De-icing/Anti-icing Review

Slides:



Advertisements
Similar presentations
What creates different climates in Canada and what impact does climate have on human activity? The Climates of Canada.
Advertisements

Earth’s Weather Patterns
A thunderstorm is one or several cumulonimbus clouds accompanied by lightning and thunder. Three Ingredients: – Lifting force – Unstable Air – Moist air.
Lecture 3: Take-off Performance
737 PNEUMATICS MENU PRINCIPAL.
Chilled Water, Hot Water, Heat Pump and Glycol Loops
Earth Systems and Patterns: SC.5.E.7.3
Metamorphism Due To Direct Weather Effects Learning Outcomes Understand the effects of direct weather on the snowpack. Understand melt-freeze and its effect.
AIR NAVIGATION Part 5 Weather.
Regional Gliding School Cloud Precipitation Fog Haze Smoke Blowing Snow Blowing Dust Blowing Sand.
UNDERSTANDING WEATHER. The Water cycle The amount of water vapor in the air is called humidity. As water evaporates and becomes air vapor, the humidity.
#4095. How much colder than standard temperature is the actual temperature at 9,000 feet, as indicated in the excerpt from the Winds and Temperature Aloft.
Aviation Weather Air Temperature and Pressure Affecting Aircraft.
Selection of measuring instruments
Choose a category. You will be given the answer. You must give the correct question. Click to begin.
1 FALL & WINTER CLIMO AND HAZARDS BRIEFING! Sacramento, CA DET 32 OSA FY08.
Weather Measuring Change. Lesson Objectives In this lesson you will learn:  identify the function of the following weather instruments used in a weather.
Boiling Point Lab Hari- Modifications 8th grade science Hari- Modifications 8th grade science.
A4A Meteorology Work Group Rick Curtis 2/26/15. ◦ Affects of in-route icing can greatly vary in degree among carriers – due to equipment type, route structure.
What creates different climates in Canada and what impact does climate have on human activity? The Climates of Canada.
Paint It Black 9-5 Project 1. Purpose The purpose of this experiment is to investigate the relationship between heat conservation and color. The questions.
Placing Quality Concrete
Aircraft Ice Protection Systems
Winter Operations Re-current training. Common standards, regulation and recommendations Effects of frost, ice, snow, slush on airplane performance Meteorological.
Earth Systems and Patterns: SC.5.E.7.1
LWE and Checktime Demo Scott Landolt & Steve Cristanelli - NCAR October 27, 2009.
© 2011 Pearson Education, Inc. All Rights Reserved Automotive Technology, Fifth Edition James Halderman COOLANT 20.
BASIC DATA SPHERE OF BUSINESS organosilicon compounds silicone resins silicone corrosion inhibitor silicone additives profesional cleaning agents De-/-Anti-Icer.
Earth Science: 15.1 Ocean Water and Life
Water in the Atmosphere I. Atmospheric Moisture Water exists on Earth in 3 forms:  Liquid  Solid (ice)  Gas.
Heat Transfer from Ice Accretion Steven Mart Baylor University Scholar’s Day: Aeronautical & Processing Applications Rogers Engineering Building February.
The Atmosphere: An Introduction to Meteorology, 12th
AIR NAVIGATION Part 5 Weather. LEARNING OUTCOMES On completion of this lesson, you should: - Know the hazards that weather presents to aviation.
LWE – Research to Operations Dr. Roy Rasmussen (NCAR) Steve Howe (Vaisala)
On the use of Liquid Water Equivalent (LWE) for estimating snowfall intensity and freezing drizzle intensity versus the use of visibility Roy Rasmussen.
AVIATION HISTORY Lecture 7: Flight Environments. Introduction  Earth is a the bottom of an ocean of air.  Dynamic layers of air interact with the Earth's.
Unit 1 Test - Tuesday, October 7th  Safety  Weather and Climate  Measurement  Density Let’s Review Together!
Mr. Nye’s Jeopardy RULES 1.There will be round robin play (start with team 1 and go to team 4). 2.The team who answers correctly wins the point value.
Meteo 3: Chapter 16 Winter Weather Read pages , ,
Introduction The environmental factors such as light, temperature and nutrients interact with each other in the marine environment and play a major role.
CHAPTER 3 TEMPERATURE AND HUMIDITY EXTREMES CHAPTER 3 TEMPERATURE AND HUMIDITY EXTREMES.
Chapter 7: Climate Weather. Precipitation  Precipitation occurs when a cold air mass meets a warm air mass.  The cold air, being more dense, forces.
AIRCRAFT GROUND DEICING/ANTI-ICING
Presented to: FPAW By: Mark Gunzelman, AvMet Applications Date: August 8, 2012 Federal Aviation Administration Improving Precipitation Measurement in ASOS.
Federal Aviation Administration Winter Operations Downloaded from 1.
The Effects of Weather on Aircraft Part 1 of 2
Winter Weather Homeroom Read. Warm Up: Define WINTER WEATHER ADVISORIES WINTER STORM WATCH WINTER STORM WARNING FROST/FREEZE WARNING.
Global Wind Currents. What do wind patterns have to do with oceans?  CURRENTS.
Meteorology 5.08 Extreme Weather References:
Surface Condensation Water vapor condensing on large surfaces is called dew. Dew Point is the temperature that saturation occurs and condensation begins.
Winter Weather Issues Oct. 19, 2006 Presentation at Friends and Partners in Aviation Weather meeting Roy Rasmussen, NCAR AWRP Winter Weather PDT lead.
DQ#4 What 4 things can occur when water vapor condenses? I do not mean any form of precipitation.
Performance Charts.
Salinity and Density Differences VERTICAL STRUCTURE, THERMOHALINE CIRCULATION & WATER MASSES.
. METEOROLOGICAL HAZARDS IN AVIATION Cpt. Ing. Naděžda Bartošová Ph.D.
Chapter Describing Weather Pages
Bell work Observe two glasses of water. One is filled with ice water, and one is filled with warm water. Why do water droplets form on the outside of the.
FOG. Fog is a cloud (usually stratus) that is in contact with the ground. –Relatively stable air ie. Shallow lapse rate needed –Temperature to dew point.
Liquid Water Equivalent Operational Demonstration.
PRECIPITATION "RAIN DROPS KEEP FALLING ON MY HEAD" B.J. THOMPSON (1969)
WEATHER -What is weather? -Why do we track it? -How does it affect us in Oakland?
20 COOLANT COOLANT.
On the Determination of Snow and Freezing Drizzle Intensity
Measuring Snowfall Intensity using LWE (Liquid Water Equivalent) -Randy Baker representing A4A Meteorology Work Group 08 AUG 2012.
Future Applications AviCast, CheckTime, Mobile Sensors
Update on the use of Liquid Equivalent for determination of snowfall and drizzle rates of light, moderate, and heavy Oct. 13, 2003 Presentation at Friends.
adidas Football Techfit Uniforms Care Instructions and Tips
Visibility & Ice Accretion
What creates different climates in Canada and what impact does climate have on human activity? The Climates of Canada.
/700/800/900 AIRCRAFT MAINTENANCE MANUAL COLD WEATHER MAINTENANCE – SERVICING TASK
Presentation transcript:

De-icing/Anti-icing Review Winter Operations De-icing/Anti-icing Review

Overview Clean Aircraft Fluids Methods Holdover tables To de-ice, anti-ice or both Fluids Methods Contamination Removal (De-ice) Contamination Prevention (Anti-ice) Holdover tables Cold weather operations require a vigilant eye to ensure a clean aircraft. When necessary, de-icing and anti-icing procedures must be properly executed.

Achieving a Clean Aircraft Remove Protect Applying anti-ice fluid to the aircraft forms a protective shield against contamination for varying amounts of time. The “clean aircraft concept” requires the critical surfaces be clear of all contaminates such as ice and frost prior to takeoff. That means you need to remove any accumulated contaminates and also ensure that they will not accumulate prior to takeoff.

Fluid Types Type I Type II Type III Type IV The four fluid types can be identified by color Type I Type II Type III Type IV Deicing formulas are categorized from Type I through Type IV, depending on fluid composition and application procedure.

Type I Fluids Primarily a De-icer Un-thickened/Low viscosity Usually 50% water and either ethylene glycol or propylene glycol Can penetrate cracks/crevices to dissolve contaminates Heated before spraying (usually 600C/1400F) Limited anti-ice protection Low-viscosity Type I deicing fluids flow quickly from aircraft surfaces, making them ideal for light applications and composite surfaces.

Type II III & IV Fluids Primarily Anti-icers Most effective when applied unheated and undiluted to a clean airplane surface While the same fluids used for deicing are also used for anti-icing, SAE types II, III, IV fluids are more typically used for anti-icing because they are thickened to stay on the airplane and thus provide longer HOT protection. Type II and Type IV fluids are often used during heavy snowfall. Type III, a compromise between Types I deicing and Type II anti-icing fluids, is used for smaller, metal-skinned aircraft.

Viscosity Viscosity can be thought of as the thickness of the fluid. Honey has a much higher viscosity than water for example. Thickening agents can be added to anti-icing fluids to make them more viscous. The more the viscosity of the fluid, the longer the holdover time.

Viscosity and Holdover Time Increasing holdover time TYPE VISCOSITY MIN TAKEOFF ROTATION SPEED I Low None III Medium 60 II High 100-110 IV The anti-icing fluid is only useful on the ground to prevent ice buildup. During the takeoff roll, it should bleed off the aircraft surfaces to allow clean airfoils. The more viscous the fluid, the higher the necessary rotation speed to bleed off the fluid.

De-icing Methods Fluids Mechanical or manual Water (Heated or Cold) Heated mixture of water and Type I fluids Heated mixture of water and Type II or Type IV fluids Mechanical or manual Brush or Broom Put aircraft in a heated hangar Dry the aircraft surfaces after the ice melts Infrared Heat Gas Heaters in a “drive-under” structure Does not heat the air, but penetrates the frost/ice to melt it JFK infrared station De-icing removes accumulated frost, ice, or snow from an airplane, typically through the application of hot water or a hot mixture of water and de-icing fluid. Although there are other approved methods for de-icing, such as infrared heat or hot air, the primary method is the use of fluids.

Anti-icing Methods Mixtures of water and Type I fluids Type II or Type IV Fluids applied as unheated concentrate Mixture of water and Type II or Type IV Fluids Once the critical surfaces are clear, it is necessary to anti-ice the aircraft if icing conditions still can cause surface contamination prior to takeoff. Anti-icing prevents ice from refreezing or reforming on the critical surfaces for a specified amount of time.

Fluid De-icing/Anti-icing Methods One Step Method Two Step Method One application to both de-ice & anti-ice Typically a heated mixture of thickened fluid and water is applied The heated fluid is used to de-ice the aircraft surfaces Provides limited anti-ice capability Step one: de-ice This process involves deicing with heated Type I fluid, a heated mixture of Type i fluid and water, or a heated mixture of water and thickened (Type II, III, or IV) fluid Step two: anti-ice application of thickened fluid for anti-icing protection. Provides maximum anti-icing capability Depending on the situation, fluid application is done in one or two steps. When anti-icing capability is needed, a two step process is always recommended. Let’s have a look at a few reasons.

The Case for Two Step Method The repeated application of Type II and IV fluids, without the subsequent application of type i fluid or hot water may cause a residue to collect in aerodynamically quiet areas. This residue may rehydrate and freeze under certain temperature, high humidity and/or rain conditions. This residue may block or impede critical flight control systems and may require removal Landing on runways where deicing fluid has been applied can leave a residual on the aircraft surfaces. You need to perform the two step process to remove this residual fluid as a means of protection for your next flight You need maximum holdover time A one step method is quicker and often sufficient. However, a two step method is necessary at times for maximum holdover time and to ensure that first any fluid residue is removed before anti-icing again.

One Step Considerations You need sufficient fluid temperature and flow rate to flush the ice and snow from the airplane surfaces More water increases the flow rate for better removal but makes the fluid less viscous, lowering holdover time If there is only snow on the airplane and the temperature is 340 F or higher, stable and on the increase, then water may be used to remove the snow Note: FAA POI’s strongly encourage use of type II or type IV anti-icing fluid, during light freezing rain or freezing drizzle. Use a heated mixture of water and either type I, II, or IV fluids when performing the one step method. Consider the weather conditions, holdover protection time necessary and condition of the airplane to determine the quantity of water necessary.

Guidelines The winter operations manual contains guidelines for fluid and mixture selections. Note mixing of type II or type IV fluids from the same or different manufacturers is not allowed.

Holdover Table Overview Current Weather Conditions Outside temperature Type and intensity of precipitation Fluid Type of fluid Dilution of fluid Time started To use the holdover time tables you will need to know several aspects of the current weather condition, as well as the fluid application. Be sure and read the cautions at the bottom of the holdover time table.

767 Composite Surfaces The holdover tables have charts for predominantly aluminum and predominately composite aircraft surfaces. Even though there are composite surfaces, the 767 obviously has predominately aluminum surfaces.

Establishing HOT Range Snowfall rate The relationship between visibility and snowfall intensity is analyzed and contained in the Snowfall Intensity Chart Precipitation rates for other than snow Due to the wide range of possible precipitation rates, the only acceptable decision criteria time for all other precipitation is the shortest time within the applicable HOT cell. The shortest time in the HOT cell correspond to the highest precipitation rate With a one step process, the holdover time begins at the start of the operation. With a two step process, the holdover time begins at the start of the second step Holdover time guidelines in the tables give an indication as the time frame of protection that could reasonable be expected under conditions of precipitation. However, due to the many variable that can influence holdover, these times should not be considered as minimums or maximums as the actual time of protection may be extended or reduced, depending upon the particular condition existing at the time.

Snowfall Intensity vs. Visibility Chart The snowfall intensity vs. visibility chart can give you a snowfall intensity, if you don’t know it. It can also refine the snowfall intensity reported in the METAR to give you a more accurate holdover time. In fact, the holdover tables now require you to use it. Let’s look at an example.

METAR Snowfall Intensity You are planning on de-icing using Cryotech Polar Guard II type II fluid diluted at 75/25 at Churchill Airport. These are your current conditions. The METAR automatically displays light snow if it is snowing and the prevailing visibility is greater than ½ statue mile. Let’s use the chart to get a more accurate snowfall rate.

Determine Snowfall Intensity Notice: Anytime the visibility is greater than 2 ½ miles, the intensity is considered very light It is daytime, visibility 10 miles with a temperature of 00 Celsius. That gives us very light snowfall instead of the light snowfall reported in the METAR. Note, we didn’t even need the precipitation from the METAR to get this. So if it is snowing, you only need the visibility and temperature to get the intensity.

Holdover Tables Be sure and select the correct holdover table according to the fluid used.

Holdover Time Calculation If we are using the Cryotech Polar Guard II type II fluid, then our holdover time range is 2:25 to 2:55.

Holdover Time Use Less than 2:25 no contamination check required Between 2:25 and 2:55 consider contamination check More than 2:55 contamination check required re-apply as necessary Recall that the holdover time started at the BEGINNING of the final application, not when it was finished If the existing weather conditions prevail for the next three hours, then we do not need an additional check if we takeoff before 2 hours twenty five minutes. Takeoff’s between 2 hours 25 minutes and 2 hours 55 minutes require a check. If we wait longer than that, we need to get another treatment.

Holdover Time Factors The heavier the precipitation, the shorter the HOT. High winds or jet blast that cause the fluid to flow off, decreasing the protection afforded by the fluid layer. Wet snow, which causes fluids to dilute and fail more quickly than dry snow. The use of incorrect equipment to apply fluids. An airplane skin temperature lower than outside air temperature. Direct sunlight followed by precipitation. Heavy precipitation rates or high moisture content, high wind velocity or jet blast may reduce holdover time below the lowest time stated in the range and holdover times may also be reduced when aircraft skin temperature is lower than OAT.

Different Table Type Note if we would have used this fluid, we do not have the light and moderate snow categories. In this case, the lower number is the holdover time for moderate snow and the upper number for light snow. So our holdover time with no check is 1 hour 10 minutes, after which we need a check. Heavy snow always requires a contamination check.

Generic Holdover Table SAE Type is the generic table you use if you can’t find a specific table. It is the most conservative table for all brands.

METAR Snowfall Intensity Finally let’s look at another example where the snow is reported as light, but the visibility is different. Here in St. Louis we have ½ sm visibility with light snow reported.

Determine Snowfall Intensity Notice: Anytime the visibility is less than ¾ miles, the snowfall intensity is Moderate or Heavy With the same light reported snowfall as the previous example, our snowfall intensity is now Heavy. So we will need contamination check.

De-icing Review Questions It’s time for a few questions.

Question Select the best statement regarding viscosity and holdover time: Type I fluid is the most viscous, with the least holdover time Type II and IV are the most viscous, giving the longest holdover time Type III is more viscous than type II and has a longer holdover time Type I fluid is the most viscous giving it the longest holdover time Please select the best choice.

Question The visibility is ¼ mile, select the best statement(s) ? You need a Pre-takeoff check and a Contamination check You need more information to determine holdover There is no holdover time Statements a & c are correct Please select the best choice.

Question The METAR reports visibility at ¾ mile. Which chart would you use to determine the snowfall rate? Select the correct answer.

Question Which of these factors decreases the holdover time? Dry snow, which causes fluids to dilute and fail more quickly than wet snow An airplane skin higher than outside air temperature Direct sunlight followed by precipitation No wind Please select the best choice.

Question Select the correct statement: It is not necessary to remove contaminates from control surfaces before anti-icing. For maximum effectiveness and minimum consumption, the de-icing solution should be only lukewarm. Apply only enough fluid to remove the ice and snow or to leave a light coating of fluid on the aircraft. The greater the precipitation the longer the holdover time.

Module Complete You have come to the end of this module.