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SAE AIR 6232 : 2013

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

AIRCRAFT SURFACE COATING INTERACTION WITH AIRCRAFT DEICING/ANTI-ICING FLUIDS
Available format(s)

Hardcopy , PDF

Superseded date

08-08-2020

Language(s)

English

Published date

01-01-2013

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Superseded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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