• Shopping Cart
    There are no items in your cart

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Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by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Superseded date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Superseded by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

01-01-2013

Sorry this product is not available in your region.

DocumentType
Standard
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

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

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.