SAE AIR 6232 : 2013
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
AIRCRAFT SURFACE COATING INTERACTION WITH AIRCRAFT DEICING/ANTI-ICING FLUIDS
Hardcopy , PDF
08-08-2020
English
01-01-2013
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FOREWORD
1. SCOPE
2. REFERENCES
3. COMPARATIVE FLUID ENDURANCE TIME TESTS
4. COMPARATIVE FLUID AERODYNAMIC TESTS
5. ADDITIONAL INFORMATIONAL TEST METHODS
6. NOTES
This SAE Aerospace Information Report (AIR) provides descriptions of test methods for determining if an aircraft surface coating of any thickness has adverse effects on aircraft deicing/anti-icing fluids with respect to fluid holdover time performance and aerodynamic performance.
| Committee |
G-12ADF
|
| DocumentType |
Revision
|
| Pages |
18
|
| ProductNote |
THIS STANDARD ALSO REFERS TO :AIP 94,AIP 97,APS 106,D6-17487
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| SAE AS 6285 : 2016 | AIRCRAFT GROUND DEICING/ANTI-ICING PROCESSES |
| SAE AS 6286 : 2016 | TRAINING AND QUALIFICATION PROGRAM FOR DEICING/ANTI-ICING OF AIRCRAFT ON THE GROUND |
| ISO 22007-3:2008 | Plastics Determination of thermal conductivity and thermal diffusivity Part 3: Temperature wave analysis method |
| SAE ARP 5945 : 2007 | ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE 1 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| SAE AMS 1424 : 2016 | FLUID, AIRCRAFT DEICING/ANTI-ICING, SAE TYPE 1 |
| ASTM D 5930 : 2017 : REDLINE | Standard Test Method for Thermal Conductivity of Plastics by Means of a Transient Line-Source Technique |
| SAE AMS 1428 : 2017 | FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN, (PSEUDOPLASTIC), SAE TYPES 2, 3 AND 4 |
| ASTM C 518 : 2017 : REDLINE | Standard Test Method for Steady-State Thermal Transmission Properties by Means of the Heat Flow Meter Apparatus |
| ISO 22007-4:2017 | Plastics — Determination of thermal conductivity and thermal diffusivity — Part 4: Laser flash method |
| SAE AMS 3095 : 2004 | PAINT: HIGH GLOSS FOR AIRLINE EXTERIOR SYSTEM |
| ISO 11507:2007 | Paints and varnishes Exposure of coatings to artificial weathering Exposure to fluorescent UV lamps and water |
| SAE AMS 1650 : 2001 | POLISH, AIRCRAFT METAL |
| SAE AS 5900 : 2016 | STANDARD TEST METHOD FOR AERODYNAMIC ACCEPTANCE OF AMS1424 AND AMS1428 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| SAE ARP 5485 : 2007 | ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE 2/3/4 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
| ISO 8301:1991 | Thermal insulation — Determination of steady-state thermal resistance and related properties — Heat flow meter apparatus |
| SAE ARP 4737 : 2008 | AIRCRAFT DEICING/ANTI-ICING METHODS |
| SAE AMS C 83231 : 2001 | COATINGS, POLYURETHANE, RAIN EROSION RESISTANT FOR EXTERIOR AIRCRAFT AND MISSILE PLASTIC PARTS |
| ISO 22007-2:2015 | Plastics Determination of thermal conductivity and thermal diffusivity Part 2: Transient plane heat source (hot disc) method |
| SAE AIR 6130 : 2011 | CADMIUM PLATE CYCLIC CORROSION TEST |
| ASTM E 1225 : 2013 : REDLINE | Standard Test Method for Thermal Conductivity of Solids Using the Guarded-Comparative-Longitudinal Heat Flow Technique |
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