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SAE AMS 4934 : 2015

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

TITANIUM ALLOY, EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 4V, SOLUTION HEAT TREATED AND AGED
Available format(s)

Hardcopy , PDF

Superseded date

03-06-2019

Language(s)

English

Published date

01-01-2015

1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES

Specifies a titanium alloy in the form of extruded bars, and shapes, flash welded rings up through 3.000 inches (76.20 mm) inclusive, in nominal diameter or least distance between parallel sides, and stock for flash welded rings of any size.

Committee
AMS-G
DocumentType
Standard
Pages
7
PublisherName
SAE International
Status
Superseded
SupersededBy

Standards Relationship
MIL-T-81556 Revision A:1983 Similar to

09/30199811 DC : 0 BS EN 4632-006 - AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 6: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
I.S. EN 4632-006:2013 AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS
NFL 06 380-24 : 2008 AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 24: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
BS EN 4632-006:2013 Aerospace series. Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys
EN 4632-006:2013 Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: 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
UNI EN 4632-006 : 2014 AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS

ASTM E 2371 : 2013 Standard Test Method for Analysis of Titanium and Titanium Alloys by Direct Current Plasma and Inductively Coupled Plasma Atomic Emission Spectrometry (Performance-Based Test Methodology)
SAE AMS 2245 : 2017 TOLERANCES, TITANIUM AND TITANIUM ALLOY EXTRUDED BARS, RODS, AND SHAPES
SAE AMS 2809 : 2007(R2011) IDENTIFICATION, TITANIUM AND TITANIUM ALLOY WROUGHT PRODUCTS
SAE AMS 2750 : 2012 PYROMETRY
ASTM E 1409 : 2013 : REDLINE Standard Test Method for Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by Inert Gas Fusion
SAE AMS 7498 : 2016 RINGS, FLASH WELDED TITANIUM AND TITANIUM ALLOYS
SAE AS 6279 : 2016 STANDARD PRACTICE FOR PRODUCTION, DISTRIBUTION, AND PROCUREMENT OF METAL STOCK
SAE AMS 2249 : 2013 CHEMICAL CHECK ANALYSIS LIMITS, TITANIUM AND TITANIUM ALLOYS
ASTM E 8/E8M : 2016-09 TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS

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