SAE AMS4911N
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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, Sheet, Strip, and Plate 6Al - 4V Annealed
Available format(s)
Hardcopy , PDF
Superseded date
28-09-2019
Superseded by
Language(s)
English
Published date
07-03-2014
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.| DocumentType |
Standard
|
| Pages |
7
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| PublisherName |
SAE International
|
| Status |
Superseded
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| SupersededBy | |
| Supersedes |
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm) inclusive in thickness (See 8.5).
| Standards | Relationship |
| MIL-T-9046 Revision J:1983 | Similar to |
| MIL-PRF-32239 Revision A:2014 | COATING SYSTEM, ADVANCED PERFORMANCE, FOR AEROSPACE APPLICATIONS |
| SAE ARP699E | High Temperature Pneumatic Duct Systems for Aircraft |
| SAE AMS1431D | Compound, Solid Runway and Taxiway Deicing/Anti-Icing |
| MIL-PRF-680 Revision C:2010 | DEGREASING SOLVENT |
| MIL-PRF-32405 Base Document:2013 | CLEANER, HAND WIPE, FOR AVIATION AND MISSILE SYSTEMS, METALLIC SUBSTRATES, LOW OR EXEMPT VOC |
| SAE AMS3281F | Sealing Compound, Polysulfide (T) Synthetic Rubber for Integral Fuel Tank and Fuel Cell Cavities Low Density for Intermittent Use to 360 °F (182 °C) |
| MIL-PRF-32359 Base Document:2012 | CLEANER, GENERAL, FOR GROUND VEHICLES AND GROUND SUPPORT EQUIPMENT, HAP-FREE |
| 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 |
| SAE AMS1428J | Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV |
| NASM 1312-21 : 2004 | FASTENER TEST METHODS METHOD 21 SHEAR JOINT FATIGUE, CONSTANT AMPLITUDE |
| SAE AMS3278B | Sealing and Coating Compound, Polyurethane (PUR) Fuel Resistant High Tensile Strength / Elongation For Integral Fuel Tanks / Fuel Cavities / General Purpose |
| SAE AMS3167B | Solvents, Wipe for Cleaning Prior to Application of Primer and Top Coat Materials, or Sealing Compounds |
| SAE AMS1536B | Cleaner for Aircraft Components Cold Tank Type, Solvent-Base |
| SAE AMS3255B | Sealing Tape, Sheet, or Gasket, Polytetrafluoroethylene, Expanded (EPTFE) Oil and Water Resistant |
| SAE AMS3379 | Sealing Compound, Polysulfide Rubber Preformed Strips for Sealing Removable Doors, Skins, and Panels |
| MIL-DTL-32139 Revision B:2017 | Connectors, Electrical, Rectangular, Nanominiature, Polarized Shell, General Specification for |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| P-W-2891 Revision A:2002 | WIPE SOLVENTS, EXEMPT AND NON-EXEMPT |
| MIL-PRF-85570 Revision E:2012 | CLEANING COMPOUNDS, AIRCRAFT, EXTERIOR |
| MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
| SAE AMS3276F | Sealing Compound, Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C) |
| SAE AMS3102 | Sealing Compound, Polythioether Rubber Fast Curing, Light Weight (Specific Gravity 0.78, max.) for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C) |
| SAE AS5127B | Aerospace Standard Test Methods for Aerospace Sealants Methods for Preparing Aerospace Sealant Test Specimens |
| SAE AMSS83318C | Sealing Compound, Polysulfide Type, Low Temperature Curing, Quick Repair, Integral Fuel Tanks and Fuel Cell Cavities |
| SAE AMS1540C | Cleaner, Thrust Reverser Water-Base |
| ASTM F 1472 : 2014 : REDLINE | Standard Specification for Wrought Titanium-6Aluminum-4Vanadium Alloy for Surgical Implant Applications (UNS R56400) |
| SAE AMS3100D | Adhesion Promoter For Polysulfide Sealing Compounds |
| SAE AMS 1453 : 2015 | DISINFECTANT CLEANER FOR AIRCRAFT INTERIOR GENERAL PURPOSE LIQUID |
| SAE AMS2437C | Coating, Plasma Spray Deposition |
| 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 M 75:1994 | Aircraft de-icing/anti-icing Newtonian fluids, ISO type I |
| BS EN 4632-006:2013 | Aerospace series. Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys |
| SAE AMS3265E | Sealing Compound, Polysulfide (T) Rubber, Fuel Resistant, Non-Chromated Corrosion Inhibiting For Intermittent Use to 360 °F (182 °C) |
| MIL-PRF-32295 Revision B:2017 | CLEANER, NON-AQUEOUS, LOW-VOC, HAP-FREE |
| MIL-PRF-32597 Base Document:2018 | CLEANER, POLYMER AND POLYMER MATRIX COMPOSITE (PMC) MATERIAL, NON-AQUEOUS, HAP-FREE |
| SAE AMS1376B | Remover, Epoxy Paint Acid-Type, Thickened |
| SAE AMS2488D | Anodic Treatment - Titanium and Titanium Alloys Solution pH 13 or Higher |
| SAE AMS 1375 : 2012 | REMOVER, PAINT, EPOXY AND POLYURETHANE PAINT SYSTEMS |
| SAE AMS1545B | Cleaner, Thrust Reverser Alkaline, Water-Base |
| SAE AMS1548B | Cleaner, Turbine Engine Gas Path Solvent Emulsion Type |
| SAE AMS3259B | Sealing Compound, Polythioether Nonchromated, Corrosion Inhibiting for Intermittent Use to 360°F (182°C) |
| SAE AMS4949B | Titanium, Sheet, Laminated, Surface Bonded |
| SAE AS1241D | Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft |
| SAE AMS 1377 : 2012 | REMOVER, PAINT, EPOXY AND POLYURETHANE PAINT SYSTEM, NON-CHLORINATED SOLVENT |
| NASA HDBK 6025 : 2014 | GUIDELINES FOR THE SPECIFICATION AND CERTIFICATION OF TITANIUM ALLOYS FOR NASA FLIGHT APPLICATIONS |
| MIL-F-18280 Revision F:1995 | FITTING, FLARELESS TUBE, FLUID CONNECTION |
| BS M 78:1995 | Aircraft de-icing/anti-icing non-Newtonian fluids, ISO type II |
| SAE AMS3381 | Sealing Compound, Aircraft Firewall, Non-Silicone |
| SAE AMS 1388 : 2008 | REMOVER, TEMPORARY COATING, ALKALINE TYPE, WATER BASE |
| SAE AMS1374A | Remover, Polyurethane/Epoxy Paint Alkaline, Hot-Tank Type |
| SAE ARP 1755 : 2000 | EFFECT OF CLEANING AGENTS ON AIRCRAFT ENGINE MATERIALS, STOCK LOSS TEST METHOD |
| SAE AMS 1432 : 1995 | FLUID, DEICING/ANTI-ICING, RUNWAYS AND TAXIWAYS, POTASSIUM ACETATE BASE |
| I.S. EN 4632-006:2013 | AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS |
| SAE AMSDTL22499A | Shim Stock, Laminated |
| EN 4632-006:2013 | Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys |
| SAE AMS3374D | Sealing Compound Aircraft Firewall, Silicone |
| SAE AMS 3686 : 2014 | ADHESIVE, POLYIMIDE RESIN, FILM AND PASTE HIGH TEMPERATURE RESISTANT, 315 DEGREES C (599 DEGREES F) |
| SAE AMS1659 | COATING, SOIL BARRIER Semi-Permanent |
| SAE AMS1426D | Fluid, Deicing/Anti-Icing, Runways and Taxiways Glycol Base |
| SAE AS5127/1C | Aerospace Standard Test Methods for Aerospace Sealants Two-Component Synthetic Rubber Compounds |
| SAE ARP 1843 : 2013 | SURFACE PREPARATION FOR STRUCTURAL ADHESIVE BONDING, TITANIUM ALLOY PARTS |
| SAE AMS1424N | Fluid, Aircraft Deicing/Anti-Icing, SAE Type 1 |
| MIL-PRF-32587 Base Document:2018 | Remover, Paint, Hap-Free, Neutral |
| SAE AMS 1527 : 2014 | CLEANER FOR AIRCRAFT EXTERIOR SURFACES, WATER-MISCIBLE, FOAM-ON, PRESSURE-SPRAYING |
| SAE AMSS8802D | Sealing Compound, Fuel Resistant, Integral Fuel Tanks and Fuel Cell Cavities |
| SAE AMS1435C | Fluid, Generic, Deicing/Anti-Icing Runways and Taxiways |
| SAE AMS3277J | Sealing Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C) |
| PREN 4632-006 : DRAFT 2008 | WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 006: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS |
| SAE AMS3284C | Sealing Compound, Low Adhesion, for Removable Panels and Fuel Tank Inspection Plates |
| SAE AMS2487B | Anodic Treatment of Titanium and Titanium Alloys Solution pH 12.4 Maximum |
| UNI EN 4632-006 : 2014 | AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS |
| SAE AMS4999A | Titanium Alloy Direct Deposited Products 6Al - 4V Annealed |
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