Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

02-14-2023

Publisher

SAE International

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 AMS 1428K : 2018

SAE ARP 4737 : 2017	AIRCRAFT DEICING/ANTI-ICING METHODS
SAE AMS2475:2009(S2019)	PROTECTIVE TREATMENTS, MAGNESIUM ALLOYS
SAE AMS 5045K : 2019	Steel, Sheet and Strip, 0.25 Carbon, Maximum, Hard Temper
SAE AMS4916M:2017(S2022)	Titanium Alloy Sheet, Strip, and Plate 8Al - 1Mo - 1V Duplex Annealed
SAE AMS 4376 : 2011(R2018)	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:2020	Aluminum Alloy, Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn (2024; -T3 Flat Sheet, -T351 Plate) Solution Heat Treated
SAE ARP 1917 : 2013	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:2019	Titanium Alloy, Sheet, Strip, and Plate, 6Al - 4V, Annealed
SAE AMS P 83310 : 2016	PLASTIC SHEET, POLYCARBONATE, TRANSPARENT
SAE ARP 5485 : 2017	ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE 2/3/4 AIRCRAFT DEICING/ANTI-ICING FLUIDS
SAE AMS 2470P : 2019	Anodic Treatment of Aluminum Alloys, Chromic Acid Process<br>
SAE AMS4049N:2022	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 AMS 5886D : 2020	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 AMS 4041T : 2019	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 AMS 2825 : 1987	MATERIAL SAFETY DATA SHEETS