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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
Superseded date
29-10-2018
Superseded by
Language(s)
English
Published date
01-03-2017
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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Superseded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 |
| 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 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 |
| 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 |
| 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 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 |
| 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 |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.