PREN 4500-004 : 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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 004: SPECIFIC RULES FOR TITANIUM AND TITANIUM ALLOYS
Available format(s)
Hardcopy , PDF
Language(s)
English
Superseded date
03-01-2024
Superseded by
$260.90
Including GST where applicable
Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Rules for drafting and presentation
Bibliography
Describes the specifies rules for the drafting and presentation of titanium and titanium alloy material standards for aerospace applications.
| DevelopmentNote |
Supersedes PREN 2500/4. (10/2002) To be used in conjunction with PREN 4500-001. (08/2003)
|
| DocumentType |
Draft
|
| Pages |
19
|
| ProductNote |
Superseded by EN 4500-004:2012
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| NF EN 4500-004 : 2013 | Identical |
| DIN EN 4500-004:2012-12 | Identical |
| 10/30239500 DC : 0 | Identical |
| BS EN 3311:2009 | Aerospace series. Titanium alloy TI-P64001 (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 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 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 |
| 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 |
| 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) |
| 09/30193242 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 2TA 48:2009 | Specification for forgings of titanium-aluminium-molybdenum- tin-silicon-carbon alloy (tensile strength 1050-1200 MPa) (limiting ruling section 100 mm) |
| 09/30193254 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 De ≤ 150 mm |
| BS EN 4675:2011 | Aerospace series. Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe). Rm ≥ 1 300 MPa. Bars. De < 110 mm |
| 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) |
| I.S. EN 3311:2009 | AEROSPACE SERIES - TITANIUM ALLOY TIP64001 (TI-6AL-4V) - ANNEALED - BAR FOR MACHINING - D < 110 MM |
| 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 3322 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P65001 - SOLUTION TREATED AND AGED - GRADE 1 - FORGINGS - D[E] <= 75 MM |
| BS 3TA 12:2009 | Specification for forging stock of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm) |
| 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 |
| 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) |
| BS EN 3456:2012 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Sheet and strip, hot rolled. a ≤ 6 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) |
| 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 |
| BS EN 3355:2012 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Extruded section. De ≤ 150 mm. 900 MPa ≤ Rm ≤ 1 160 MPa |
| 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) |
| 09/30193535 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) |
| EN 3310:2011 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Not heat treated - Forging stock, for annealed forgings - De ≤ 360 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 |
| 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. De ≤ 360 mm |
| 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) |
| 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 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 3TA 2:2009 | Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 MPa) |
| 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) |
| 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 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) |
| 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 2TA 56:2009 | Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm) |
| BS EN 4685:2011 | 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 3TA 21:2009 | 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 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) |
| 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 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) |
| 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 3TA 6:2009 | 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 2TA 52:2009 | 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 - Rm ≥ 1 240 MPa |
| 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 |
| 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 |
| 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 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 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 |
| 09/30210353 DC : 0 | BS EN 3464 EDP3 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - PLATE - 6 MM < A <= 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) |
| EN ISO 12737:2010 | Metallic materials - Determination of plane-strain fracture toughness (ISO 12737:2010) |
| 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 (ISO 4288:1996) |
| 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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Users cannot be edited or removed once added to your Multi user PDF.