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BSI - BS EN 3813

Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - De ≤ 50 mm

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Organization: BSI
Publication Date: 31 January 2013
Status: active
Page Count: 12
ICS Code (Titanium): 49.025.30

Document History

BS EN 3813
January 31, 2013
Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - De ≤ 50 mm
A description is not available for this item.
BS EN 3813
January 31, 2013
Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - De ≤ 50 mm
A description is not available for this item.

References

This document references:
EN 2032-2 - Aerospace Series Metallic Materials Part 2: Coding of Metallurgical Condition in Delivery Condition
Published by CEN on January 1, 1994
A description is not available for this item.
This document references:
EN 4800-002 - Aerospace series - Titanium and titanium alloys - Technical specification - Part 002: Bar and section
Published by CEN on November 1, 2010
This standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy bar and section. It shall be applied when referred to and in...
This document references:
EN 3114-002 - Aerospace series - Test method - Microstructure of (a + ß) titanium alloy wrought products - Part 002: Microstructure of bars, sections, forging stock and forgings
Published by CEN on March 1, 2007
A description is not available for this item.
This document references:
EN 4258 - Aerospace Series - Metallic Materials - General Organization of Standardization - Links between Types of EN Standards and Their Use
Published by CEN on May 1, 1998
A description is not available for this item.
This document references:
EN 4500-004 - Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 004: Specific rules for titanium and titanium alloys
Published by CEN on October 1, 2012
This European Standard specifies the specific rules for the drafting and presentation of titanium and titanium alloy material standards for aerospace applications. It should be used in conjunction...
This document is referenced by:
BS 2A 266 TO 2A 271 + A1 - AEROSPACE SERIES Bolt, 100° Countersunk head, Hi-Torque speed drive recess, close tolerance shank, UNJF thread, split pin hole option, titanium alloy, various finishes. Classification: Rm 1100–1250 MPa (160 000–180 000 lbf/in2) at Ambient Temperature | +315 °C
Published by BSI on February 29, 2016
A description is not available for this item.
This document is referenced by:
BS EN 4424 - Rod-ends, adjustable, single fork and threaded shank with engagement: 1,5 × thread diameter in titanium alloys - Dimensions and loads
Published by BSI on June 30, 2006
A description is not available for this item.
This document is referenced by:
BS 2A 254 TO 2A 259 - Bolts, hexagonal head, close tolerance shank, UNJF threads, split pin & locking wire hole options, titanium alloy, various finishes Classification: Rm 1 100–1 250 MPa (160 000–180 000 lbf/in2) at Ambient Temperature | +315°C
Published by BSI on September 30, 2019
A description is not available for this item.
This document is referenced by:
BS EN 3725 - Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated - Strength class: 1 100 MPa (at ambient temperature)
Published by BSI on January 5, 2005
A description is not available for this item.
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