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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Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 001: GENERAL RULES

Available format(s)

Hardcopy , PDF

Superseded date

03-01-2024

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Superseded by EN 4500-001:2012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Superseded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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