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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
MINIMIZING STRESS-CORROSION CRACKING IN WROUGHT TITANIUM ALLOY PRODUCTS
Available format(s)
Hardcopy , PDF
Superseded date
09-24-2020
Superseded by
Language(s)
English
Published date
09-28-2016
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.
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Superseded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 AMS4990C | 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 AMS6906B | 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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