ICAO Abbreviations and Terms Applicable to Aircraft De-icing & Anti-icing

Posted by on in Regulatory
  • Font size: Larger Smaller
  • Hits: 101

Sofema Online (SOL) www.sofemaonline.com considers the typical terms and abbreviations compliant
with ICAO Document 9640 and SAE AS6285E

Abbreviations and Terms

Active frost: Condition when frost is forming. Active frost occurs when
(1) the aircraft surface temperature is at or below the frost point, or
(2) there is water in liquid form (e.g., dew) on the aircraft surface and the surface falls to/or
below 0 °C (frozen dew).


Anti-icing: Procedure by which fluid is applied to protect against the formation of frost or ice
or the accumulation of snow or slush on treated surfaces of an aircraft for a limited period.
Anti-icing fluid:
1. Mixture of water and Type I fluid.
2. Premix Type I fluid.
3. Type II, III, or IV fluids.
4. Mixture of water and Type II, III, or IV fluids.


Note: For deicing/anti-icing purposes in a one-step procedure, fluids in 1, 2, and 4 shall be heated to
ensure a temperature of 60 °C (140 °F) minimum at the nozzle.


Anti-icing code: Report given to the flight crew that deicing/anti-icing has been carried out and the
details of the anti-icing procedure that was applied. Also known as post-deicing/anti-icing report.
Cold-soak effect. The wings of airplanes are said to be “cold-soaked” when they contain very cold fuel
as a result of having just landed after a flight at high altitude or from having been refueled with very cold
fuel.
Cold-soaking: Ice can form on aircraft surfaces even when the outside air temperature (OAT) is well
above 0 °C (32 °F). An aircraft equipped with wing fuel tanks may have fuel that is at a sufficiently low
temperature such that it lowers the wing skin temperature to below the freezing point of water.


 The following factors contribute to cold soaking:
o temperature and quantity of fuel in fuel cells,
o type and location of fuel cells,
o length of time at high altitude,
o temperature of refueled fuel and
o time since refueling.
 While on the ground, the cold-soaked aircraft will cause ice to form when water as rain or as
vapor (humidity), comes in contact with cold-soaked surfaces.

Clear ice. Whenever precipitation falls on a cold-soaked airplane when on the ground, clear icing may
occur.
 Even in ambient temperatures between –2°C and +15°C, ice or frost can form in the presence of
visible moisture or high humidity if the airplane structure remains at 0°C or below.


Note - Clear ice is very difficult to detect visually and may break loose during or after take-off.
Critical surfaces.
 Wings, control surfaces, propellers, horizontal stabilizers, vertical stabilizers, or any other
stabilizing surface on an aircraft.
 These surfaces should be completely free of ice, snow, slush, or frost before take-off.
o The critical surfaces should be determined by the aircraft manufacturer.

Certificate of analysis: A document, issued by a manufacturer, attesting that a lot or batch of a product
fulfills the manufacturer’s sales specification requirements, listing the tests, the test requirements, the
test results on that lot or batch, the lot or batch number, and a date.


Certificate of conformance: A document declaring that a product fulfills the requirements of a standard.
Also known as a certificate of conformity.
Check: Examination against a relevant standard by a trained and qualified person to ascertain
satisfactory condition.
Chemical contamination (Contamination): Condition when substances (chemicals) are present where
they should not be or are at concentrations higher than they should be.
Contamination check: A check of aircraft surfaces and components for contamination to establish the
need for deicing.


De-icing. The process removes ice, snow, slush, or frost from aircraft surfaces.
De-icing/anti-icing. A procedure combining both the de-icing process and the anti-icing process 
can be performed in one or two steps:


 One-step de-icing/anti-icing. This procedure is carried out with heated anti-icing fluid. The fluid
is used to de-ice the aircraft and remains on the surfaces to provide anti-icing capability.


 Two-step de-icing/anti-icing. This procedure contains two distinct steps. The first step, de-icing,
is followed by the second step, anti-icing, as a separate fluid application. After de-icing, a
separate overspray of anti-icing fluid is applied to protect the aircraft’s critical surfaces, thus
providing maximum anti-icing protection.


Drizzle. Fairly uniform precipitation composed exclusively of fine drops (diameter less than 0.5 mm (0.02
in)) very close together. Drizzle appears to float while following air currents although, unlike fog
droplets, drizzle falls to the ground.
Deicing fluid:
1. Heated water.

2. Heated mixture of water and Type I fluid.
3. Heated premix Type I fluid.
4. Heated Type II, III, or IV fluids.
5. Heated mixture of water and Type II, III, or IV fluids.


NOTE: Unheated fluids are ineffective in de-icing.


Deicing service provider: The company responsible for the aircraft deicing/anti-icing operations on an
airfield.
Deicing personnel: Groundcrew personnel with roles and responsibilities associated with aircraft ground
icing operations.
Dewpoint: the temperature at which unsaturated air must be cooled to cause saturation concerning
liquid water.
 The moisture condenses to liquid water either on surfaces as dew or as tiny liquid droplets
suspended in air.
Fog and ground fog. A visible aggregate of minute water particles (droplets) in the air reduces the
horizontal visibility at the Earth’s surface to less than 1 kilometer.
Freezing fog. Fog is formed of supercooled water droplets that freeze upon contact with exposed
objects and form a coating of rime/clear ice.
 Generally, reduces the horizontal visibility at the earth’s surface to less than 1 km (5/8 mile).
Freezing drizzle. drizzle in the form of supercooled water drops which freeze upon impact with any
surface. Fairly uniform precipitation composed exclusively of fine drops [diameter less than 0.5 mm
(0.02 inch)] very close together, which freezes upon impact with the ground or other exposed objects.
Frost. A deposit of small, white ice crystals formed on the ground or other surfaces. Frost is formed by
sublimation, i.e. when water vapor is deposited upon a surface whose temperature is at or below
freezing.
Freezing point: Temperature at which a liquid starts to become a solid.
Freezing point buffer: The difference between the outside air temperature (OAT) and the freezing point
of the fluid used.
Freezing point buffer, negative: Condition when the freezing point of a deicing/anti-icing fluid is above
the OAT.
Freezing rain
 Light: Precipitation of liquid water particles that freeze upon impact with the ground or other
exposed objects, either in the form of drops of more than 0.5 mm (0.02 inch) or smaller drops
which, in contrast to drizzle, are widely separated.

The measured intensity of liquid water particles is up to 2.5 mm/h (0.10 in/h) or 25 g/dm2/h
with a maximum of 0.25 mm (0.01 inch) in 6 minutes.

 Moderate: Precipitation of liquid water particles that freeze upon impact with the ground or
other exposed objects.
o Moderate freezing rain may appear in the form of large drops or can appear to fall in
sheets where individual drops are not identifiable. Moderate freezing rain has a
measured intensity of between 0.10 to 0.30 in/h.

 Heavy: Precipitation of liquid water particles that freeze upon impact with the ground or
other exposed objects.
o Heavy freezing rain can seem to fall in sheets and individual drops may not be
identifiable. Heavy freezing rain has a measured intensity of more than 0.30 in/h.
Frost/hoarfrost: Tiny ice crystals formed on a surface at or below the frost point. Frost generally occurs
with clear skies at temperatures below freezing point. Frost can also occur from the freezing of dew.
 Frost, local: The limited formation of frost in localized wing areas cooled by cold fuel or large
masses of cold metal in the wing structure; this type of frost does not cover the entire wing.
 Frost point: temperature, at or below 0 °C, at which air undersaturated with moisture must be
cooled (at constant pressure) to cause saturation for ice.
o The moisture directly deposits, without going through the liquid phase, as frost on
exposed surfaces provides nucleation sites.
o The frost point is higher (warmer) than the dew point by about 10% at a given humidity
level in the air. Air temperature readings given by a thermometer apply to the
height above ground of the thermometer itself.
o Because cool air sinks and the ground often cools very quickly, especially on clear nights,
the ground temperature on clear, still nights is invariably lower than the temperature
only a few feet higher.
o Thus, frost can form even when a thermometer gives a reading above freezing. The
same happens with aircraft—frost can form on aircraft when the thermometer air
temperature reading is above 0 °C.

Fuel frost: Frost, normally in the area of the wing fuel tanks, is caused by the cold-soaking. Also known as
non-environmental frost or cold-soaked fuel frost.
Groundcrew: Personnel with responsibilities for the handling, maintenance, and servicing of an aircraft
while on the ground, as well as the coordination of these activities.
High humidity. An atmospheric condition where the relative humidity is close to saturation.
Hoar frost. A greyish-white crystalline deposit of frozen water vapor formed on surfaces in clear, still
weather.

(Note — this differs from the World Meteorological Organization (WMO) definition of hoar frost
for this document.)
Holdover time. Holdover time (HOT) is the estimated time the anti-icing fluid will prevent the formation
of ice and frost and the accumulation of snow on the protected (treated) surfaces of an airplane.
Hail: Precipitation of small balls or pieces of ice with a diameter ranging from 5 to 50 mm (0.2 to >2.0
inches) falling either separately or agglomerated.
Highest on-wing viscosity (HOWV): The highest viscosity of a thickened deicing/anti-icing fluid that is still
aerodynamically acceptable.
Hoarfrost: A synonym for frost. See frost/hoarfrost.
Holdover time: Estimated time for which an anti-icing fluid will prevent the formation of frost or ice and
the accumulation of snow on the treated surfaces of an aircraft.
Ice pellets: Precipitation of transparent (grains of ice) or translucent (small hail) pellets of ice, which are
spherical or irregular, and have a diameter of 5 mm (0.2 inch) or less. Ice pellets usually bounce when
hitting hard ground.
Lowest on-wing viscosity (LOWV): Lowest viscosity of a thickened deicing/anti-icing fluid for which the
applicable holdover timetable can still be used.
Lowest operational use temperature (LOUT): The LOUT is the higher (warmer) of:
 The lowest temperature at which the fluid meets the aerodynamic acceptance test (according to
AS5900) for a given type (high speed or low speed) of aircraft, or
 The freezing point of the fluid plus the buffer of 10 °C (18 °F) for Type I fluid and 7 °C (13 °F) for
Type II, III, or IV fluids.
Post-deicing check: A check by qualified ground personnel to ensure that all critical surfaces are free of
adhering to contamination after the deicing procedure has been completed.
Post-deicing/anti-icing check: A check by qualified ground personnel to ensure that all critical surfaces
are free of adhering contamination after the deicing/anti-icing procedure has been completed.
Post-deicing/anti-icing report: A report given to the flight crew confirming that deicing/anti-icing has
been carried out and the details of the deicing/anti-icing procedure that was applied.
Pre-deicing process: A process to remove large quantities of frozen contamination before the regular
deicing/anti-icing process to reduce the quantity of deicing fluid to be used.
Pre-flight contamination check: A check performed by the flight crew or groundcrew before departure
to verify the presence of adhering contamination to establish the need for deicing/anti-icing. It may be
part of the flight crew walk-around before the flight.
Pre-takeoff check: A check by the flight crew before takeoff and within holdover time. This check is
normally conducted from inside the flight deck. It is normally accomplished by a continuous assessment of the conditions that affect holdover time and includes an assessment and adjustment of holdover
time.
Pre-takeoff contamination check: A check of the critical surfaces for adhering contamination. This check
is accomplished after the holdover time has been exceeded and must be completed within 5 minutes
before the beginning of takeoff.
Proximity sensor: A proximity sensor is a safety feature on some models of deicing equipment that,
upon activation, disengages relevant systems, preventing equipment movement and damage from
occurring due to physical contact between equipment components (e.g., spray nozzle, forced air nozzle,
operator basket, etc.) and aircraft surfaces.
 As a safety mechanism, the proximity sensor is designed to prevent damage from occurring to
aircraft surfaces, normally while the equipment chassis is in a stationary position (not
maneuvering).
 Where equipped, the type of sensor used may vary by design and may activate either by
physical contact (e.g., a proximity switch with contact mechanism), or by non-physical activation
(e.g., infrared, radar, etc.).
Precipitation intensity. The intensity of precipitation is an indication of the amount of precipitation collected
per unit time interval.
 It is expressed as light, moderate, or heavy. Intensity is defined as the type of
precipitation occurring, based either on the rate of fall for rain and ice pellets or visibility for snow
and drizzle.
 The rate of fall criterion is based on time and does not accurately describe the intensity at a
particular time of observation.
Qualified staff: Trained staff who have passed theoretical and practical training tests and have been
qualified to perform this type of job; refer to AS6286.
Quality assurance: This is process-oriented, and it focuses on preventing quality issues. It is a proactive
approach. An audit is done to validate QA processes, and the quality procedures to be followed (e.g.,
“documented”)
Quality control: Is product-oriented and focused on identifying quality issues in manufactured products
and performance of service. It is a reactive approach. Inspections/checks/tests are done as part of the
QC procedure, to verify the quality of the available procedures and operations. (e.g., “implemented”).
Rain. Precipitation of liquid water particles, either in the form of drops of more than 0.5 mm in diameter
or smaller drops which, in contrast to drizzle, are widely separated.
Rime. A deposit of ice is produced by freezing supercooled fog or cloud droplets on objects at
temperatures below or slightly above freezing. It is composed of grains separated by air, sometimes
adorned with crystalline branches.
 Rime ice: Small, frozen, spherical water droplets, opaque/milky and granular in appearance,
which look similar to frost in a freezer; typically, rime ice has low adhesion to the surface and its
surrounding rime ice particles.

Refraction: The bending of light as it passes from one transparent substance into another. For solutions,
the refraction will vary on the concentration of the solute in the solvent.
 Using a calibration curve, it is possible to determine the concentration of the solute in the
solvent.
o For example, for aqueous glycol solutions, it is possible to determine the concentration
of the glycol in water by measuring refraction with a refractometer and comparing the
result to the calibration curve.
o Refraction can be expressed as a dimensionless number (index of refraction) or as a
scale of concentration, e.g., degrees Brix (°Brix), or freezing point (°C or °F). See also
refractometer.

 Refractive index: Unit of measurement of refraction expressed in the form of a dimensionless
number. See also refraction and refractometer.
Refractometer: An instrument to measure refraction. The result of measurement with a refractometer can
be expressed as a dimensionless number (index of refraction) or as a scale of concentration, e.g.,
degrees Brix (°Brix), or freezing point (°C or °F).
Residue/gel: A buildup of dried-, out thickened fluids typically found in aerodynamically quiet areas of the
aircraft.
Slush: Snow or ice that has been combined with water.
 Water-saturated snow which with a heel-and-toe slap-down motion against the ground will be
displaced with a splatter.
Snow: Precipitation of ice crystals, most of which are branched, star-shaped, or mixed with unbranched
crystals. At temperatures higher than -5 °C (23 °F), the crystals are generally agglomerated into
snowflakes.
Snow grains: Precipitation of very small white and opaque particles of ice that are fairly flat or elongated
with a diameter of less than 1 mm (0.04 inch); when snow grains hit hard ground, they do not bounce or
shatter.
Snow pellets: Precipitation of white, opaque particles of ice. The particles are round or sometimes
conical, their diameters range from approximately 2 to 5 mm (0.08 to 0.2 inch), they are brittle and
easily crushed, and they do bounce and may break upon contact with hard ground.
Storage tank: A vessel for holding fluid that can be fixed, or mobile; includes rolling tanks (ISO tanks),
totes, tank trucks, or drums.
Shear force. Shear force is a force applied laterally on an anti-icing fluid.
 When applied to a Type II, III, or IV fluid, the shear force will reduce the viscosity of the fluid;
when the shear force is no longer applied, the anti-icing fluid should recover its viscosity.
 For instance, shear forces are applied whenever the fluid is pumped, forced through an orifice, or when subjected to airflow. If excessive shear force is applied, the thickener system could be

permanently degraded and the fluid viscosity may fall outside the range set by the manufacturer
and tested for certification.
 Fluid degraded in this manner should not be used for operational purposes.
Snow. Precipitation of ice crystals mostly branched in the form of six-pointed stars.
 The crystals are isolated or agglomerated to form snowflakes.
 Dry snow. Snow from which a snowball cannot readily be made and which has a temperature
less than 0°C.
Tactile check: Process by which a person touches specific aircraft surfaces. Tactile checks, under certain
circumstances, maybe the only way of confirming the critical surfaces of an aircraft are not
contaminated. For some aircraft, tactile checks are mandatory as part of the deicing/anti-icing check
process to ensure the critical surfaces are free of frozen contaminants.
Thickened fluid. A fluid that contains polymeric thickeners. AMS1428 Type II, III, and IV fluids are
thickened fluids; AMS1424 Type I fluids are not thickened.
Wet snow. Snow which contains a great deal of liquid water.
Visible moisture. Fog, rain, snow, sleet, high humidity (condensation on surfaces), and ice crystals can all
produce visible moisture on aircraft, taxiways, and runways exposed to and contaminated by these
conditions.

Next Steps


For Training Related to Aircraft De–Icing & Anti-Icing please see www.sassofia.com,
and www.sofemaonline.com. For questions please email [email protected]

Last modified on