
Ice and Rain Control System
Authored by Jonathan Fayt
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Professional Development

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27 questions
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1.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Which of the following is the best means to use when removing wet snow from an aircraft?
Hot air
A brush or a squeegee
Warm water
Chemical deicing fluid
Answer explanation
A brush or a squeegee is the best means to remove wet snow from an aircraft as it effectively clears the snow without damaging the surface, unlike hot air or warm water which may not be as efficient.
2.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What icing condition may occur when there is no visible moisture present?
Injector ice
Inlet ice
Carburetor ice
Rime ice
Answer explanation
Carburetor ice can form even when no visible moisture is present, as it occurs due to the cooling effect of fuel vaporization in the carburetor. This can lead to engine performance issues, making it a critical condition to monitor.
3.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Which of the following are found in a laminated integral electrically heated windshield system?
Autotransformer, heat control relay, heat control toggle switch, 115V DC power supply, and indicating light
Heat control relay, heat control toggle switch, 24V DC power supply, and indicating light
Autotransformer, heat control relay, heat control toggle switch, and indicating light
Thermostat, 28V DC bus, and heating grid
Answer explanation
The correct choice includes an autotransformer, heat control relay, heat control toggle switch, and indicating light, which are essential components in a laminated integral electrically heated windshield system.
4.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Some aircraft are protected against airframe icing by heating the leading edges of the airfoils and intake ducts. When is this type of anti-ice system usually operated during flight?
Continuously while the aircraft is in flight
In symmetric cycles during icing conditions to remove ice as it accumulates
Whenever icing conditions are first encountered or expected to occur
Only after ice has built up 1/2 inch
Answer explanation
The anti-ice system is activated whenever icing conditions are first encountered or expected to occur to prevent ice accumulation, ensuring safe flight operations.
5.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Which of the following indications occur during a normal operational check of a pneumatic deicer system?
Relatively steady readings on the pressure gauge and fluctuating readings on the vacuum gauge
Fluctuating readings on the pressure gauge and relatively steady readings on the vacuum gauge
Pressure and vacuum gauges will fluctuate as the deicer boots inflate and deflate
Constant pressure and vacuum readings
Answer explanation
During a normal operational check of a pneumatic deicer system, the pressure gauge fluctuates as the deicer boots inflate and deflate, while the vacuum gauge remains relatively steady, indicating proper system function.
6.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Where are the heating elements located on most aircraft with electrically heated windshields?
Laminated in the glass
Attached to the glass
Inside the windshield frame
On the outside surface
Answer explanation
The heating elements in most aircraft with electrically heated windshields are laminated in the glass. This integration allows for efficient heating without obstructing visibility, making it the correct choice.
7.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Two possible sources of heat for the operation of a wing thermal anti-icing system are
First stage of the aircycle turbine and turbo compressor
Compressor bleed air and aircraft electrical system
Combustion heater and exhaust gases
Ram air and engine oil
Answer explanation
The correct choice is 'Compressor bleed air and aircraft electrical system' as these sources provide the necessary heat for the wing thermal anti-icing system, ensuring effective operation in cold conditions.
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