AMS-T-9047
Revision: “N/A” issued 05/2003 ***Obsolete, S/S by AMS 6932***
Alloy: 6AL-4V Eli
Product Forms: Titanium and Titanium Alloy Bars (Rolled or Forged) and
Reforging Stock, Aircraft Quality
Condition: Annealed
Please note, the AMS-T-9047 specification covers various Alloys and Conditions. This Spec Sheet is only for the Alloy and Condition listed above.
| Composition Analysis | |
|---|---|
| Aluminum: 5.5 – 6.5% | Nitrogen (Maximum): 0.05% |
| Vanadium: 3.5 – 4.5% | Hydrogen (Maximum): 0.0125% |
| Iron (Maximum): 0.25% | Yttrium (Maximum): 0.005% |
| Oxygen (Maximum): 0.13% | Other Elements (Total): 0.30% |
| Carbon (Maximum): 0.08% | Titanium: Balance |
| Tensile Properties (Minimums)* | |
|---|---|
| Tensile: 125 – 130 ksi | Elongation: 10% |
| Yield: 115 – 120 ksi | Reduction of Area: 20 – 25% |
*Tensile property requirements vary based on orientation, section thickness/diameter, and cognizant engineering organization requirements.
Required Acceptance Tests
- Chemical Composition
- Microstructure
- Macrostructure
- Ultrasonic (where required)
- Tensile Properties
Disclaimer
The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. This Material Spec Sheet contains generalizations and is in no way a substitution for the AMS-T-9047 specification.
To purchase AMS-T-9047, please visit: https://www.sae.org/standards/content/amst9047/
Changes may be made to the information contained herein.
