SAE AMS1424M
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Deicing/Anti-Icing Fluid, Aircraft SAE Type 1
Available format(s)
Hardcopy , PDF
Superseded date
14-09-2019
Superseded by
Language(s)
English
Published date
03-05-2016
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.This foundation specification (AMS1424P) and its associated category specifications (AMS1424/1 and AMS1424/2) cover a deicing/anti-icing material in the form of a fluid
| DocumentType |
Standard
|
| Pages |
17
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This foundation specification (AMS1424M) and its associated category specifications (AMS1424/1 and AMS1424/2) cover a deicing/anti-icing material in the form of a fluid.
| 15/30332965 DC : 0 | BS EN 6059-303 - AEROSPACE SERIES - PROTECTION SLEEVES - TEST METHODS - PART 303: RESISTANCE TO FLUIDS |
| SAE AS5116C | Minimum Operational Performance Specification for Ground Ice Detection Systems |
| MIL-PRF-32517 Base Document:2015 | SPLICE, CONDUCTOR, ELECTRICAL, COAXIAL CABLE, MATCHED IMPEDANCE, GENERAL SPECIFICATION FOR |
| SAE ARP6207 | Qualifications Required for SAE Type I Aircraft Deicing/Anti-Icing Fluids |
| I.S. EN 3155-068:2009 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 068: CONTACTS, ELECTRICAL, COAXIAL, SIZE 08, FEMALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| SAE ARP4737J | Aircraft Deicing/Anti-Icing Methods |
| SAE AS5272E | Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, Procurement Specification |
| MIL-PRF-24667 Revision C:2008 | COATING SYSTEM, NON-SKID, FOR ROLL, SPRAY, OR SELF-ADHERING APPLICATION |
| 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 |
| MIL-PRF-83383 Revision F:2017 | Circuit Breakers, Remote Control, Thermal, Trip Free General Specification For |
| 09/30210064 DC : DRAFT SEP 2009 | BS EN 4531-001 - AEROSPACE SERIES - CONNECTORS, OPTICAL, CIRCULAR, SINGLE AND MULTIPIN, COUPLED BY THREADED RING - FLUSH CONTACTS - PART 001: TECHNICAL SPECIFICATION |
| MIL-PRF-32577 Base Document:2017 | Coating System, Nonskid, Metallic Thermal Spray Application |
| BS EN 3155-067:2009 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, size 08, male, type D, solder, class R. Product standard |
| MIL-DTL-32149 Revision A:2007 | CLOTH, WATERPROOF, FLAME RESISTANT, MOISTURE VAPOR PERMEABLE |
| PREN 4697 : 200P2 | AEROSPACE SERIES - GENERAL AND INSTALLATION REQUIREMENTS FOR PASSENGER SEAT FITTINGS |
| SAE AS81714B | Terminal Junction System (TJS), Environment Resistant General Specification For |
| PREN 3155-067 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 067: CONTACTS, ELECTRICAL, COAXIAL, SIZE 08, MALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| PREN 3155-025 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 025: CONTACTS, ELECTRICAL, TRIAXIAL, SIZE 8, FEMALE D, CRIMP, CLASS S - PRODUCT STANDARD |
| SAE AMS1424/1 | Deicing/Anti-Icing Fluid, Aircraft SAE Type I Glycol (Conventional and Non-Conventional) Based |
| PREN 3545-001 : 200P4 | AEROSPACE SERIES - CONNECTORS, ELECTRICAL, RECTANGULAR, WITH SEALED AND NON-SEALED REAR, PLASTIC HOUSING, LOCKING DEVICE, OPERATING TEMPERATURES -55 DEGREES C TO 175 DEGREES C - PART 001: TECHNICAL SPECIFICATION |
| SAE ARD 50102 : 2002 | FORCED AIR OR FORCED AIR/FLUID EQUIPMENT FOR REMOVAL OF FROZEN CONTAMINANTS |
| I.S. EN 3733-001:2009 | AEROSPACE SERIES - CONNECTOR, OPTICAL, CIRCULAR, SINGLE CHANNEL, COUPLED BY SELF-LOCKING RING, OPERATING TEMPERATURE UP TO 150 DEGREES C CONTINUOUS - PART 001: TECHNICAL SPECIFICATION |
| SAE AS81820D | Bearings, Plain, Self-Aligning, Self-Lubricating, Low Speed Oscillation |
| SAE AS5900C | Standard Test Method for Aerodynamic Acceptance of AMS1424 and AMS1428 Aircraft Deicing/Anti-Icing Fluids |
| SAE AMS3255B | Sealing Tape, Sheet, or Gasket, Polytetrafluoroethylene, Expanded (EPTFE) Oil and Water Resistant |
| BS EN 3155-039:2007 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, size 16, female, type D, solder, class R. Product standard |
| BS EN 3372-001:2007 | Aerospace series. Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures -65°C to 175°C or 200°C continuous Technical specification |
| BS EN 3545-001:2008 | Aerospace series. Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55°C to 175°C Technical specification |
| EN 12312-6:2017 | Aircraft ground support equipment - Specific requirements - Part 6: Deicers and de-icing/anti-icing equipment |
| BS EN 3733-001:2009 | Aerospace series. Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150°C continuous Technical specification |
| BS ISO 11075:2007 | Aircraft. De-icing/anti-icing fluids. ISO type I |
| SAE AS 23053 : 2016 | INSULATION SLEEVING, ELECTRICAL, HEAT SHRINKABLE, GENERAL SPECIFICATION FOR |
| 14/30298727 DC : 0 | BS EN 3155-024 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 024: CONTACTS, ELECTRICAL, TRIAXIAL, SIZE 8, MALE, TYPE D, CRIMP, CLASS S - PRODUCT STANDARD |
| SAE AIR 6232 : 2013 | AIRCRAFT SURFACE COATING INTERACTION WITH AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| SAE AS8942 | Bearings, Plain and PTFE Lined, Self - Aligning |
| 14/30298728 DC : 0 | BS EN 3155-025 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 025: CONTACTS, ELECTRICAL, TRIAXIAL, SIZE 8, FEMALE, TYPE D, CRIMP, CLASS S - PRODUCT STANDARD |
| MIL-DTL-3702 Revision F:2012 | CABLE, POWER, ELECTRICAL: IGNITION, HIGH-TENSION |
| MIL-DTL-83528 Revision H:2018 | Gasketing Material, Conductive, Shielding Gasket, Electronic, Elastomer, EMI/RFI, General Specification for |
| FAA AC 135-16 : 0 | GROUND DEICING AND ANTI-ICING TRAINING AND CHECKING |
| SAE AS83819 | Bearings, Plain, Self-Aligning, Self-Lubricating, 1400 cpm (15 fpm), Oscillation, -65 to +160 °F (-54 to +71 °C) |
| SAE ARP5718B | Qualifications Required for SAE Type II/III/IV Aircraft Deicing/Anti-Icing Fluid |
| SAE AIR786B | Elastomer Compatibility Considerations Relative to Elastomeric Sealant Selection |
| SAE AS 1701 : 2017 | LUBRICANT, SOLID FILM |
| 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 3545-001:2008 | AEROSPACE SERIES - CONNECTORS, ELECTRICAL, RECTANGULAR, WITH SEALED AND NON-SEALED REAR, PLASTIC HOUSING, LOCKING DEVICE, OPERATING TEMPERATURES -55 DEGREES C TO 175 DEGREES C - PART 001: TECHNICAL SPECIFICATION |
| I.S. EN 12312-6:2017 | AIRCRAFT GROUND SUPPORT EQUIPMENT - SPECIFIC REQUIREMENTS - PART 6: DEICERS AND DE-ICING/ANTI-ICING EQUIPMENT |
| SAE AS82819 | Bearings, Plain, Self-Aligning, Self-Lubricating, 300 cpm Oscillation (13 fpm), -65 to +160 °F (-54 to +71 °C), Liners Less Than 0.015 inches |
| MIL-PRF-81975 Revision C:2008 | COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
| MIL-DTL-83723-27 Revision C:2015 | CONNECTORS, ELECTRICAL, BACKSHELL, WITH HEAT-SHRINKABLE STRAIN-RELIEF BOOT (STRAIGHT AND RIGHT ANGLE), THREADED COUPLING |
| MIL-DTL-26482 Revision H:2007 | Connectors, Electrical, Circular, Miniature, Quick Disconnect, Environment Resisting, Receptacles and Plugs, General Specification for |
| MIL-PRF-46010 Revision H:2013 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING NATO CODE S-1738 |
| SAE AS81934B | Bearings, Sleeve, Plain and Flanged, Self-Lubricating |
| MIL-PRF-32058 Revision B:2017 | CHOCK, WHEEL-TRACK - AVIATION, ADJUSTABLE ROPE TYPE |
| BS EN 3155-069:2009 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, size 16, female, type D, solder, class P. Product standard |
| 13/30291179 DC : 0 | BS EN 4697 - AEROSPACE SERIES - GENERAL AND INSTALLATION REQUIREMENTS FOR PASSENGER SEAT FITTINGS |
| FAA AC 120-60 : 2004 | GROUND DEICING AND ANTI-ICING PROGRAM |
| MIL-STD-3004 Revision D:2014 | QUALITY ASSURANCE/SURVEILLANCE FOR FUELS, LUBRICANTS AND RELATED PRODUCTS |
| SAE AS22759C | Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy |
| SAE ARP4902C | Design of Aircraft Deicing Facilities |
| SAE ARP5945A | Endurance Time Test Procedures for SAE Type I Aircraft Deicing/Anti-Icing Fluids |
| I.S. EN 4697:2016 | AEROSPACE SERIES - GENERAL AND INSTALLATION REQUIREMENTS FOR PASSENGER SEAT FITTINGS |
| SAE AS6285 | Aircraft Ground Deicing/Anti-Icing Processes |
| ISO 11075:2007 | Aircraft — De-icing/anti-icing fluids — ISO type I |
| MIL-PRF-57267 Base Document:2017 | COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
| UNE-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 ARP5058B | Enclosed Operator’s Cabin for Aircraft Ground Deicing Equipment |
| 16/30350072 DC : 0 | BS EN 3155-024 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 024: CONTACTS, ELECTRICAL, TRIAXIAL, SIZE 8, MALE, TYPE D, CRIMP, CLASS S - PRODUCT STANDARD |
| 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 AMS3604 | Heat Resistant Aluminized Paint |
| SAE AS7928B | Terminals, Lug: Splices, Conductor: Crimp Style, Copper, General Specification For |
| SAE AS60491 | Sleeve, Protection, For Cable and Harness Protection |
| SAE AIR6284 | Forced Air or Forced Air/Fluid Equipment for Removal of Frozen Contaminants |
| SAE AMS1424/2 | Deicing/Anti-Icing Fluid, Aircraft SAE Type I Non-Glycol Based |
| SAE AS85560B | Bearings, Fiber Reinforced Plastic, Sleeve, Plain and Flanged, Self-Lubricating; General Specification For |
| 13/30278621 DC : 0 | BS EN 4165-001 - AEROSPACE SERIES - CONNECTORS, ELECTRICAL, RECTANGULAR, MODULAR - OPERATING TEMPERATURE 175 DEGREES C CONTINUOUS - PART 001: TECHNICAL SPECIFICATION |
| BS EN 3155-068:2009 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, size 08, female, type D, solder, class R. Product standard |
| MIL-STD-2161 Revision C:2014 | Paint Schemes and Exterior Markings for U.S. Navy and Marine Corps Aircraft |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| PREN 6059-303 : 200P3 | AEROSPACE SERIES - ELECTRICAL CABLES, INSTALLATION - PROTECTION SLEEVES - TEST METHODS - PART 303: RESISTANCE TO FLUIDS |
| SAE AS 81582 : 2017 | CONNECTORS, ELECTRICAL, BAYONET COUPLING, ENVIRONMENT RESISTING, UMBILICAL, GENERAL SPECIFICATION FOR |
| SAE AS 6224 : 2015 | WRAP-AROUND INSULATION REPAIR AND PROTECTION SLEEVE, PERMANENT, ELECTRIC, ENVIRONMENT RESISTANT |
| BS EN 6059-303:2017 | Aerospace series. Electrical cables, installation. Protection sleeves. Test methods Resistance to fluids |
| BS EN 3716-001:2006 | Aerospace series. Connectors, single-way, with triaxial interface, for transmission of digital data Technical specification |
| BS EN 3155-041:2007 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, size 12, female, type D, solder, class R. Product standard |
| BS EN 3155-025:2006 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, triaxial, size 8, female, type D, crimp, class S. Product standard |
| BS EN 3708-001:2006 | Aerospace series. Modular interconnection systems. Terminal junction systems Technical specification |
| BS EN 3155-040:2007 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, size 12, male, type D, solder, class R. Product standard |
| BS EN 3155-024:2006 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, triaxial, size 8, male, type D, crimp, class S. Product standard |
| EN 3708-001:2006 | Aerospace series - Modular interconnection systems - Terminal junction systems - Part 001: Technical specification |
| EN 3155-040:2007 | Aerospace series - Electrical contacts used in elements of connection - Part 040: Contacts, electrical, coaxial, size 12, male, type D, solder, class R - Product standard |
| EN 4697:2016 | Aerospace series - General and installation requirements for passenger seat fittings |
| EN 3155-068:2009 | Aerospace series - Electrical contacts used in elements of connection - Part 068: Contacts, electrical, coaxial, size 08, female, type D, solder, class R - Product standard |
| EN 3155-025:2006 | Aerospace series - Electrical contacts used in elements of connection - Part 025: Contacts, electrical, triaxial, size 8, female, type D, crimp, class S - Product standard |
| EN 3155-067:2009 | Aerospace series - Electrical contacts used in elements of connection - Part 067: Contacts, electrical, coaxial, size 08, male, type D, solder, class R - Product standard |
| EN 3372-001:2007 | Aerospace series - Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures - 65 °C to 175 °C or 200 °C continuous - Part 001: Technical specification |
| EN 3733-001:2009 | Aerospace series - Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous - Part 001: Technical specification |
| EN 3218-001:2006 | Aerospace series - Connectors, rectangular, with metallic shells and screw-locking - Part 001: Technical specification |
| EN 6059-303:2017 | Aerospace series - Electrical cables, installation - Protection sleeves - Test methods - Part 303: Resistance to fluids |
| EN 3155-041:2007 | Aerospace series - Electrical contacts used in elements of connection - Part 041: Contacts, electrical, coaxial, size 12, female, type D, solder, class R - Product standard |
| EN 3716-001:2006 | Aerospace series - Connector, single-way, with triaxial interface, for transmission of digital data - Part 001: Technical specification |
| EN 3545-001:2008 | Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 °C to 175 °C - Part 001: Technical specification |
| EN 3155-069:2009 | Aerospace series - Electrical contacts used in elements of connection - Part 069: Contacts, electrical, coaxial, size 16, female, type D, solder, class P - Product standard |
| EN 3155-024:2006 | Aerospace series - Electrical contacts used in elements of connection - Part 024: Contacts, electrical, triaxial, size 8, male, type D, crimp, class S - Product standard |
| EN 3155-039:2007 | Aerospace series - Electrical contacts used in elements of connection - Part 039: Contacts, electrical, coaxial, size 16, female, type D, solder, class R - Product standard |
| FAA AC 20-73 : 2006 | AIRCRAFT ICE PROTECTION |
| SAE AS 5258 : 2012 | INSULATING COMPONENT, MOLDED, ELECTRICAL, HEAT SHRINKABLE, CONNECTOR AND CABLE ACCESSORY, SEALING STRAIN RELIEF, GENERAL SPECIFICATION FOR |
| SAE AS 81511 : 2016 | CONNECTORS, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING AND ACCESSORIES, GENERAL SPECIFICATION FOR |
| I.S. EN 6059-303:2017 | AEROSPACE SERIES - ELECTRICAL CABLES, INSTALLATION - PROTECTION SLEEVES - TEST METHODS - PART 303: RESISTANCE TO FLUIDS |
| 16/30350073 DC : 0 | BS EN 3155-025 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 025 - CONTACTS, ELECTRICAL, TRIAXIAL, SIZE 8, FEMALE, TYPE D, CRIMP, CLASS S - PRODUCT STANDARD |
| MIL-DTL-83420 Revision P:2017 | WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR |
| PREN 3155-024 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 024: CONTACTS, ELECTRICAL, TRIAXIAL, SIZE 8, MALE, TYPE D, CRIMP, CLASS S - PRODUCT STANDARD |
| PREN 3155-068 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 068: CONTACTS, ELECTRICAL, COAXIAL, SIZE 08, FEMALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| SAE AS5681B | Minimum Operational Performance Specification for Remote On-Ground Ice Detection Systems |
| SAE AS81824D | Splice, Electric, Crimp, Copper, Environment Resistant |
| SAE AS85485B | Cable, Electric, Filter Line, Radio Frequency Absorptive |
| SAE AIR5490A | Carbon Brake Contamination and Oxidation |
| SAE AS83519C | Shield Termination, Solder Style, Insulated, Heat-Shrinkable, Environment Resistant General Specification For |
| I.S. EN 3155-069:2009 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 069: CONTACTS, ELECTRICAL, COAXIAL, SIZE 16, FEMALE, TYPE D, SOLDER, CLASS P - PRODUCT STANDARD |
| PREN 3155-069 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 069: CONTACTS, ELECTRICAL, COAXIAL, SIZE 16, FEMALE, TYPE D, SOLDER, CLASS P - PRODUCT STANDARD |
| SAE AS6286 | Training and Qualification Program for Deicing/Anti-icing of Aircraft on the Ground |
| I.S. EN 3155-067:2009 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 067: CONTACTS, ELECTRICAL, COAXIAL, SIZE 08, MALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| BS EN 3218-001:2006 | Aerospace series. Connectors, rectangular, with metallic shells and screw-locking Technical specification |
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.