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Standard

Water Spray and High Humidity Endurance Test Methods for SAE Ams 1424 and SAE Ams 1428 Aircraft Deicing/Anti-Icing Fluids

2003-02-10
HISTORICAL
AS5901
This document establishes the minimum requirements for an environmental test chamber, and test procedures to carry out anti-icing performance tests according to the current materials specification for aircraft deicing/anti-icing fluids. The primary purpose for such a test method is to determine the anti-icing endurance under controlled laboratory conditions of AMS 1424 Type I and AMS 1428 Type II, III and IV.
Standard

Standard Test Method for Aerodynamic Acceptance of SAE AMS 1424 and SAE AMS 1428 Aircraft Deicing/Anti-icing Fluids

2003-02-10
HISTORICAL
AS5900
This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements for SAE AMS 1424 Type I and SAE AMS 1428 Type II, III and IV. Fluids used to deice and/or anti-ice: a Large transport type jet aircraft while on the ground where the takeoff rotation speeds generally exceed approximately 100 to 110 knots. (The procedure for this type of aircraft is referred to as the High Speed Ramp Tests). and/or b Commuter type aircraft while on the ground and when no compensating measures are taken in the aircraft takeoff procedure where the takeoff rotation speeds generally exceed approximately 60 knots. (The procedure for this type of aircraft is referred to as the Low Speed Ramp Tests.) The objective of this standard is to ensure acceptable aerodynamic characteristics of the deicing/ anti-icing fluids as they flow off aircraft lifting and control surfaces during the takeoff ground acceleration and climb.
Standard

Standard Test Method for Aerodynamic Acceptance of SAE AMS 1424 and SAE AMS 1428 Aircraft Deicing/Anti-icing Fluids

2003-05-23
HISTORICAL
AS5900A
This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements for SAE AMS 1424 Type I and SAE AMS 1428 Type II, III and IV. Fluids used to deice and/or anti-ice: a Large transport type jet aircraft while on the ground where the takeoff rotation speeds generally exceed approximately 100 to 110 knots. (The procedure for this type of aircraft is referred to as the High Speed Ramp Tests). and/or b Commuter type aircraft while on the ground and when no compensating measures are taken in the aircraft takeoff procedure where the takeoff rotation speeds generally exceed approximately 60 knots. (The procedure for this type of aircraft is referred to as the Low Speed Ramp Tests.) The objective of this standard is to ensure acceptable aerodynamic characteristics of the deicing/ anti-icing fluids as they flow off aircraft lifting and control surfaces during the takeoff ground acceleration and climb.
Standard

Deicing/Anti-Icing Fluid, Aircraft, SAE Type 1

2003-07-22
HISTORICAL
AMS1424E
This specification covers a deicing/anti-icing material in the form of a fluid. The fluid is generally used heated either diluted with water, or as supplied, for the removal of, and time-limited protection against, deposits of frost, ice, and snow on exterior aircraft surfaces prior to takeoff. Consult aircraft manufacturer's maintenance manual and service letters to determine any restrictions relating to the use of deicing/anti-icing fluids for type and model of aircraft being treated. Refer also to SAE ARP 4737. The manufacturer shall determine and report the lowest operational use temperature (LOUT) for the recommended dilutions of their fluid(s). The LOUT for an SAE Type I fluid is the lowest temperature at which the fluid has been tested and certified in accordance with the appropriate aerodynamic acceptance tests (3.5.3) while maintaining the 10 degree C (18 degrees F) freezing point buffer (see SAE ARP 4737).
Standard

Deicing/Anti-Icing Fluid, Aircraft, SAE Type 1

2005-05-06
HISTORICAL
AMS1424F
This specification covers a deicing/anti-icing material in the form of a fluid. The fluid is generally used heated either diluted with water, or as supplied, for the removal of, and time-limited protection against, deposits of frost, ice, and snow on exterior aircraft surfaces prior to takeoff. Consult aircraft manufacturer's maintenance manual and service letters to determine any restrictions relating to the use of deicing/anti-icing fluids for type and model of aircraft being treated. Refer also to SAE ARP 4737. The manufacturer shall determine and report the lowest operational use temperature (LOUT) for the recommended dilutions of their fluid(s). The LOUT for an SAE Type I fluid is the lowest temperature at which the fluid has been tested and certified in accordance with the appropriate aerodynamic acceptance tests (3.5.3) while maintaining the 10 degree C (18 degrees F) freezing point buffer (see SAE ARP 4737).
Standard

Deicing/Anti-Icing Fluid, Aircraft, SAE Type 1

2001-08-01
HISTORICAL
AMS1424D
This specification covers a deicing/anti-icing material in the form of a fluid. The fluid is generally used heated either diluted with water, or as supplied, for the removal of, and time-limited protection against, deposits of frost, ice, and snow on exterior aircraft surfaces prior to takeoff. Consult aircraft manufacturer's maintenance manual and service letters to determine any restrictions relating to the use of deicing/anti-icing fluids for type and model of aircraft being treated. Refer also to ARP4737. The manufacturer shall determine and report the lowest operational use temperature (LOUT) for the recommended dilutions of their fluid(s). The LOUT for an SAE Type I fluid is the lowest temperature at which the fluid has been tested and certified in accordance with the appropriate aerodynamic acceptance tests (3.5.3) while maintaining the 10 degree C (18 degrees F) freezing point buffer (see ARP4737).
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