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  • PREN 4500-004 : 200P2

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 004: SPECIFIC RULES FOR TITANIUM AND TITANIUM ALLOYS

    Available format(s):  Hardcopy, PDF

    Superseded date:  01-10-2012

    Language(s):  English

    Published date: 

    Publisher:  Aerospace & Defence Industries Association of Europe

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

    Foreword
    Introduction
    1 Scope
    2 Normative references
    3 Terms and definitions
    4 Rules for drafting and presentation
    Bibliography

    Abstract - (Show below) - (Hide below)

    Describes the specifies rules for the drafting and presentation of titanium and titanium alloy material standards for aerospace applications.

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

    Comment Closes On
    Development Note Supersedes PREN 2500/4. (10/2002) To be used in conjunction with PREN 4500-001. (08/2003)
    Document Type Draft
    Publisher Aerospace & Defence Industries Association of Europe
    Status Superseded
    Superseded By
    Supersedes

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

    I.S. EN 3310:2011 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - D[E] <= 360 MM
    BS EN 3311 : 2009 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - BAR FOR MACHINING - D < 110 MM
    I.S. EN 3311:2009 AEROSPACE SERIES - TITANIUM ALLOY TIP64001 (TI-6AL-4V) - ANNEALED - BAR FOR MACHINING - D < 110 MM
    I.S. EN 4685:2011 AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA
    PREN 3120 : 200P3 AEROSPACE SERIES - TITANIUM ALLOY TI-P64003 - COLD WORKED AND STRESS RELIEVED - SEAMLESS TUBE FOR PRESSURE SYSTEMS - 4 MM <= D <= 51 MM - 690 MPA <= R[M] <= 1030 MPA
    PREN 3351 : 200P3 AEROSPACE SERIES - TITANIUM ALLOY TI-4AL-4MO-2SN - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 150MM
    PREN 3352 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-C64001 - INVESTMENT CASTING - HOT ISOSTATIC PRESSED - A < 30 MM - R[M] >= 880 MPA
    PREN 3312 : 200P3 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - FORGINGS - D[E] <= 150 MM
    PREN 3456 : 200P3 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM
    PREN 3321 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-P65001 - AS FORGED - GRADE 1 FORGING STOCK, FOR SOLUTION TREATED AND AGED FORGINGS - A OR D <= 360 MM
    PREN 3354 : 200P4 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - SHEET FOR SUPERPLASTIC FORMING - A <= 6 MM
    PREN 3355 : 200P3 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - EXTRUDED SECTION - D[E] <= 150 MM - 900 MPA <= R[M] <= 1160 MM MPA
    PREN 3315 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 75 MM
    PREN 3528 : 200P2 AEROSPACE SERIES - STEEL FE-PM2701 (X2NICOMO18-8-5) - VACUUM INDUCTION MELTED AND VACUUM ARC REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 150 MM - 1750 MPA <= R[M] <= 2000 MPA
    PREN 3378 : 200P2 AEROSPACE SERIES - TITANIUM TI-P99002 - ANNEALED - WIRE FOR RIVET - 1,6 MM <= D <= 10 MM
    PREN 3310 : 200P3 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - D[E] <= 360 MM
    PREN 3464 : 200P3 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - PLATE - 6 MM < A <= 100 MM
    PREN 3322 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-P65001 - SOLUTION TREATED AND AGED - GRADE 1 - FORGINGS - D[E] <= 75 MM
    PREN 3813 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - D[E] <= 50 MM
    PREN 3460 : 200P2 AEROSPACE SERIES - TITANIUM TI-P99002 - ANNEALED - BAR FOR MATCHING - A OR D <= 150 MM - R[M] >= 390 MPA
    PREN 3467 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-C64001 - NOT HEAT TREATED - REMELTING STOCK - D[E] <= 300 MM
    PREN 4685 : 200P1 AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA
    PREN 4342 : 200P1 AEROSPACE SERIES - TITANIUM TI-W99001 - FILLER METAL FOR WELDING - WIRE AND ROD
    I.S. EN 3456:2012 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM
    PREN 4675 : 200P1 AEROSPACE SERIES - TITANIUM TI-P63002 (TI5AL5MO5V3CR0,4FE) - R[M] >= 1300 MPA - BARS - D[E] <= 100 MM
    PREN 4500-001 : 200P2 AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 001: GENERAL RULES
    BS 3TA12(2009) : 2009 SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 900-1160 MPA) (LIMITING RULING SECTION 150 MM)
    BS EN 3355 : 2012 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - EXTRUDED SECTION - D[E] <= 150 MM - 900 MPA <= R[M] <= 1160 MPA
    I.S. EN 3464:2012 AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - PLATE - 6 MM < A <= 100 MM
    I.S. EN 4675:2011 AEROSPACE SERIES - TITANIUM TI-P63002 (TI5AL5MO5V3CR0.4FE) - R[M] >= 1300 MPA - BARS - D[E] < 110 MM
    I.S. EN 3355:2012 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - EXTRUDED SECTION - D[E] <= 150 MM - 900 MPA <= R[M] <= 1160 MPA
    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)
    I.S. EN 3351:2012 AEROSPACE SERIES - TITANIUM ALLOY TI-4AL-4MO-2SN - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 150 MM
    I.S. EN 3459:2010 AEROSPACE SERIES - TITANIUM ALLOY TI-P63001 (TI-4AL-4MO-2SN) - SOLUTION TREATED AND AGED - PLATE - 6 MM < A <= 50 MM
    BS 2TA40(2009) : 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 2TA42(2009) : 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)
    BS EN 3456 : 2012 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM
    BS 2TA38(2009) : 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 2TA49(2009) : 2009 SPECIFICATION FOR BAR AND SECTION FOR MACHINING 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 2TA58(2009) : 2009 SPECIFICATION FOR PLATE OF TITANIUM-COPPER ALLOY (TENSILE STRENGTH 520-640 MPA) (MAXIMUM THICKNESS 10 MM)
    09/30193242 DC : 0 BS 3TA 2 - SPECIFICATION FOR SHEET AND STRIP OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 390-540 MPA)
    09/30207946 DC : 0 BS EN 3312 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - FORGINGS - D[E] <= 150 MM
    BS 2TA46(2009) : 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 2TA59(2009) : 2009 SPECIFICATION FOR SHEET OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 920-1180 MPA)
    BS 2TA57(2009) : 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 3TA7(2009) : 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
    09/30210353 DC : 0 BS EN 3464 EDP3 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - PLATE - 6 MM < A <= 100 MM
    BS EN 3464 : 2012 AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - PLATE - 6 MM < A <= 100 MM
    BS EN 3310 : 2011 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - D[E] <= 360 MM
    BS 2TA47(2009) : 2009 SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY (TENSILE STRENGTH 1050-1220 MPA) (LIMITING RULING SECTION 100 MM)
    BS EN 3459 : 2010 AEROSPACE SERIES - TITANIUM ALLOY TI-P63001 (TI-4AL-4MO-2SN) - SOLUTION TREATED AND AGED - PLATE - 6 MM < A <= 50 MM
    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 2TA45(2009) : 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 3TA2(2009) : 2009 SPECIFICATION FOR SHEET AND STRIP OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 390-540 MPA)
    BS 2TA39(2009) : 2009 SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1250-1420 MPA) (LIMITING RULING SECTION 25 MM)
    09/30193240 DC : 0 BS 3TA 1 - SPECIFICATION FOR SHEET AND STRIP OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 290-420 MPA)
    BS 3TA1(2009) : 2009 SPECIFICATION FOR SHEET AND STRIP OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 290-420 MPA)
    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)
    09/30193181 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)
    BS 2TA48(2009) : 2009 SPECIFICATION FOR FORGINGS OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY (TENSILE STRENGTH 1050-1200 MPA) (LIMITING RULING SECTION 100 MM)
    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)
    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 EN 3312 : 2012 AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - FORGINGS D[E] <= 150 MM
    BS EN 4675 : 2011 AEROSPACE SERIES - TITANIUM TI-P63002 (TI5AL5MO5V3CR0.4FE) - R[M] >= 1300 MPA - BARS - D[E] < 110 MM
    BS 2TA41(2009) : 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)
    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)
    09/30193179 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)
    09/30201382 DC : 0 BS EN 4685 - AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA
    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)
    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 2TA50(2009) : 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)
    09/30209898 DC : DRAFT SEP 2009 BS EN 3813 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - D[E] <= 50 MM
    BS 2TA56(2009) : 2009 SPECIFICATION FOR PLATE OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 895-1150 MPA) (MAXIMUM THICKNESS 100 MM)
    BS EN 4685:2011 (published 2011-07) Aerospace series. Titanium Ti10V2Fe3Al. Bars. D < 110 mm. Rm ≥ 1240 MPa
    09/30193244 DC : 0 BS 3TA 6 - SPECIFICATION FOR SHEET AND STRIP OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 570-730 MPA)
    BS 3TA21(2009) : 2009 SPECIFICATION FOR SHEET AND STRIP OF TITANIUM-COPPER ALLOY (TENSILE STRENGTH 540-700 MPA)
    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)
    09/30193547 DC : 0 BS 2TA 59 - SPECIFICATION FOR SHEET OF TITANIUM-ALUMINIUM-VANADIUM ALLOY - TENSILE STRENGTH 920-1180 MPA
    09/30193248 DC : 0 BS 3TA 10 - SPECIFICATION FOR SHEET OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 960-1270 MPA)
    BS 2TA51(2009) : 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)
    09/30208131 DC : DRAFT AUG 2009 BS EN 3354 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET FOR SUPERPLASTIC FORMING - A <= 6 MM
    BS 3TA13(2009) : 2009 SPECIFICATION FOR FORGINGS OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 900-1160 MPA) (LIMITING RULING SECTION 150 MM)
    BS 3TA10(2009) : 2009 SPECIFICATION FOR SHEET OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 960-1270 MPA)
    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
    09/30207945 DC : 0 BS EN 3310 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - A OR D <= 360 MM
    09/30193256 DC : 0 BS 3TA 21 - SPECIFICATION FOR SHEET AND STRIP OF TITANIUM-COPPER ALLOY (TENSILE STRENGTH 540-700 MPA)
    BS 3TA6(2009) : 2009 SPECIFICATION FOR SHEET AND STRIP OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 570-730 MPA)
    09/30210361 DC : 0 BS EN 3456 EDP3 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM
    BS 2TA52(2009) : 2009 SPECIFICATION FOR SHEET AND STRIP OF TITANIUM-COPPER ALLOY (TENSILE STRENGTH 690-920 MPA)
    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 3456:2012 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM
    EN 3355 : 2012 Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Extruded section - De ≤ 150 mm - 900 MPa ≤ Rm ≤ 1 160 MPa
    EN 3464:2012 AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - PLATE - 6 MM < A <= 100 MM
    EN 3892 : 2001 AEROSPACE SERIES - TITANIUM ALLOY TI-W64001 - FILLER METAL FOR WELDING
    EN 3893 : 2001 AEROSPACE SERIES - TITANIUM ALLOY TI-W19001 - FILLER METAL FOR WELDING
    EN 4342 : 2001 AEROSPACE SERIES - TITANIUM TI-W99001 - FILLER METAL FOR WELDING - WIRE AND ROD
    EN 3311 : 2009 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - BAR FOR MACHINING - D < 110 MM
    EN 3459 : 2010 AEROSPACE SERIES - TITANIUM ALLOY TI-P63001 (TI-4AL-4MO-2SN) - SOLUTION TREATED AND AGED - PLATE - 6 MM < A <= 50 MM
    EN 4685 : 2011 AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA
    EN 3310 : 2011 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - D[E] <= 360 MM

    Standards Referencing This Book - (Show below) - (Hide below)

    EN ISO 12737:2010 METALLIC MATERIALS - DETERMINATION OF PLANE-STRAIN FRACTURE TOUGHNESS
    PREN 4800-004 : 200P2 AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 4: WIRE
    EN 2545-1 : 1995 AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOY REMELTING STOCK AND CASTINGS - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS
    EN ISO 8493 : 2004 Metallic materials - Tube - Drift-expanding test (ISO 8493:1998)
    EN 2003-009 : 2007 AEROSPACE SERIES - TEST METHODS - TITANIUM AND TITANIUM ALLOYS - PART 009: DETERMINATION OF SURFACE CONTAMINATION
    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
    PREN 4050-1 : 200P1 AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION BARS, PLATES, FORGING STOCK AND FORGINGS - GENERAL INFORMATION
    EN ISO 4288 : 1997 GEOMETRICAL PRODUCT SPECIFICATIONS (GPS) - SURFACE TEXTURE: PROFILE METHOD - RULES AND PROCEDURES FOR THE ASSESSMENT OF SURFACE TEXTURE
    EN 3114-002 : 2007 Aerospace series - Test method - Microstructure of (α + β) titanium alloy wrought products - Part 002: Microstructure of bars, sections, forging stock and forgings
    EN ISO 643:2012 STEELS - MICROGRAPHIC DETERMINATION OF THE APPARENT GRAIN SIZE (ISO 643:2012)
    ISO 9649:2016 Metallic materials Wire Reverse torsion test
    PREN 4800-002 : 200P2 AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 2: BAR AND SECTION
    PREN 2043 : 200P1 AEROSPACE SERIES - METALLIC MATERIALS - GENERAL REQUIREMENTS FOR SEMI-FINISHED PRODUCT QUALIFICATION (EXCLUDING FORGINGS AND CASTINGS)
    ISO 8493:1998 Metallic materials Tube Drift-expanding test
    ISO 12737:2010 Metallic materials Determination of plane-strain fracture toughness
    PREN 4800-001 : 200P2 AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 1: PLATE, SHEET AND STRIP
    EN 3684 : 2007 Aerospace series - Test methods - Titanium alloy wrought products - Determination of β transus temperature - Metallographic method
    PREN 4800-005 : 200P2 AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 5: FORGING STOCK
    EN 2032-1 : 2001 AEROSPACE SERIES - METALLIC MATERIALS - PART 1: CONVENTIONAL DESIGNATION
    PREN 3322 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-P65001 - SOLUTION TREATED AND AGED - GRADE 1 - FORGINGS - D[E] <= 75 MM
    ISO 643:2012 Steels Micrographic determination of the apparent grain size
    PREN 4800-003 : 200P2 AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 3: TUBE
    ISO 8492:2013 Metallic materials Tube Flattening test
    ISO 7802:2013 Metallic materials Wire Wrapping test
    EN ISO 8492:2013 METALLIC MATERIALS - TUBE - FLATTENING TEST (ISO 8492:2013)
    EN 2954-002 : 2010 AEROSPACE SERIES - MACROSTRUCTURE OF TITANIUM AND TITANIUM ALLOY WROUGHT PRODUCTS - PART 002: MACROSTRUCTURE OF BAR, SECTION, FORGING STOCK AND FORGINGS
    EN 4258 : 1998 AEROSPACE SERIES - METALLIC MATERIALS - GENERAL ORGANIZATION OF STANDARDIZATION - LINKS BETWEEN TYPES OF EN STANDARDS AND THEIR USE
    PREN 4800-006 : 200P2 AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 6: PRE-PRODUCTION AND PRODUCTION FORGINGS
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