SAE AMS1428L
Current
Current
The latest, up-to-date edition.
Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
14-02-2023
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.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.
| Committee |
G-12ADF
|
| DocumentType |
Revision
|
| Pages |
27
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| 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 AIR 9968 : 2015 | 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 ARP 571 : 1994 | FLIGHT DECK CONTROLS AND DISPLAYS FOR COMMUNICATION AND NAVIGATION EQUIPMENT FOR TRANSPORT AIRCRAFT |
| SAE AMS4911R | Titanium Alloy, Sheet, Strip, and Plate, 6Al - 4V, Annealed |
| SAE AMSP83310A | PLASTIC SHEET, POLYCARBONATE, TRANSPARENT |
| SAE ARP 5485 : 2017 | ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE 2/3/4 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| SAE AMS2470P | Anodic Treatment of Aluminum Alloys, Chromic Acid Process<br> |
| 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:2021 | 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<br> |
| 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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