SAE AMS1428L
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
Hardcopy , PDF
English
02-14-2023
06-27-2025
This foundation specification (AMS1428L) 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.
| DocumentType |
Standard
|
| Pages |
27
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This foundation specification (AMS1428L) 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 ARP4737J | Aircraft Deicing/Anti-Icing Methods |
| SAE AMS2475H | Protective Treatments Magnesium Alloys |
| SAE AMS5045K | Steel, Sheet and Strip 0.25 Carbon, Maximum Hard Temper |
| SAE AMS4916M | Titanium Alloy Sheet, Strip, and Plate 8Al - 1Mo - 1V Duplex Annealed |
| SAE AMS4376H | Plate, Magnesium Alloy 3.0Al - 1.0Zn - 0.20Mn (AZ31B-H26) Cold Rolled and Partially Annealed |
| SAE AIR9968B | Viscosity Test of Thickened Aircraft Deicing/Anti-icing Fluids |
| SAE AMS4037R | Aluminum Alloy, Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn (2024; -T3 Flat Sheet, -T351 Plate) Solution Heat Treated |
| SAE ARP1917A | Clarification of Terms Used in Aerospace Metals Specifications |
| SAE AMS4911R | Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed |
| SAE AMSP83310A | Plastic Sheet, Polycarbonate, Transparent |
| SAE ARP5485B | Endurance Time Test Procedures for SAE Type II/III/IV Aircraft Deicing/Anti-Icing Fluids |
| SAE AMS2470P | Anodic Treatment of Aluminum Alloys Chromic Acid Process |
| SAE AMS4049N | 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 AS5900E | Standard Test Method for Aerodynamic Acceptance of AMS1424 and AMS1428 Aircraft Deicing/Anti-Icing Fluids |
| SAE AMS5886D | 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 AMS4041T | Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (2024, -T3 Sheet/-T351 Plate with 1-1/2% Alclad) Solution Heat Treated, Cold Worked and Naturally Aged |
| SAE AMS2825B | Material Safety Data Sheets |
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