SAE ARP 982 : 2016
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
MINIMIZING STRESS-CORROSION CRACKING IN WROUGHT TITANIUM ALLOY PRODUCTS
Available format(s)
Hardcopy , PDF
Superseded date
09-24-2020
Language(s)
English
Published date
09-28-2016
Publisher
1. SCOPE
2. APPLICABLE DOCUMENTS
3. GENERAL
4. RECOMMENDATIONS
5. NOTES
Gives recommendations concerning minimizing stress-corrosion cracking in wrought titanium alloy products.
| Committee |
AMS-G
|
| DocumentType |
Standard
|
| Pages |
4
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE AMS 6935 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 6.0V - 2.0SN, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4916L : 2017 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED |
| SAE AMS T 81556 : 2001 | TITANIUM AND TITANIUM ALLOYS, EXTRUDED BARS AND SHAPES, AIRCRAFT QUALITY |
| SAE AMS 4905 : 2017 | TITANIUM ALLOY, DAMAGE-TOLERANT GRADE PLATE, 6AL - 4V, BETA ANNEALED |
| SAE AMS 6932 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V EXTRA LOW INTERSTITIAL, ANNEALED |
| SAE AMS 6926 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 13V - 11CR - 3AL, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4988 : 2014 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, SOLUTION HEAT TREATED |
| SAE AMS4933F : 2017 | TITANIUM ALLOY EXTRUSIONS AND FLASH WELDED RINGS 8AL - 1MO - 1V SOLUTION HEAT TREATED AND STABILIZED |
| SAE AMS 6905 : 2014 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 2.0MO, DUPLEX ANNEALED |
| SAE AMS 4990 : 2015 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4965 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4976 : 2017 | TITANIUM ALLOY, FORGINGS, 6.0AL - 2.0SN - 4.0ZR - 2.0MO - 08SI, SOLUTION AND PRECIPITATION HEAT TREATED |
| MIL-T-81556 Revision A:1983 | TITANIUM & TITANIUM ALLOYS, EXTRUDED BARS AND SHAPES, AIRCRAFT QUALITY |
| SAE AMS 6901 : 2015 | TITANIUM ALLOY BARS, FORGINGS, AND FORGING STOCK 5AL - 2.5SN, EXTRA LOW INTERSTITIAL ANNEALED |
| SAE AMS 6910 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 8AL - 1MO - 1V, DUPLEX ANNEALED |
| SAE AMS 6915 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 7.0AL - 4.0MO, ANNEALED |
| SAE AMS 4907 : 2013 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6.0AL - 4.0V, EXTRA LOW INTERSTITIAL, ANNEALED |
| SAE AMS 4975 : 2017 | TITANIUM ALLOY, BARS, WIRE, AND RINGS, 6.0AL - 2.0SN - 4.0ZR - 2.0MO - 0.08SI, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4959 : 2017 | TITANIUM ALLOY WIRE 13.5V - 11CR - 3AL SPRING TEMPER |
| SAE AMS 4903 : 2015 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 4V, SOLUTION HEAT TREATED |
| SAE AMS6926D:2019(S2022) | Titanium Alloy Bars, Forgings and Forging Stock 13V - 11Cr - 3Al Solution Heat Treated and Aged(STABILIZED Nov 2022) |
| SAE AMS7011:2022 | Electron Beam-Powder Bed Fusion (EB-PBF) Produced Preforms and Parts Titanium Alloy, 6Al - 4V Hot Isostatically Pressed |
| SAE AMS 4909 : 2016 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN, EXTRA LOW INTERSTITIAL ANNEALED |
| SAE AMS 6953 : 2018 | TITANIUM ALLOY SHEET, 6AL - 4SN - 3NB - 0.5MO - 0.3SI, DUPLEX ANNEALED |
| SAE AMS 4963 : 2016 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL - 4.0V, ANNEALED, HEAT TREATABLE, MODIFIED STRENGTH |
| SAE AMS 6947 : 2015 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 4AL - 2.5V -1.5 FE ANNEALED, HEAT TREATABLE |
| SAE AMS 6952 : 2018 | TITANIUM ALLOY, FORGINGS, 5.8AL - 4.0SN - 3.5ZR - 2.8MO - 0.7NB - 0.35SI - 0.06C, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4981 : 2017 | TITANIUM ALLOY BARS, WIRE, AND FORGINGS, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS T 9046 : 2006 | TITANIUM AND TITANIUM ALLOY, SHEET, STRIP, AND PLATE |
| SAE AMS 4898 : 2014 | TITANIUM ALLOY, SHEET, 6AL - 2SN - 2ZR - 2MO - 2CR - 0.15SI, ANNEALED |
| SAE MAM 4911 : 1994 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4V, ANNEALED |
| SAE AMS 6930 : 2014 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 6900 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 5AL - 2.5SN, ANNEALED |
| SAE AMS 4939C : 2017 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED |
| SAE AMS 4910 : 2017 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN ANNEALED |
| SAE AMS 6945 : 2014 | TITANIUM ALLOY, SINGLE MELT, SHEET, STRIP, AND PLATE 6AL - 4V ANNEALED |
| SAE AMS 4937 : 2014 | TITANIUM ALLOY, EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 6V - 2SN, BETA EXTRUDED PLUS ANNEALED, HEAT TREATABLE |
| SAE AMS 4978 : 2018 | TITANIUM ALLOY BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, ANNEALED |
| SAE AMS 4919 : 2014 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 6AL - 2SN - 4ZR - 2MO - 0.08SI DUPLEX ANNEALED |
| SAE AMS 4917 : 2017 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 13.5V - 11CR - 3.0AL - SOLUTION HEAT TREATED |
| SAE AMS 4972 : 2015 | TITANIUM ALLOY BARS, WIRE, AND RINGS, 8AL - 1MO - 1V, SOLUTION HEAT TREATED AND STABILIZED |
| SAE AMS 6931 : 2017 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V, ANNEALED |
| SAE AMS 6920 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED |
| SAE AMS 4993F : 2017 | TITANIUM ALLOY, BLENDED POWDER COMPACTS, SINTERED, 6AL - 4V |
| SAE AMS 4971L : 2017 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, ANNEALED, HEAT TREATABLE |
| SAE AMS 4973 : 2016 | TITANIUM ALLOY FORGINGS, 8AL - 1MO - 1V, SOLUTION HEAT TREATED AND STABILIZED |
| SAE AMS 4979J : 2017 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4970 : 2016 | TITANIUM ALLOY BARS, WIRE, AND FORGINGS 7AL - 4MO SOLUTION AND PRECIPITATION HEAT TREATED |
| MIL-DTL-46077 Revision G:2006 | ARMOR PLATE, TITANIUM ALLOY, WELDABLE |
| SAE AMS 4908 : 1988 | TITANIUM ALLOY, SHEET AND STRIP 8MN ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH |
| SAE AMS 4920 : 2015 | TITANIUM ALLOY, FORGINGS, 6AI - 4V, ALPHA-BETA OR BETA PROCESSED, ANNEALED |
| SAE AMS 4915 : 2017 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1V - 1MO SINGLE ANNEALED |
| SAE AMS 6925 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 13V - 11CR - 3AL, SOLUTION HEAT TREATED |
| SAE AMS 4918 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, ANNEALED |
| SAE AMS 4904 : 2015 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 4V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 6907 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, DUPLEX ANNEALED |
| SAE AMS 4967 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS 6.0AL - 4.0V ANNEALED, HEAT TREATABLE |
| SAE AMS 6936 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6AL - 6V - 2SN, ANNEALED |
| SAE AMS 6906 : 2015 | TITANIUM ALLOY BARS, FORGINGS, AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4938 : 2013 | FORGINGS, TITANIUM ALLOYS HEAT-TREATED, FINISHED-PART PROPERTIES: SHORT-TRANSVERSE TENSILE, FRACTURE TOUGHNESS, AND LONGITUDINAL TIME-DEPENDENT-TENSION |
| SAE AMS 4950 : 2015 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL - 4.0V, SOLUTION HEAT TREATED AND AGED, MODIFIED STRENGTH |
| SAE AMS 6921 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4911 : 2018 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED |
| SAE AMS6900:2019(S2024) | Titanium Alloy Bars, Forgings and Forging Stock 5Al - 2.5Sn Annealed |
| SAE AMS4988E:2023 | Titanium Alloy Sheet, Strip, and Plate 6Al - 6V - 2Sn Solution Heat Treated |
| SAE AMS4950F:2023 | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Solution Heat Treated and Aged Modified Strength |
| SAE ARP 1795 : 1984 | STRESS CORROSION OF TITANIUM ALLOYS, EFFECT OF CLEANING AGENTS ON AIRCRAFT ENGINE MATERIALS |
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Hardcopy - English
PDF - English
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