PREN 4500-001 : 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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 001: GENERAL RULES
Available format(s)
Hardcopy , PDF
Superseded date
01-03-2024
Language(s)
English
Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Rules for drafting and presentation
Annex A (normative) - Form 1
Annex B (normative) - Form 2
Annex C (normative) - Form 3
Annex D (normative) - Allocation of numbers to optional
lines
Describes the general rules for the drafting and presentation of metallic material standards for aerospace applications.
| DevelopmentNote |
Supersedes PREN 2500/1. (10/2002)
|
| DocumentType |
Draft
|
| Pages |
22
|
| ProductNote |
Superseded by EN 4500-001:2012
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| DIN EN 4500-001:2012-12 | Identical |
| 10/30239356 DC : 0 | Identical |
| 95/712874 DC : 0 | Identical |
| I.S. EN 2032-1:2002 | AEROSPACE SERIES - METALLIC MATERIALS - PART 1: CONVENTIONAL DESIGNATION |
| PREN 4500-6 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 6: SPECIFIC RULES FOR FILLER METALS FOR BRAZING |
| PREN 4500-004 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 004: SPECIFIC RULES FOR TITANIUM AND TITANIUM ALLOYS |
| BS 3TA11(2009) : 2009 | AEROSPACE SERIES - SPECIFICATION FOR BAR AND SECTION FOR MACHINING OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 900-1160 MPA) (LIMITING RULING SECTION 150 MM) |
| BS 2TA 38:2009 | Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon- carbon alloy (tensile strength 1250-1420 MPa) (limiting ruling section 25 mm) |
| BS 2TA 49:2009 | Specification for bar and section for machining of titanium-aluminium- molybdenum-tin-silicon-carbon alloy (Tensile strength 1000-1200 MPa) (Limiting ruling section over 100 mm up to and including 150 mm) |
| BS 2TA 58:2009 | Specification for plate of titanium-copper alloy (tensile strength 520-640 MPa) (maximum thickness 10 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) |
| 09/30193242 DC : 0 | BS 3TA 2 - SPECIFICATION FOR SHEET AND STRIP OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 390-540 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) |
| 09/30181191 DC : 0 | BS 2B 23 - SPECIFICATION FOR COPPER-ALUMINIUM-NICKEL-IRON ALLOY RODS, SECTIONS, FORGING STOCK AND FORGINGS |
| BS 2B 26:2001 | Copper-nickel-silicon alloy rods, sections and parts (solution treated, cold worked and precipitation treated) |
| 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 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 2B 30:2001 | Copper-beryllium alloy strip, foil and parts (solution treated, cold rolled: half hard and precipitation treated) |
| 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 3B 33:2009 | Specification for copper-beryllium alloy wire(solution treated and precipitation treated) |
| 09/30181209 DC : 0 | BS 3B 32 - SPECIFICATION FOR COPPER-BERYLLIUM ALLOY RODS AND SECTIONS (SOLUTION TREATED AND PRECIPITATION TREATED) |
| 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 2TA 48:2009 | Specification for forgings of titanium-aluminium-molybdenum- tin-silicon-carbon alloy (tensile strength 1050-1200 MPa) (limiting ruling section 100 mm) |
| 09/30181197 DC : 0 | BS 3B 26 - SPECIFICATION FOR COPPER-NICKEL-SILICON ALLOY RODS, SECTIONS AND PARTS (SOLUTION TREATED, COLD WORKED AND PRECIPITATION TREATED) |
| 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) |
| 09/30193254 DC : 0 | BS 3TA 13 - SPECIFICATION FOR FORGINGS OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 900-1160 MPA) (LIMITING RULING SECTION 150 MM) |
| 09/30181193 DC : 0 | BS 2B 24 - SPECIFICATION FOR COPPER-TIN-PHOSPHOROUS ALLOY RODS AND SECTIONS |
| 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) |
| 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) |
| BS 2TA 41:2009 | Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm) |
| PREN 6071 : 200P1 | AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PLATE |
| BS 3TA 12:2009 | Specification for forging stock of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 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) |
| BS 2TA 40:2009 | Specification for bar for machining of titanium- aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm) |
| BS 2TA 42:2009 | Specification for forgings of titanium-aluminium- molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm) |
| 10/30239357 DC : 0 | BS EN 4500-3 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 3: SPECIFIC RULES FOR HEAT RESISTING ALLOYS |
| 09/30181199 DC : 0 | BS 3B 27 - SPECIFICATION FOR COPPER-ZINC-ALUMINIUM-NICKEL-SILICON ALLOY TUBE |
| 09/30193181 DC : 0 | BS 2TA 46 - SPECIFICATION FOR BAR AND SECTION FOR MACHINING OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1050-1220 MPA) (LIMITING RULING SECTION OVER 25 MM UP TO AND INCLUDING 100 MM) |
| 09/30193171 DC : 0 | BS 2TA 39 - SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1250-1420 MPA) (LIMITING RULING SECTION 25 MM) |
| 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) |
| 09/30181211 DC : 0 | BS 3B 33 - SPECIFICATION FOR COPPER-BERYLLIUM ALLOY WIRE (SOLUTION TREATED AND PRECIPITATION TREATED) |
| PREN 2032-001 : 200P5 | AEROSPACE SERIES - METALLIC MATERIALS - PART 001: CONVENTIONAL DESIGNATION |
| 09/30193240 DC : 0 | BS 3TA 1 - SPECIFICATION FOR SHEET AND STRIP OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 290-420 MPA) |
| BS 3TA 1:2009 | Specification for sheet and strip of commercially pure titanium (tensile strength 290-420 MPa) |
| 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) |
| 09/30193535 DC : 0 | BS 2TA 50 - SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY - TENSILE STRENGTH 1000-1200 MPA - LIMITING RULING SECTION OVER 100 MM UP TO AND INCLUDING 150 MM |
| 09/30193250 DC : 0 | BS 3TA 11 - SPECIFICATION FOR BAR AND SECTION FOR MACHINING OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 900-1160 MPA) (LIMITING RULING SECTION 150 MM) |
| 09/30181203 DC : 0 | BS 3B 29 - SPECIFICATION FOR COPPER-BERYLLIUM ALLOY STRIP AND FOIL (SOLUTION TREATED, COLD ROLLED: QUARTER HARD AND PRECIPITATION TREATED) |
| PREN 4500-2 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 2: SPECIFIC RULES FOR ALUMINIUM, ALUMINIUM ALLOYS AND MAGNESIUM ALLOYS |
| 11/30248021 DC : 0 | AEROSPACE SERIES - COPPER ALLOY CUBE 1.9 - SOLUTION TREATED, COLD WORKED TO [1/2] HARD AND PRECIPITATION TREATED - BAR - 5 MM <= A OR D <= 190 MM - R[M] >= 1220 MPA |
| 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) |
| BS S 164:2002 | 1 % Chromium-molybdenum steel billets, bars, forgings and parts. (1150 to 1300 MPa: Limiting ruling section 16 mm) (Suitable for welding) |
| 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 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) |
| BS 3B 25:2009 | Specification for copper-nickel-silicon alloy rods, bars, sections, forging stock and forgings (heat treated) |
| 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) |
| BS 2TA 47:2009 | Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 MPa) (limiting ruling section 100 mm) |
| 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 2B 28:2001 | Copper-beryllium alloy strip, foil and parts (solution treated and precipitation treated) |
| BS 3B 29:2009 | Specification for copper-beryllium alloy strip and foil (solution treated, cold rolled: quarter hard and precipitation treated) |
| 09/30193175 DC : 0 | BS 2TA 41 - SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1205-1375 MPA) (LIMITING RULING SECTION OVER 25 MM UP TO AND INCLUDING 75 MM) |
| 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 2TA 45:2009 | Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1100-1280 MPa) (limiting ruling section 25 mm) |
| 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) |
| BS 3TA 2:2009 | Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 MPa) |
| BS 3B 31:2009 | Specification for copper-beryllium alloy strip and foil (solution treated, cold rolled: full hard and precipitation treated) |
| BS 2TA 39:2009 | Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 MPa) (limiting ruling section 25 mm) |
| BS 2B 31:2001 | Copper-beryllium alloy strip, foil and parts (solution treated, cold rolled: full hard and precipitation treated) |
| 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 2B 29:2001 | Copper-beryllium alloy strip, foil and parts (solution treated, cold rolled: quarter hard and precipitation treated) |
| 09/30193179 DC : 0 | BS 2TA 45 - SPECIFICATION FOR BAR AND SECTION OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1100-1280 MPA) (LIMITING RULING SECTION 25 MM) |
| 09/30193183 DC : 0 | BS 2TA 47 - SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1050-1220 MPA) (LIMITING RULING SECTION 100 MM) |
| 09/30193537 DC : 0 | BS 2TA 51 - SPECIFICATION FOR FORGINGS OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY - TENSILE STRENGTH 1000-1200 MPA - LIMITING RULING SECTION OVER 100 MM UP TO AND INCLUDING 150 MM |
| 09/30193177 DC : 0 | BS 2TA 42 - SPECIFICATION FOR FORGINGS OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1205-1375 MPA) (LIMITING RULING SECTION OVER 25 MM UP TO AND INCLUDING 75 MM) |
| BS 2B 32:2001 | Copper-beryllium alloy rods, sections and parts (solution treated and precipitation treated) |
| 09/30193543 DC : 0 | BS 2TA 57 - SPECIFICATION FOR PLATE OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY - TENSILE STRENGTH 1030-1220 MPA - MAXIMUM THICKNESS 65 MM |
| BS S 206:1999 | Chromium-nickel-aluminium corrosion resisting steel (precipitation hardening) rod, cold drawn wire and springs |
| 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 2TA 50:2009 | Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 MPa) (limiting ruling section over 100 mm up to and including 150 mm) |
| 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 2TA 56:2009 | Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm) |
| 09/30193244 DC : 0 | BS 3TA 6 - SPECIFICATION FOR SHEET AND STRIP OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 570-730 MPA) |
| BS 3TA 21:2009 | Specification for sheet and strip of titanium-copper alloy (tensile strength 540-700 MPa) |
| 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) |
| 09/30193541 DC : 0 | BS 2TA 56 - SPECIFICATION FOR PLATE OF TITANIUM-ALUMINIUM-VANADIUM ALLOY - TENSILE STRENGTH 895-1150 MPA - MAXIMUM THICKNESS 100 MM |
| 09/30193173 DC : 0 | BS 2TA 40 - SPECIFICATION FOR BAR FOR MACHINING OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1205-1375 MPA) (LIMITING RULING SECTION OVER 25 MM UP TO AND INCLUDING 75 MM) |
| BS 2B 24:2009 | Specification for copper-tin-phosphorous alloy rods and sections |
| 09/30193547 DC : 0 | BS 2TA 59 - SPECIFICATION FOR SHEET OF TITANIUM-ALUMINIUM-VANADIUM ALLOY - TENSILE STRENGTH 920-1180 MPA |
| 11/30248019 DC : 0 | AEROSPACE SERIES - COPPER ALLOY CUBE 1.9 - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - 5 MM <= A OR D <= 190 MM - R[M] >= 1050 MPA |
| 09/30193248 DC : 0 | BS 3TA 10 - SPECIFICATION FOR SHEET OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 960-1270 MPA) |
| BS 2TA 51:2009 | Specification for forgings of titanium-aluminium- molybdenum-tin-silicon alloy (tensile strength 1000-1200 MPa) (limiting ruling section over 100 mm up to and including 150 mm) |
| 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 2B 27:2002 | Copper-zinc-aluminium-nickel-silicon alloy tube |
| BS 3TA 13:2009 | Specification for forgings of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm) |
| BS 3TA 10:2009 | Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 960-1270 MPa) |
| 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) |
| BS 2B 23:2009 | Specification for copper-aluminium-nickel-iron alloy rods, bars, sections, forging stock and forgings |
| 09/30193246 DC : 0 | BS 3TA 7 - SPECIFICATION FOR BAR AND SECTION OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 540-740 MPA) |
| 09/30193545 DC : 0 | BS 2TA 58 - SPECIFICATION FOR PLATE OF TITANIUM-COPPER ALLOY - TENSILE STRENGTH 520-640 MPA - MAXIMUM THICKNESS 10 MM |
| 09/30193256 DC : 0 | BS 3TA 21 - SPECIFICATION FOR SHEET AND STRIP OF TITANIUM-COPPER ALLOY (TENSILE STRENGTH 540-700 MPA) |
| BS 3B 30:2009 | Specification for copper-beryllium alloy strip and foil (solution treated, cold rolled: half hard and precipitation treated) |
| 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 3TA 6:2009 | Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 MPa) |
| 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 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 2TA 52:2009 | Specification for sheet and strip of titanium- copper alloy (tensile strength 690-920 MPa) |
| 09/30181201 DC : 0 | BS 3B 28 - SPECIFICATION FOR COPPER-BERYLLIUM ALLOY STRIP AND FOIL (SOLUTION TREATED AND PRECIPITATION TREATED) |
| 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) |
| 09/30193185 DC : 0 | BS 2TA 48 - SPECIFICATION FOR FORGINGS OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1050-1200 MPA) (LIMITING RULING SECTION 100 MM) |
| 09/30193252 DC : 0 | BS 3TA 12 - SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 900-1160 MPA) (LIMITING RULING SECTION 150 MM) |
| EN 2032-1 : 2001 | AEROSPACE SERIES - METALLIC MATERIALS - PART 1: CONVENTIONAL DESIGNATION |
| PREN 4500-005 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 005: SPECIFIC RULES FOR STEELS |
| PREN 4500-003 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 003: SPECIFIC RULES FOR HEAT RESISTING SLLOYS |
| BS 3B 27:2009 | Specification for copper-zinc-aluminium-nickel-silicon alloy tube |
| 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) |
| 11/30248020 DC : 0 | AEROSPACE SERIES - COPPER ALLOY CUBE 1.9 - SOLUTION TREATED, COLD WORKED TO [1/4] HARD AND PRECIPITATION TREATED - BAR - 5 MM <= A OR D <= 190 MM - R[M] >= 1100 MPA |
| 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 2TA 46:2009 | Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 MPa) (limiting ruling section over 25 mm up to and including 100 mm) |
| BS 2TA 59:2009 | Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 920-1180 MPa) |
| BS 2TA 57:2009 | Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (thickness over 50 mm up to and including 65 mm) |
| 09/30193169 DC : 0 | BS 2TA 38 - SPECIFICATION FOR BAR FOR MACHINING OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1250-1420 MPA) (LIMITING RULING SECTION 25 MM) |
| 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 3TA 7:2009 | Specification for bar and section for machining of commercially pure titanium (tensile strength 540-740 MPa) |
| 10/30239500 DC : 0 | BS EN 4500-4 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 4: SPECIFIC RULES FOR TITANIUM AND TITANIUM ALLOYS |
| 09/30193539 DC : 0 | BS 2TA 52 - SPECIFICATION FOR SHEET AND STRIP OF TITANIUM-COPPER ALLOY - TENSILE STRENGTH 690-920 MPA |
| 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 3B 32:2009 | Specification for copper-beryllium alloy rods, bars and sections (solution treated and precipitation treated) |
| 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 7S 80:2002 | High chromium-nickel corrosion resisting steel forging stock, bars, forgings and parts (880 to 1080 MPa: limiting ruling section 100 mm) |
| 09/30193187 DC : 0 | BS 2TA 49 - SPECIFICATION FOR BAR AND SECTION FOR MACHINING OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1000-1200 MPA) (LIMITING RULING SECTION OVER 100 MM UP TO AND INCLUDING 150 MM) |
| 09/30181207 DC : 0 | BS 3B 31 - SPECIFICATION FOR COPPER-BERYLLIUM ALLOY STRIP AND FOIL (SOLUTION TREATED, COLD ROLLED: FULL HARD AND PRECIPITATION TREATED) |
| 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 2B 25:2001 | Copper-nickel-silicon alloy rods, sections, forging stock, forgings and parts (heat treated) |
| 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 2B 33:2001 | Copper-beryllium alloy wire and springs (solution treated and precipitation treated) |
| 09/30181195 DC : 0 | BS 3B 25 - SPECIFICATION FOR COPPER-NICKEL-SILICON ALLOY RODS, SECTIONS, FORGING STOCK AND FORGINGS (HEAT TREATED) |
| BS 3B 28:2009 | Specification for copper-beryllium alloy strip and foil (solution treated and precipitation treated) |
| ISO 80000-4:2006 | Quantities and units Part 4: Mechanics |
| PREN 4500-004 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 004: SPECIFIC RULES FOR TITANIUM AND TITANIUM ALLOYS |
| EN 2032-2 : 1994 | AEROSPACE SERIES - METALLIC MATERIALS - CODING OF METALLURGICAL CONDITION IN DELIVERY CONDITION |
| PREN 4500-6 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 6: SPECIFIC RULES FOR FILLER METALS FOR BRAZING |
| PREN 2043 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - GENERAL REQUIREMENTS FOR SEMI-FINISHED PRODUCT QUALIFICATION (EXCLUDING FORGINGS AND CASTINGS) |
| ISO 80000-3:2006 | Quantities and units Part 3: Space and time |
| ISO 80000-2:2009 | Quantities and units Part 2: Mathematical signs and symbols to be used in the natural sciences and technology |
| EN 2032-1 : 2001 | AEROSPACE SERIES - METALLIC MATERIALS - PART 1: CONVENTIONAL DESIGNATION |
| ISO 80000-1:2009 | Quantities and units — Part 1: General |
| PREN 4259 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - DEFINITION OF GENERAL TERMS |
| PREN 4500-003 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 003: SPECIFIC RULES FOR HEAT RESISTING SLLOYS |
| 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 |
| PREN 4500-2 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 2: SPECIFIC RULES FOR ALUMINIUM, ALUMINIUM ALLOYS AND MAGNESIUM ALLOYS |
| ISO 80000-5:2007 | Quantities and units Part 5: Thermodynamics |
| PREN 4500-005 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 005: SPECIFIC RULES FOR STEELS |
| ISO 80000-10:2009 | Quantities and units Part 10: Atomic and nuclear physics |
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