Customer Support: 131 242

  • Shopping Cart
    There are no items in your cart
Please Select Your Option.
It seems you are away from your “home” country. Do you wish to be re-directed to your “home” store? If you choose “YES”, you will see product, taxation, and shipping information relevant to your country. If you select “NO”, the current store's conditions will apply.
We noticed you’re not on the correct regional site. Switch to our AMERICAS site for the best experience.
Dismiss alert

SAE AMS4966P

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Titanium Alloy, Forgings 5Al - 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength

Superseded date

11-06-2017

Superseded by

SAE AMS4966R

Published date

26-02-2013

DocumentType
Standard
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

This specification covers a titanium alloy in the form of forgings and forging stock.

Standards Relationship
MIL-F-83142 Revision A:1969 Similar to

EN 4632-006:2013 Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys
BS EN 4632-006:2013 Aerospace series. Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys
PREN 4632-006 : DRAFT 2008 WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 006: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS

Sorry this product is not available in your region.

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.