SAE AMS4965L
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 Solution Heat Treated and Aged
Available format(s)
Hardcopy , PDF
Superseded date
27-09-2019
Superseded by
Language(s)
English
Published date
19-03-2014
Publisher
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1 SCOPE
2 APPLICABLE DOCUMENTS
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 ACKNOWLEDGMENT
7 REJECTIONS
8 NOTES
Describes a titanium alloy in the form of bars, wire, forgings, and flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and of stock of any size for forging and flash welded rings.
| DevelopmentNote |
Supersedes MIL F 83142 (A). (05/2006)
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| DocumentType |
Standard
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| Pages |
8
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
This specification covers a titanium alloy in the form of bars, wire, forgings, and flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and of stock of any size for forging and flash welded rings.
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| SAE AS4098A | Hose Assembly, Polytetrafluoroethylene, Heavy Duty, Metallic Reinforced, 400 °F, 5000 psi Hydraulic and Pneumatic |
| SAE AS1975G | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems |
| SAE MA2126B | Hose Assembly, Polytetrafluoroethylene (PTFE), up to 232 °C and 10 500 kPa Procurement Specification, Metric (ISO/DIS 10502) |
| SAE AIR5693 | Compatibility of PTFE Hose Assemblies With Typical Fluids Found in Aerospace Applications |
| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| MIL-DTL-25427 Revision B:2009 | COUPLING ASSEMBLY, HYDRAULIC, SELF SEALING, QUICK DISCONNECT, GENERAL SPECIFICATION FOR |
| SAE AS5960B | Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35 000 kPa), 400 °F (204 °C), Aircraft Hydraulic Systems |
| SAE AS4623E | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3,000 psi, 275 °F, Heavy Duty, Aircraft Hydraulic Systems |
| SAE AS5958F | Fittings, Axially Swaged Tube with Flareless Separable, Fluid System for Operating Pressures up to and Including 5080 psi (35000 kPa), Specification for |
| ASTM F 1472 : 2014 : REDLINE | Standard Specification for Wrought Titanium-6Aluminum-4Vanadium Alloy for Surgical Implant Applications (UNS R56400) |
| 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 |
| SAE AS5951D | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35000 kPa), 275 °F (135 °C), Aircraft Hydraulic Systems |
| BS EN 4632-006:2013 | Aerospace series. Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys |
| 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 |
| SAE AS5000C | Fitting, Plug-in Union, Ring Locked, 24 Degree Cone, Fluid Connection, 5080 psi (35 000 kPa), Specification for |
| SAE AS45909A | Stud, Locked In, Ring Locked, Serrated, General Specification For |
| NASA HDBK 6025 : 2014 | GUIDELINES FOR THE SPECIFICATION AND CERTIFICATION OF TITANIUM ALLOYS FOR NASA FLIGHT APPLICATIONS |
| MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| 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 |
| AN848 Revision 13:2015 | Elbow, Hose, 90 Degree |
| SAE AS4604B | Hose Assembly, 3000 psi, Polytetrafluoroethylene, Metallic Reinforced, 400 °F, Heavy Duty, Aircraft Hydraulic Systems |
| SAE MA1975 | Hose Assemblies, Polytetrafluoroethylene, Aramid Reinforced, 135 °C, Standard Duty, 28 000/21 000 kPa, Hydraulic, Aircraft Systems |
| SAE AS85720B | Fittings, Tube, Fluid Systems, Separable, High Pressure Beam Seal, 5000/8000 psi, General Specification For |
| TR 4661 : 2009 | AEROSPACE SERIES - HINGES, FLIGHT CONTROLS MATERIALS AND SURFACE TREATMENTS |
| I.S. EN 4632-006:2013 | AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS |
| SAE AS4897 | Hose Assembly, Polytetrafluoroethylene (PTFE), Low Pressure, 450 °F and Fireproof, Procurement Specification for |
| EN 4632-006:2013 | Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys |
| MIL-F-85720 Base Document:1985 | FITTING, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM, SEAL, GENERAL 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 |
| 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 4510 : DRAFT 2017 | AEROSPACE SERIES - PIPE COUPLING, 60 DEGREES, SPHERICAL, IN TITANIUM ALLOY TI-P64001, PORT ADAPTER, STRAIGHT, DOUBLE END, WITH LOCKING RING |
| 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 |
| SAE AS85421A | Fittings, Tube, Fluid Systems, Separable, Beam Seal, 3000/4000 psi, General Specification For |
| SAE MA614A | Hose Assembly, Polytetrafluoroethylene (PTFE), Metallic Reinforced, 28,000 kPa, 204 °C, Hydraulic, Metric |
| SAE AS614D | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 4000 psi, 400 °F, Heavy Duty, Hydraulic and Pneumatic |
| SAE MA4623 | Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric |
| SAE AS1946E | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, Up to 1500 psi and 450 °F, Hydraulic and Pneumatic |
| SAE AMS2241S | 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 |
| SAE AMS2750E | 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 AMS7498R | Rings, Flash Welded Titanium and Titanium Alloys |
| SAE AS6279A | Standard Practice for Production, Distribution, and Procurement of Metal Stock |
| SAE AMS2249G | Chemical Check Analysis Limits Titanium and Titanium Alloys |
| SAE AMS2808E | 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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