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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 - 4 V, ANNEALED
Available format(s)
Hardcopy , PDF
Superseded date
09-28-2019
Superseded by
Language(s)
English
Published date
01-01-2014
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.| DocumentType |
Revision
|
| Pages |
7
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| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| 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 AMS 1431 : 2012 | 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 AMS 3281 : 2016 | SEALING COMPOUND, POLYSULFIDE (T) SYNTHETIC RUBBER FOR INTEGRAL FUEL TANK AND FUEL CELL CAVITIES LOW DENSITY FOR INTERMITTENT USE TO 360 DEGREES F (182 DEGREES 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 AMS 1428 : 2017 | FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN, (PSEUDOPLASTIC), SAE TYPES 2, 3 AND 4 |
| NASM 1312-21 : 2004 | FASTENER TEST METHODS METHOD 21 SHEAR JOINT FATIGUE, CONSTANT AMPLITUDE |
| SAE AMS 3278 : 2016 | SEALING AND COATING COMPOUND, POLYURETHANE (PUR), FUEL RESISTANT, HIGH TENSILE STRENGTH/ELONGATION, FOR INTEGRAL FUEL TANKS/FUEL CAVITIES/GENERAL PURPOSE |
| SAE AMS 1551 : 2008 | CLEANER, TURBINE ENGINE GAS PATH AQUEOUS TYPE |
| SAE AMS 3167 : 2005 | SOLVENTS, WIPE FOR CLEANING PRIOR TO APPLICATION OF PRIMER AND TOP COAT MATERIALS, OR SEALING COMPOUNDS |
| SAE AMS 1536 : 2008 | CLEANER FOR AIRCRAFT COMPONENTS COLD TANK TYPE, SOLVENT-BASE |
| SAE AMS 3255 : 2017 | SEALING TAPE, SHEET, OR GASKET, POLYTETRAFLUOROETHYLENE, EXPANDED (EPTFE) OIL AND WATER RESISTANT |
| SAE AMS 3379 : 2013(R2018) | 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 AMS 3276 : 2016 | SEALING COMPOUND, INTEGRAL FUEL TANKS AND GENERAL PURPOSE, INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C) |
| SAE AMS 3102 : 2017 | SEALING COMPOUND, POLYTHIOETHER RUBBER FAST CURING, LIGHT WEIGHT (SPECIFIC GRAVITY 0.78, MAX.) FOR INTEGRAL FUEL TANKS AND GENERAL PURPOSE, INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C) |
| SAE AS 5127 : 2013 | AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS METHODS FOR PREPARING AEROSPACE SEALANT TEST SPECIMENS |
| SAE AMS S 83318 : 2016 | SEALING COMPOUND, POLYSULFIDE TYPE, LOW TEMPERATURE CURING, QUICK REPAIR, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES |
| SAE AMS 1540 : 2015 | 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 AMS 1526 : 2008 | CLEANER FOR AIRCRAFT EXTERIOR SURFACES, WATER-MISCIBLE, PRESSURE-SPRAYING TYPE |
| SAE AMS 3100 : 2013 | 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 AMS 3265 : 2015 | SEALING COMPOUND, POLYSULFIDE (T) RUBBER, FUEL RESISTANT, NON-CHROMATED CORROSION INHIBITING, FOR INTERMITTENT USE TO 360 DEGREES F (182 DEGREES 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 AMS 1545 : 2015 | CLEANER, THRUST REVERSER, ALKALINE, WATER-BASE |
| SAE AMS 1548 : 2017 | CLEANER, TURBINE ENGINE GAS PATH, SOLVENT EMULSION TYPE |
| SAE AMS 3259 : 1997 | SEALING COMPOUND, POLYTHIOETHER - NONCHROMATED, CORROSION INHIBITING FOR INTERMITTENT USE TO 360 DEGREE F (182 DEGREE C) |
| SAE AMS 4949 : 2017 | TITANIUM, SHEET, LAMINATED, SURFACE BONDED |
| SAE AS 1241 : 2016 | 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 AMS 3381 : 2014 | SEALING COMPOUND, AIRCRAFT FIREWALL, NON-SILICONE |
| SAE AMS 1388 : 2008 | REMOVER, TEMPORARY COATING, ALKALINE TYPE, WATER BASE |
| SAE AMS 1374 : 2004 | 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 AMS DTL 22499 : 2013 | 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 AMS 3374 : 2013 | 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 AMS 1659 : 1991 | COATING, SOIL BARRIER, SEMI-PERMANENT |
| SAE AMS 1426 : 2016 | FLUID, DEICING/ANTI-ICING, RUNWAYS AND TAXIWAYS GLYCOL BASE |
| SAE AS 5127/1 : 2014 | 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 AMS 1424 : 2017 | 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 AMS S 8802 : 2015 | SEALING COMPOUND, FUEL RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES |
| SAE AMS 1435 : 2012 | FLUID, GENERIC, DEICING/ANTI-ICING, RUNWAYS AND TAXIWAYS |
| SAE AMS 3277 : 2015 | SEALING COMPOUND, POLYTHIOETHER RUBBER, FAST CURING FOR INTEGRAL FUEL TANKS AND GENERAL PURPOSE, INTERMITTENT USE TO 360 DEGREES F (182 DEGREES 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 AMS 3284 : 2017 | SEALING COMPOUND, LOW ADHESION, FOR REMOVABLE PANELS AND FUEL TANK INSPECTION PLATES |
| SAE AMS 2487 : 2018 | 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 AMS 4999 : 2016 | TITANIUM ALLOY DIRECT DEPOSITED PRODUCTS, 6AL - 4V, ANNEALED |
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