SAE AMS 1428 : 2017
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN, (PSEUDOPLASTIC), SAE TYPES 2, 3 AND 4
Available format(s)
Hardcopy , PDF
Superseded date
29-10-2018
Superseded by
Language(s)
English
Published date
01-01-2017
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. SIMILAR SPECIFICATIONS
9. NOTES
APPENDIX A - SUCCESSIVE DRY OUT AND REHYDRATION
TEST FOR DEICING/ANTI-ICING FLUID
Specifies three types of deicing/anti-icing fluids, each in the form of a non-Newtonian fluid.
| Committee |
G-12ADF
|
| DevelopmentNote |
Supersedes SAE AS 8243. (04/2010)
|
| DocumentType |
Standard
|
| Pages |
25
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE ARP 6207 : 2017 | QUALIFICATIONS REQUIRED FOR SAE TYPE 1 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| SAE ARP 4737 : 2017 | AIRCRAFT DEICING/ANTI-ICING METHODS |
| SAE ARP 5485 : 2017 | ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE 2/3/4 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| 14/30299187 DC : 0 | BS EN 12312-6 - AIRCRAFT GROUND SUPPORT EQUIPMENT - SPECIFIC REQUIREMENTS - PART 6: DEICERS AND DEICING/ANTIICING EQUIPMENT |
| BS EN 4697:2016 | Aerospace series. General and installation requirements for passenger seat fittings |
| SAE AMS 1428/2 : 2017 | FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN (PSEUDOPLASTIC), SAE TYPES 2, 3, AND 4 NON-GLYCOL BASED |
| PREN 4708-101 : DRAFT 2015 | AEROSPACE SERIES - SLEEVING, HEAT-SHRINKABLE, FOR BINDING, INSULATION AND IDENTIFICATION - PART 101: POLYOLEFIN SLEEVING - OPERATING TEMPERATURES -55 DEGREES C TO 135 DEGREES C - PRODUCT STANDARD |
| PREN 3909 : 200P3 | AEROSPACE SERIES - TEST FLUIDS FOR ELECTRICAL AND OPTICAL COMPONENTS AND SUB-ASSEMBLIES |
| PREN 4697 : 200P2 | AEROSPACE SERIES - GENERAL AND INSTALLATION REQUIREMENTS FOR PASSENGER SEAT FITTINGS |
| SAE ARD 50102 : 2002 | FORCED AIR OR FORCED AIR/FLUID EQUIPMENT FOR REMOVAL OF FROZEN CONTAMINANTS |
| SAE AIR 5704 : 2016 | FIELD VISCOSITY TEST FOR THICKENED AIRCRAFT ANTI-ICING FLUIDS |
| SAE AS 5900 : 2016 | STANDARD TEST METHOD FOR AERODYNAMIC ACCEPTANCE OF AMS1424 AND AMS1428 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| BS EN 3909:2016 | Aerospace series. Test fluids and test methods for electrical and optical components and sub-assemblies |
| I.S. EN 3909:2016 | AEROSPACE SERIES - TEST FLUIDS AND TEST METHODS FOR ELECTRIC COMPONENTS AND SUB-ASSEMBLIES |
| EN 12312-6:2017 | Aircraft ground support equipment - Specific requirements - Part 6: Deicers and de-icing/anti-icing equipment |
| SAE ARP 5149 : 2013 | TRAINING PROGRAM GUIDELINES FOR DEICING/ANTI-ICING OF AIRCRAFT ON GROUND |
| SAE AIR 6232 : 2013 | AIRCRAFT SURFACE COATING INTERACTION WITH AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| 16/30354036 DC : 0 | BS EN 4854-3 - AEROSPACE SERIES - BEARINGS, SPHERICAL PLAIN, IN CORROSION RESISTING STEEL WITH SELF-LUBRICATING LINER, LOW STARTING TORQUE AND LOW FRICTION COEFFICIENT, ELEVATED DUTY CYCLES UNDER LOW OSCILLATIONS AT DIFFERENT OPERATING CONDITIONS - PART 3: TECHNICAL SPECIFICATION |
| BS EN 4708-101:2017 | Aerospace series. Sleeving, heat-shrinkable, for binding, insulation and identification Polyolefin sleeving. Operating temperatures -55 °C to 135 °C. Product standard |
| SAE AMS 1428/1 : 2017 | Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV Glycol (Conventional and Non-Conventional) Based |
| FAA AC 135-16 : 0 | GROUND DEICING AND ANTI-ICING TRAINING AND CHECKING |
| PREN 4641-102 : 200P1 | AEROSPACE SERIES - CABLES, OPTICAL 125 [MU]M DIAMETER CLADDING - PART 102: SEMI-LOOSE 62,5/125 [MU]M GI FIBRE NOMINAL 1,8 MM OUTSIDE DIAMETER - PRODUCT STANDARD |
| SAE AS 5958 : 2017 | FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPARABLE, FLUID SYSTEM FOR OPERATING PRESSURES UP TO AND INCLUDING 5080 PSI (35 000 KPA), SPECIFICATION FOR |
| SAE ARP 5718 : 2017 | Qualifications Required for SAE Type II/III/IV Aircraft Deicing/Anti-Icing Fluid |
| SAE AS 9968 : 2014 | LABORATORY VISCOSITY MEASUREMENT OF THICKENED AIRCRAFT DEICING/ANTI-ICING FLUIDS WITH THE BROOKFIELD LV VISCOMETER |
| SAE AS 6332 : 2017 | AIRCRAFT GROUND DEICING/ANTI-ICING QUALITY MANAGEMENT |
| BS EN 12312-6:2017 | Aircraft ground support equipment. Specific requirements Deicers and de-icing/anti-icing equipment |
| I.S. EN 12312-6:2017 | AIRCRAFT GROUND SUPPORT EQUIPMENT - SPECIFIC REQUIREMENTS - PART 6: DEICERS AND DE-ICING/ANTI-ICING EQUIPMENT |
| BS ISO 11078:2007 | Aircraft. De-icing/anti-icing fluids. ISO type II, III and IV |
| MIL-PRF-81975 Revision C:2008 | COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
| I.S. EN 4641-102:2009 | AEROSPACE SERIES - CABLES, OPTICAL 125 [MU]M OUTSIDE DIAMETER CLADDING - PART 102: SEMI-LOOSE 62,5/125 [MU]M GI FIBRE NOMINAL 1,8 MM OUTSIDE DIAMETER - PRODUCT STANDARD |
| BS EN 4641-102:2009 | Aerospace series. Cables, optical 125 μm outside diameter cladding Semi-loose 62,5/125 μm GI fibre nominal 1,8 mm outside diameter. Product standard |
| 13/30291179 DC : 0 | BS EN 4697 - AEROSPACE SERIES - GENERAL AND INSTALLATION REQUIREMENTS FOR PASSENGER SEAT FITTINGS |
| MIL-STD-3004 Revision D:2014 | QUALITY ASSURANCE/SURVEILLANCE FOR FUELS, LUBRICANTS AND RELATED PRODUCTS |
| FAA AC 120-60 : 2004 | GROUND DEICING AND ANTI-ICING PROGRAM |
| PREN 6059-303 : 200P3 | AEROSPACE SERIES - ELECTRICAL CABLES, INSTALLATION - PROTECTION SLEEVES - TEST METHODS - PART 303: RESISTANCE TO FLUIDS |
| SAE AIR 9968 : 2015 | VISCOSITY TEST OF THICKENED AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| SAE ARP 4902 : 2018 | DESIGN OF AIRCRAFT DEICING FACILITIES |
| I.S. EN 4697:2016 | AEROSPACE SERIES - GENERAL AND INSTALLATION REQUIREMENTS FOR PASSENGER SEAT FITTINGS |
| SAE AS 6285 : 2016 | AIRCRAFT GROUND DEICING/ANTI-ICING PROCESSES |
| EN 4708-101:2017 | Aerospace series - Sleeving, heat-shrinkable, for binding, insulation and identification - Part 101: Polyolefin sleeving - Operating temperatures -55 °C to 135 °C - Product standard |
| MIL-PRF-57267 Base Document:2017 | COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
| SAE ARP 5058 : 2004 | ENCLOSED OPERATORS CABIN FOR AIRCRAFT GROUND DEICING EQUIPMENT |
| SAE AS 5901 : 2014 | WATER SPRAY AND HIGH HUMIDITY ENDURANCE TEST METHODS FOR SAE AMS1424 AND SAE AMS1428 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| SAE ARP 6852 : 2017 | METHODS AND PROCESSES FOR EVALUATION OF AERODYNAMIC EFFECTS OF SAE-QUALIFIED AIRCRAFT GROUND DEICING/ANTI-ICING FLUIDS |
| SAE AIR 6284 : 2015 | FORCED AIR OR FORCED AIR/FLUID EQUIPMENT FOR REMOVAL OF FROZEN CONTAMINANTS |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| I.S. EN 4708-101:2017 | AEROSPACE SERIES - SLEEVING, HEAT-SHRINKABLE, FOR BINDING, INSULATION AND IDENTIFICATION - PART 101: POLYOLEFIN SLEEVING - OPERATING TEMPERATURES -55 DEGREES C TO 135 DEGREES C - PRODUCT STANDARD |
| SAE AS 6286 : 2016 | TRAINING AND QUALIFICATION PROGRAM FOR DEICING/ANTI-ICING OF AIRCRAFT ON THE GROUND |
| UNE-EN 12312-6:2017 | Aircraft ground support equipment - Specific requirements - Part 6: Deicers and de-icing/anti-icing equipment |
| BS EN 6059-303:2017 | Aerospace series. Electrical cables, installation. Protection sleeves. Test methods Resistance to fluids |
| EN 4697:2016 | Aerospace series - General and installation requirements for passenger seat fittings |
| EN 6059-303:2017 | Aerospace series - Electrical cables, installation - Protection sleeves - Test methods - Part 303: Resistance to fluids |
| EN 4641-102:2009 | Aerospace series - Cables, optical 125 μm outside diameter cladding - Part 102: Semi-loose 62,5/125 µm GI fibre nominal 1,8 mm outside diameter - Product standard |
| EN 3909:2016 | Aerospace series - Test fluids and test methods for electrical and optical components and sub-assemblies |
| FAA AC 20-73 : 2006 | AIRCRAFT ICE PROTECTION |
| I.S. EN 6059-303:2017 | AEROSPACE SERIES - ELECTRICAL CABLES, INSTALLATION - PROTECTION SLEEVES - TEST METHODS - PART 303: RESISTANCE TO FLUIDS |
| SAE AS 5116 : 2003 | MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR GROUND ICE DETECTION SYSTEMS |
| SAE AS 5681 : 2016 | MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR REMOTE ON-GROUND ICE DETECTION SYSTEMS |
| SAE AIR 5490 : 2016 | CARBON BRAKE CONTAMINATION AND OXIDATION |
| ISO 11078:2007 | Aircraft — De-icing/anti-icing fluids — ISO types II, III and IV |
| SAE AMS 4049 : 2016 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD 5.6ZN - 2.5MG - 1.6CU - 0.23CR (ALCLAD 7075; -T6 SHEET - T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 2475H : 2009 | PROTECTIVE TREATMENTS, MAGNESIUM ALLOYS |
| ASTM D 1177 : 2017 : REDLINE | Standard Test Method for Freezing Point of Aqueous Engine Coolants |
| SAE AMS 5886 : 2014 | ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 50NI - 20CR - 20CO - 5.8MO - 2.2TI - 0.45AL CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 2100 DEGREES F (1149 DEGREES C) SOLUTION HEAT TREATED |
| SAE AMS 4911 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED |
| SAE AMS 4376 : 2011(R2018) | PLATE, MAGNESIUM ALLOY - 3.0AL - 1.0ZN - 0.20MN (AZ31B-H26) COLD ROLLED AND PARTIALLY ANNEALED |
| SAE AMS 4037 : 2014 | ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED |
| SAE AIR 9968 : 2015 | VISCOSITY TEST OF THICKENED AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| MIL-STD-870 Revision C:2007 | Cadmium Plating, Low Embrittlement, Electrodepositon |
| ASTM E 70 | TEST METHOD FOR PH OF AQUEOUS SOLUTIONS WITH THE GLASS ELECTRODE |
| SAE AMS 1428/1 : 2017 | Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV Glycol (Conventional and Non-Conventional) Based |
| SAE AMS 1428/2 : 2017 | FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN (PSEUDOPLASTIC), SAE TYPES 2, 3, AND 4 NON-GLYCOL BASED |
| ASTM D 1331 : 2014 : REDLINE | Standard Test Methods for Surface and Interfacial Tension of Solutions of Paints, Solvents, Solutions of Surface-Active Agents, and Related Materials |
| SAE AMS P 83310 : 2016 | PLASTIC SHEET, POLYCARBONATE, TRANSPARENT |
| SAE AS 5900 : 2016 | STANDARD TEST METHOD FOR AERODYNAMIC ACCEPTANCE OF AMS1424 AND AMS1428 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| SAE ARP 5485 : 2007 | ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE 2/3/4 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| SAE ARP 1917 : 2002 | CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS |
| SAE ARP 4737 : 2008 | AIRCRAFT DEICING/ANTI-ICING METHODS |
| SAE AS 6285 : 2016 | AIRCRAFT GROUND DEICING/ANTI-ICING PROCESSES |
| ASTM D 93 : 2016-07 | TEST METHODS FOR FLASH POINT BY PENSKY-MARTENS CLOSED CUP TESTER |
| MIL-PRF-25690 Revision B:1993 | PLASTIC, SHEET AND FORMED PARTS, MODIFIED ACRYLIC BASE, MONOLITHIC, CRACK PROPAGATION RESISTANT |
| SAE AMS 2825 : 1987 | MATERIAL SAFETY DATA SHEETS |
| SAE AMS 4916 : 2014 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED |
| ASTM D 891 : 2009-04 | TEST METHODS FOR SPECIFIC GRAVITY, APPARENT, OF LIQUID INDUSTRIAL CHEMICALS |
| SAE ARP 5718 : 2012 | QUALIFICATIONS REQUIRED FOR SAE TYPE 2/3/4 AIRCRAFT, DEICING/ANTI-ICING FLUID |
| SAE AS 5901 : 2014 | WATER SPRAY AND HIGH HUMIDITY ENDURANCE TEST METHODS FOR SAE AMS1424 AND SAE AMS1428 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| SAE AMS 2470 : 2013 | ANODIC TREATMENT OF ALUMINUM ALLOYS, CHROMIC ACID PROCESS |
| SAE AMS 5045 : 2015 | STEEL, SHEET AND STRIP, 0.25 CARBON, MAXIMUM HARD TEMPER |
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