SAE AMS1428J
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 II, III, and IV
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
01-03-2017
Publisher
Superseded date
29-10-2018
Superseded by
€135.00
Excluding VAT
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.
| DevelopmentNote |
Supersedes SAE AS 8243. (04/2010)
|
| DocumentType |
Standard
|
| Pages |
25
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This foundation specification (AMS1428J) and its associated category specifications (AMS1428/1 and AMS1428/2) cover three types of deicing/anti-icing fluids, each in the form of a non-Newtonian fluid.
| SAE ARP6207 | Qualifications Required for SAE Type I Aircraft Deicing/Anti-Icing Fluids |
| SAE ARP4737J | Aircraft Deicing/Anti-Icing Methods |
| SAE ARP5485B | Endurance Time Test Procedures for SAE Type II/III/IV 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 AMS1428/2 | Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV 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 AIR5704 | Field Viscosity Test for Thickened Aircraft Anti-Icing Fluids |
| SAE AS5900C | 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 ARP5149C | Training Program Guidelines for Deicing/Anti-Icing of Aircraft on Ground |
| 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 AMS1428/1 | 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 AS5958F | Fittings, Axially Swaged Tube with Flareless Separable, Fluid System for Operating Pressures up to and Including 5080 psi (35000 kPa), Specification for |
| SAE ARP5718B | Qualifications Required for SAE Type II/III/IV Aircraft Deicing/Anti-Icing Fluid |
| SAE AS9968 | Laboratory Viscosity Measurement of Thickened Aircraft Deicing/Anti-icing Fluids with the Brookfield LV Viscometer |
| SAE AS6332 | 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 (S/S by MIL-STD-3004-1 and MIL-STD-3004-2) |
| 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 AIR9968B | Viscosity Test of Thickened Aircraft Deicing/Anti-icing Fluids |
| SAE ARP4902C | Design of Aircraft Deicing Facilities |
| I.S. EN 4697:2016 | AEROSPACE SERIES - GENERAL AND INSTALLATION REQUIREMENTS FOR PASSENGER SEAT FITTINGS |
| SAE AS6285 | 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 ARP5058B | Enclosed Operator’s Cabin for Aircraft Ground Deicing Equipment |
| SAE AS5901C | Water Spray and High Humidity Endurance Test Methods for SAE AMS1424 and SAE AMS1428 Aircraft Deicing/Anti-icing Fluids |
| SAE ARP6852B | Methods and Processes for Evaluation of Aerodynamic Effects of SAE-Qualified Aircraft Ground Deicing/Anti-icing Fluids |
| SAE AIR6284 | 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 AS6286 | Training and Qualification Program for Deicing/Anti-icing of Aircraft on the Ground |
| 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 AS5116C | Minimum Operational Performance Specification for Ground Ice Detection Systems |
| SAE AS5681B | Minimum Operational Performance Specification for Remote On-Ground Ice Detection Systems |
| SAE AIR5490A | Carbon Brake Contamination and Oxidation |
| ISO 11078:2007 | Aircraft — De-icing/anti-icing fluids — ISO types II, III and IV |
| UNE-EN 12312-6:2017 | Aircraft ground support equipment - Specific requirements - Part 6: Deicers and de-icing/anti-icing equipment |
| SAE AMS4049M | 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 AMS2475G | Protective Treatments Magnesium Alloys |
| ASTM D 1177 : 2017 : REDLINE | Standard Test Method for Freezing Point of Aqueous Engine Coolants |
| SAE AMS5886C | 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 °F (1149 °C) Solution Heat Treated |
| SAE AMS4911N | Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed |
| SAE AMS4376H | Plate, Magnesium Alloy 3.0Al - 1.0Zn - 0.20Mn (AZ31B-H26) Cold Rolled and Partially Annealed |
| SAE AMS4037Q | Aluminum Alloy, Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn (2024; -T3 Flat Sheet, -T351 Plate) Solution Heat Treated |
| SAE AIR9968B | 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 AMS1428/1 | Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV Glycol (Conventional and Non-Conventional) Based |
| SAE AMS1428/2 | Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV 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 AMSP83310A | Plastic Sheet, Polycarbonate, Transparent |
| SAE AS5900C | Standard Test Method for Aerodynamic Acceptance of AMS1424 and AMS1428 Aircraft Deicing/Anti-Icing Fluids |
| SAE ARP5485A | Endurance Time Tests for Aircraft Deicing/Anti-icing Fluids SAE Type II, III, and IV |
| SAE ARP 1917 : 2002 | CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS |
| SAE ARP4737H | Aircraft Deicing/Anti-icing Methods |
| SAE AS6285 | 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 AMS2825B | Material Safety Data Sheets |
| SAE AMS4916K | 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 ARP5718A | Process to Obtain Holdover Times for Aircraft Deicing/Anti-Icing Fluids, SAE AMS1428 Types II, III, and IV |
| SAE AS5901C | Water Spray and High Humidity Endurance Test Methods for SAE AMS1424 and SAE AMS1428 Aircraft Deicing/Anti-icing Fluids |
| SAE AMS2470N | Anodic Treatment of Aluminum Alloys Chromic Acid Process |
| SAE AMS5045J | Steel, Sheet and Strip 0.25 Carbon, Maximum Hard Temper |
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