SAE AS5900C
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Standard Test Method for Aerodynamic Acceptance of AMS1424 and AMS1428 Aircraft Deicing/Anti-Icing Fluids
Hardcopy , PDF
06-08-2020
English
25-10-2016
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1. SCOPE
2. REFERENCES
3. GENERAL INFORMATION
4. TEST FACILITY REQUIREMENTS
5. TEST FLUID REQUIREMENTS
6. TEST PROCEDURE
7. DEICING/ANTI-ICING FLUID ACCEPTANCE CRITERIA
8. TEST RESULTS
9. REPORT
10. NOTES
Sets up the aerodynamic flow-off requirements and test procedures for AMS1424 Type I and AMS1428 Type II, III and IV fluids used to deice and/or anti-ice aircraft.
| DocumentType |
Standard
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| Pages |
28
|
| PublisherName |
SAE International
|
| Status |
Superseded
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| SupersededBy | |
| Supersedes |
This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements and test procedures for AMS1424 Type I and AMS1428 Type II, III and IV fluids used to deice and/or anti-ice aircraft.The objective of this standard is to ensure acceptable aerodynamic characteristics of the deicing/anti-icing fluids as they flow off of aircraft lifting and control surfaces during the takeoff ground acceleration and climb. Aerodynamic acceptance of an aircraft ground deicing/anti-icing fluid is based upon the fluid’s boundary layer displacement thickness (BLDT) on a flat plate, measured after experiencing the free stream velocity time history of a representative aircraft takeoff. Acceptability of the fluid is determined by comparing BLDT measurements of the candidate fluid with a datum established from the values of a reference fluid BLDT and the BLDT over the dry (clean) test plate. Testing is carried out in the temperature range at which the fluid, undiluted and diluted, is to be used in airline service.NOTE: No additional testing is required for non-glycol fluids at this time. For more information about non-glycol fluids please refer to AMS1424.
| SAE ARP6207 | Qualifications Required for SAE Type I Aircraft Deicing/Anti-Icing Fluids |
| SAE AMS1428J | Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV |
| SAE AIR 6232 : 2013 | AIRCRAFT SURFACE COATING INTERACTION WITH AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| SAE ARP5718B | Qualifications Required for SAE Type II/III/IV Aircraft Deicing/Anti-Icing Fluid |
| SAE ARP5945A | Endurance Time Test Procedures for SAE Type I Aircraft Deicing/Anti-Icing Fluids |
| SAE AS6285 | Aircraft Ground Deicing/Anti-Icing Processes |
| SAE ARP6852B | Methods and Processes for Evaluation of Aerodynamic Effects of SAE-Qualified Aircraft Ground Deicing/Anti-icing Fluids |
| SAE AS6286 | Training and Qualification Program for Deicing/Anti-icing of Aircraft on the Ground |
| SAE AMS1424N | Fluid, Aircraft Deicing/Anti-Icing, SAE Type 1 |
| SAE AMS1424M | Deicing/Anti-Icing Fluid, Aircraft SAE Type 1 |
| SAE AMS1428J | Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV |
| ASTM E 70 | TEST METHOD FOR PH OF AQUEOUS SOLUTIONS WITH THE GLASS ELECTRODE |
| ASTM D 1331 : 2014 : REDLINE | Standard Test Methods for Surface and Interfacial Tension of Solutions of Paints, Solvents, Solutions of Surface-Active Agents, and Related Materials |
| SAE ARP6852B | Methods and Processes for Evaluation of Aerodynamic Effects of SAE-Qualified Aircraft Ground Deicing/Anti-icing Fluids |
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