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SAE AMS 4967 : 2014

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by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, BARS, WIRE, FORGINGS, AND RINGS 6.0AL - 4.0V ANNEALED, HEAT TREATABLE

Available format(s)

Hardcopy , PDF

Superseded date

15-10-2018

Superseded by

SAE AMS 4967M:2018

Language(s)

English

Published date

01-01-2014

$169.83
Including GST where applicable

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 bars, wire, forgings, flash welded rings up through 4.000 inches (101.60 mm) in diameter or least distance between parallel sides and stock of any size for forging, heading, or flash welded rings.

Committee
AMS-G
DocumentType
Standard
Pages
9
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

17/30369678 DC : 0 PREN 7010 - AEROSPACE SERIES - USER GUIDE FOR CREATION AND DESIGNATION OF BOLTS
SAE AS 269J:2012:(S2018) IDENTIFICATION OF MATERIAL FOR AN, MS AND AS ENGINE AND PROPELLER STANDARD UTILITY PARTS AND ALSO FOR COMPANY PARTS
MIL-P-87988 Base Document:1989 PIN-RIVET, THREADED WITH HEX SOCKET
PREN 4832 : DRAFT 2017 AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION
SAE AS 45909 : 2015 STUD, LOCKED IN, RING LOCKED, SERRATED, GENERAL SPECIFICATION FOR
MIL-S-45909 Revision C:1989 STUD, LOCKED IN - RING LOCKED SERRATED
MIL-R-83459 Revision A:1978 RIVET, TITANIUM, BIMETAL 95 KSI F SU GENERAL SPECIFICATION FOR
MIL-B-23964 Revision D:1981 BOLT, SELF-RETAINING, POSITIVE LOCKING
MIL I 45910 : C INSERT, SCREW THREAD LOCKED IN & RING LOCKED 1 SERRATED GENERAL SPECIFICATION FOR
10/30227763 DC : 0 BS EN 6114 - AEROSPACE SERIES - BOLT, COUNTERSUNK HEAD, SHORT THREAD - INCH SERIES
PREN 4510 : DRAFT 2017 AEROSPACE SERIES - PIPE COUPLING, 60 DEGREES, SPHERICAL, IN TITANIUM ALLOY TI-P64001, PORT ADAPTER, STRAIGHT, DOUBLE END, WITH LOCKING RING
SAE AS 7461 : 2015 BOLTS AND SCREWS, TITANIUM ALLOY, 6AL-4V, UNS R56400, FATIGUE-RATED, PROCUREMENT SPECIFICATION FOR
15/30329889 DC : 0 BS A 266 TO 271 - BOLT, 100 DEGREES COUNTERSUNK HEAD, HI-TORQUE SPEED DRIVE RECESS, UNJF THREAD, SPLIT PIN HOLE OPTION, TITANIUM ALLOY, VARIOUS FINISHES, CLASSIFICATION: 80 TF/IN[2] (1100 MPA) AT TA/+315 DEGREES C
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
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
10/30227764 DC : 0 BS EN 6115 - AEROSPACE SERIES - BOLT - PROTRUDING HEAD, SHORT THREAD - INCH SERIES
14/30310862 DC : 0 BS EN 4832 - AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION
BS 2A 266 to 2A 271:2016+A1:2019 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: R<sub>m</sub> 1100–1250 MPa (160 000–180 000 lbf/in<sup>2</sup>) at Ambient Temperature | +315 °C
NASA HDBK 6025 : 2014 GUIDELINES FOR THE SPECIFICATION AND CERTIFICATION OF TITANIUM ALLOYS FOR NASA FLIGHT APPLICATIONS
MIL-DTL-45910 Revision D:2015 INSERT, SCREW THREAD-LOCKED IN AND RING LOCKED, SERRATED GENERAL SPECIFICATION FOR
BS EN 4632-006:2013 Aerospace series. Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys
16/30346081 DC : 0 BS EN 4510 - AEROSPACE SERIES - PIPE COUPLINGS, 60 DEGREE, SPHERICAL IN TITANIUM ALLOY TIP64001 - ADAPTERS, STRAIGHT, DOUBLE END, WITH LOCKING RING
SAE AS 5000 : 2010 FITTING, PLUG-IN UNION, RING LOCKED, 24 DEGREE CONE, FLUID CONNECTION, 5080 PSI (35000 KPA), SPECIFICATION FOR
I.S. EN 4632-006:2013 AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: 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
SAE AS 7460 : 2017 BOLTS AND SCREWS, TITANIUM ALLOY, 6.0AL-4.0V, PROCUREMENT SPECIFICATION FOR
PREN 4833 : DRAFT 2017 AEROSPACE SERIES - PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING LOCKED FITTING - FLARELESS END - INCH SERIES - EXTRA FINE THREAD PITCH
MIL B 85667/12 : 0 BOLT, SLEEVE 100 DEGREE TENSION FLUSH HEAD, STRAIGHT SHANK, CRES 304 SLEEVE, TITANIUM ALLOY PIN, 95 KSI FSU, 160 KSI FTU
PREN 4836 : DRAFT 2017 AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING REDUCER - FLARELESS END - INCH SERIES - EXTRA FINE THREAD PITCH
PREN 4632-006 : DRAFT 2008 WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 006: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
TR 4661 : 2009 AEROSPACE SERIES - HINGES, FLIGHT CONTROLS MATERIALS AND SURFACE TREATMENTS
UNI EN 4632-006 : 2014 AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS

SAE AMS 2241 : 2016 TOLERANCES, CORROSION AND HEAT-RESISTANT STEEL, IRON ALLOY, TITANIUM, AND TITANIUM ALLOY BARS AND WIRE
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 2809 : 2007(R2011) IDENTIFICATION, TITANIUM AND TITANIUM ALLOY WROUGHT PRODUCTS
ASTM E 2994 : 2016 Standard Test Method for Analysis of Titanium and Titanium Alloys by Spark Atomic Emission Spectrometry and Glow Discharge Atomic Emission Spectrometry (Performance-Based Method)
SAE AS 1814 : 2016 TERMINOLOGY FOR TITANIUM MICROSTRUCTURES
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 ARP 1917 : 2002 CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS
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
SAE AMS 2808 : 2017 IDENTIFICATION FORGINGS
ASTM E 8/E8M : 2016-09 TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS
SAE ARP 982 : 2016 MINIMIZING STRESS-CORROSION CRACKING IN WROUGHT TITANIUM ALLOY PRODUCTS

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