITANIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CR 19.5, TI 0.4) |
| BS 2HR 10:2010 | Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5) |
| BS 2HR 40:2010 | Specification for cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy billets, bars and forgings (cobalt base Cr 20, W 15, Ni 10, Mn 1.5) |
| BS EN 4670:2010 | Aerospace series. Steel FEPM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Softened. Forging stock. a or D ≤ 300 mm |
| BS 2HR 51:2010 | Specification for high expansion heat-resisting steel billets, bars, forgings and parts (Ni 25.5, Cr 15, Ti 2, Mn 1.5, Mo 1.25, Si 0.7, V 0.3) (Solution treated at 980 °C) |
| BS EN 4372:2009 | Aerospace series. Heat resisting nickel alloy with copper NI-PD9001 (NiCu31). Wire for solid rivets. D ≤ 10 mm |
| BS 3HR2(2010) : 2010 | AEROSPACE SERIES - SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CR 19.5, CO 18.0,TI 2.5, AL 1.5) |
| EN 4329:2001 | Aerospace series - Heat resisting alloy NI-WH0001 (NiCr20) - Filler metal for welding - Wire and rod |
| EN 4372:2009 | Aerospace series - Heat resisting nickel alloy with copper NI-PD9001 (NiCu31) - Wire for solid rivets - D ≤ 10 mm |
| EN 4384:2007 | Aerospace series - Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al) - Non heat treated - Remelting stock |
| EN 4379:2007 | Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De ≤ 200 mm |
| 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 2399 : 2008 | AEROSPACE SERIES - HEAT RESISTING STEEL FE-PA2601 (X4NICRTIMOV26-15) - R[M] >= 900 MPA - BARS FOR FORGED BOLTS - D <= 25 MM |
| EN 4338:2001 | Aerospace series - Heat resisting alloy NI-WH3902 (NiCr25Mo10C) - Filler metal for welding - Wire and rod |
| EN 3887:2001 | Aerospace series - Heat resisting alloy CO-WH4101 (CoCr20W15Ni) - Filler metal for welding |
| EN 4382:2006 | Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated - Seamless tubes - For hydraulic application - D ≤ 50 mm, a ≤ 3 mm |
| EN 4325:2001 | Aerospace series - Heat resisting alloy NI-WH1302 (NiCr20Co13Mo4Ti3AI) - Filler metal for welding - Wire and rod |
| EN 4317:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D ≤ 200 mm |
| EN 4383:2006 | Aerospace series - Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3) - Non heat treated - Remelting stock |
| EN 3895:2001 | Aerospace series - Heat resisting alloy NI-WH3901 (NiCr16Mo15) - Filler metal for welding |
| EN 3885:2001 | Aerospace series - Heat resisting alloy NI-WH3601 (NiCr22Mo9Nb4) - Filler metal for welding |
| EN 4670:2010 | Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Softened - Forging stock - a or D ≤ 300 mm |
| EN 3668:2006 | Aerospace series - Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) - Non heat treated - Forging stock - a or D ≤ 250 mm |
| EN 3888:2001 | Aerospace series - Heat resisting alloy CO-WH1402 (CoCr22Ni22W15) - Filler metal for welding |
| EN 3894:2001 | Aerospace series - Heat resisting alloy NI-WD3201 (NiMo25Fe6Cr5) - Filler metal for welding |
| EN 4327:2001 | Aerospace series - Heat resisting alloy CO-WH1401 (CoCr26Ni11W8) - Filler metal for welding - Wire and rod |
| EN 2398 : 2008 | Aerospace series - Heat resisting steel FE-PA2601 (X6NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for machined bolts - D ≤ 25 mm |
| EN 3671 : 2007 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - NON HEAT TREATED - FORGING STOCK - A OR D <= 250 MM |
| EN 4339:2001 | Aerospace series - Heat resisting alloy CO-WH4001 (CoCr29W9) - Filler metal for welding - Wire and rod |
| EN 4314:2007 | Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Non heat treated, forging stock a or D ≤ 250 mm |
| EN 3638:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Consumable electrode remelted - Solution and precipitation treated - Sheet, strip and plate - 0,5 mm ≤ a ≤ 10 mm |
| EN 4337:2001 | Aerospace series - Heat resisting alloy NI-WH8901 (NiCr16Ti3Mn3) - Filler metal for welding - Wire and rod |
| EN 4373:2007 | Aerospace series - Heat resisting alloy NI-PD9001 (NiCu31) - Annealed, seamless tube D ≤ 75 mm, a ≤ 3 mm |
| EN 4672:2011 | Aerospace series - Steel FE-PM1504 (X1CrNiMoAlTi12-10-2) - Vacuum induction melted and consumable electrode remelted - Softened - Forging stock - a or D ≤ 300 mm |
| EN 4671:2010 | Aerospace series - Steel FE-PM1506 (X1CrNiMoAlTi12-10-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 1400 MPa |
| 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 |
| EN 4326:2001 | Aerospace series - Heat resisting alloy CO-WH4102 (CoCr28W20Ni5V1) - Filler metal for welding - Wire and rod |
| EN 3886:2001 | Aerospace series - Heat resisting alloy NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - Filler metal for welding |
| I.S. EN 4372:2009 | AEROSPACE SERIES - HEAT RESISTING NICKEL ALLOY WITH COPPER NI-PD9001 (NICU31) - WIRE FOR SOLID RIVETS - D <= 10 MM |
| PREN 4573 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 100 MM |
| PREN 2405 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NI-PH2601 (NICR19FE19NB5MO3) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 200 MM |
| PREN 2663 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - SOLUTION TREATED - SHEET, STRIP AND PLATE - 0,2 MM <= A <= 10 MM |
| PREN 2185 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2301 (NICR21FE18MO9) - SOLUTION TREATED - SHEET, STRIP AND PLATE - 0,2 MM <= A <= 10 MM |
| PREN 2662 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - ANNEALED - SHEET, STRIP AND PLATE - 0,2 MM <= A <= 10 MM |
| PREN 4574 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 100 MM |
| PREN 3510 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2602 (X4NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 100 MM |
| PREN 4374 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1301 (NICR19CO18MO4TI3AL3) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 200 MM |
| PREN 2175 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2602 (X4NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - SHEET, STRIP AND PLATE - 0,5 MM <= A <= 10 MM - R[M] >= 850 MPA |
| PREN 4381 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - SOLUTION TREATED - SEAMLESS TUBES - FOR STRUCTURAL APPLICATION - D <= 50 MM, A <= 3 MM |
| PREN 4672 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1504 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| PREN 4339 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-WH4001 (COCR29W9) - FILLER METAL FOR WELDING - WIRE AND ROD |
| PREN 4572 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED - SHEET AND STRIP - A <= 3 MM |
| PREN 4315 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - A OR D <= 100 MM - R[M] >= 900 MPA |
| PREN 4327 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-WH1401 (COCR26NI11W8) - FILLER METAL FOR WELDING - WIRE AND ROD |
| PREN 3974 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH8001 (NICR20TI) - ANNEALED - SEAMLESS DRAWN CAPILLARY TUBE - 0,6 MM <= D <= 2,0 MM |
| PREN 4368 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CD1701 (NICO15CR10AL6TI5MO3) - NON HEAT TREATED - REMELTING STOCK |
| PREN 2030 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3501 (X105CRMO17) - HARDENED AND TEMPERED - BARS D[E] <= 150 MM |
| PREN 4670 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| PREN 4092 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3901 (NICR25MO10) - AIR MELTED AND VACUUM REFINED - ANNEALED - SHEET AND STRIP - 0,25 MM <= A <= 3 MM |
| PREN 2177 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2501 (X4NICRMOTI43-13) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 100 MM |
| PREN 2172 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 100 MM - R[M] >= 900 MPA |
| PREN 4096 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY - NI-CD1401 (NICO10210CR9A16TA3) - VACUUM MELTED - NON HEAT TREATED - REMELTING STOCK |
| PREN 4500-001 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 001: GENERAL RULES |
| BS 2HR 505:2010 | Specification for nickel-chromium-iron-titanium-niobium-aluminium heat-resisting alloy round wire with a maximum diameter of 2 mm for thread inserts (nickel base Cr 15.5, Fe 7.0, Ti 2.5, Nb/Ta 0.95, Al 0.70) |
| 09/30201771 DC : 0 | BS 2HR 40 - SPECIFICATION FOR COBALT-CHROMIUM-TUNGSTEN-NICKEL-MANGANESE HEAT-RESISTING ALLOY BILLETS, BARS AND FORGINGS (COBALT BASE CR 20, W 15, NI 10, MN 1.5) |
| BS 3HR 501:2011 | Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) |
| BS EN 4672:2011 | Aerospace series. Steel FE-PM1504 (X1CrNiMoAlTi12-10-2). Vacuum induction melted and consumable electrode remelted. Softened. Forging stock. a or D ≤ 300 mm |
| BS EN 3638:2007 | Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Consumable electrode remelted. Solution and precipitation treated. Sheet, strip and plate. 0,5 mm ≤ a ≤ 10 mm |
| 10/30230595 DC : 0 | BS 2HR 650 - SPECIFICATION FOR HIGH EXPANSION HEAT RESISTING STEEL BAR AND WIRE FOR THE MANUFACTURE OF BOLTS, STUDS, SET SCREWS AND NUTS (NI 25.5, CR 15, TI 2, MN 1.5, MO 1.25, SI 0.7, V 0.3) (LIMITING RULING SECTION 20 MM) |
| BS 2HR 203:2009 | Specification for nickel-chromium-titanium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 0.4) |
| BS EN 4384:2007 | Aerospace series. Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al). Non heat treated. Remelting stock |
| 09/30201203 DC : DRAFT MAY 2009 | BS 3HR 202 - SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY SHEET AND STRIP (NICKEL BASE, CR 19.5, CO 18.0, TI 2.5, AL 1.5) |
| 09/30201208 DC : DRAFT MAY 2009 | BS 2HR 204 - SPECIFICATION FOR NICKEL-CHROMIUM-IRON-MOLYBDENUM-COBALT-TUNGSTEN HEAT-RESISTING ALLOY SHEET AND STRIP (NICKEL BASE, CR 21.7, FE 18.5, MO 9, CO 1.5, W 0.6) |
| BS 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 |
| BS 2HR 4:2010 | Specification for nickel-chromium-cobalt-aluminium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 15, Co 14.2, Al 5, Mo 4, Ti 4) |
| BS EN 4317:2007 | Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Non heat treated, forging stock a or D ? 200 mm |
| PREN 2957 : 200P1 | AEROSPACE SERIES - METHOD OF PREPARATION OF FORGED SAMPLES |
| PREN 4500-001 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 001: GENERAL RULES |
| 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 |
| PREN 4700-002 : 200P3 | 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) |
| 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 |
| PREN 4700-004 : 200P2 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 4: WIRE |
| ISO 643:2012 | Steels Micrographic determination of the apparent grain size |
| PREN 4700-003 : 200P2 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 003: TUBE |
| PREN 6018 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - DETERMINATION OF DENSITY ACCORDING TO DISPLACEMENT METHOD |
| 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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