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About This Item

 

Full Description

BS 3TA 11:2009+A1:2017 specifies requirements for titanium-aluminiumvanadium alloy bar and section with a tensile strength of 900 MPa to 1 160 MPa.


Cross References:
BS TA 100
BS TA 10
BS TA 12
BS TA 13
BS TA 28
BS TA 56
EN 4500-1
EN 4500-4


Incorporates the following:
Amendment, March 2017. Amends and replaces BS 3TA 11:2009
 

Document History

  1. BS EN 3311:2023


    Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bars for machining. D ≤ 300 mm. 900 MPa ≤ Rm ≤ 1 160 MPa

    • Most Recent
  2. BS EN 3311:2009


    Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bar for machining. D < 110 mm

    • Historical Version
  3. BS 3TA 11:2009+A1:2017

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    Specification for bar and section for machining of titanium-aluminium-vanadium alloy (Tensile strength 900–1 160 MPa) (Limiting ruling section 150 mm)

    • Historical Version
  4. BS 09/30193250 DC


    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)

    • Historical Version
  5. BS 2TA 11:1974


    Specification for bar and section for machining of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)

    • Historical Version