MIL-T-9047 6AL-4V

MIL-T-9047
Revision: “G, Amendment 2” issued 09/1986 ***Obsolete, S/S by AMS-T-9047***
Alloy: 6AL-4V
Product Forms: Titanium and Titanium Alloy Bars (Rolled or Forged) and
Reforging Stock, Aircraft Quality
Condition: Annealed

Please note, the MIL-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 – 6.75%Nitrogen (Maximum): 0.05%
Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.015%
Iron (Maximum): 0.30%Yttrium (Maximum): 0.005%
Oxygen (Maximum): 0.20%Other Elements (Total): 0.40%
Carbon (Maximum): 0.08%Titanium: Balance

 

Tensile Properties (Minimums)*
Tensile: 130 ksiElongation: 8 – 10%
Yield: 120 ksiReduction of Area: 15 – 25%

*Tensile property requirements vary based on orientation, section thickness/diameter, and cognizant engineering organization requirements.

Required Acceptance Tests

  • Chemical Composition
  • Microstructure
  • Macrostructure
  • Ultrasonic
  • 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 MIL-T-9047 specification.

To download MIL-T-9047G, please visit: https://assist.dla.mil/online/start/

Changes may be made to the information contained herein.

PERFORMANCE TITANIUM GROUP: A CUT ABOVE THE REST