Auxiliary Midterms 2 Flashcards

1
Q

effects of icing

A

lift decreases, thrust decreases, weight increases, drag increases, stalling speed increases

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2
Q

clouds have no ice but have

A

supercooled water droplets

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3
Q

when droplets hit the aircraft, they change from ____ to ____

A

liquid water, solid ice

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4
Q

negative effect on the aerodynamics and a higher weight

A

engine [ice formation on engine]

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5
Q

clouds have no ice but have supercooled water droplets. when this droplets hit the aircraft they change from liquid water to solid ice

A

wings [ice formation on wings]

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6
Q

has milky white appearance and generally follows the surface closely

A

rime

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7
Q

sometimes clear and smooth but usually contain some air pockets that result in a lumpy translucent appearance, denser, harder, and more difficult to break.

A

clear/glaze

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8
Q

brittle and frost-like

A

rime

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9
Q

hard and glossy

A

clear

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10
Q

hard rough conglomerate

A

mixed

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11
Q

removal of the ice after it has performed

A

de-icing

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12
Q

employed in certain types of piston-engine and turbo-prop aircraft

A

pneumatic de-icing system (boots)

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13
Q

pneumatic de-icing system (boots) consists of:

A

air supply; air distribution system; pneumatic de-icer boots; controls and indications

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14
Q

when pneumatic de-icing system is switched on?

A

pressure is admitted to the pneumatic boot (cyclically) sections to inflate the tubes. Ice breaks up and is carried away by the air flow

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15
Q

air is dumped to atmosphere via?

A

valves

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16
Q

pneumatic de-icing system operates on a?

A

timed cycle with each section for about 20 seconds and then off for about 80 seconds

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17
Q

tubes are then fully deflated by a ___

A

vacuum supply

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18
Q

when pneumatic de-icing system is off?

A

vacuum is continually supplied and used to hold boots flat agains the wing

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19
Q

susceptible to damage by?

A

refueling and bright sunlight

20
Q

do not operate until? (pneumatic de-icing system)

A

after ice has formed

21
Q

used primarily on small turbo-jets (business jet types)

A

fluid de-icing system (weeping wing)

22
Q

what is drawn from a storage tank by electrically driven pump and fed through micro-filters to a number of porous metal distributor panels

A

de-icing fluid (glygol)

23
Q

De-icing fluid (glycol) is drawn from a storage tank by?

A

electrically driven pump and fed through micro-filters to a number of porous metal distributor panels

24
Q

formed to profile of the wing to which they are fitted

25
as fluid escapes?
it breaks the adhesion between the ice and the wing and the airflow carries it away
26
as fluid escapes it breaks the adhesion between __ and the ___ and the ____ carries it away
ice and the wing
27
As fluid escapes, it breaks the adhesion between the ice and the wing and?
airflow carries it away
28
ensures an even distribution through all wing areas
head compensating valve
29
amount of fluid that can be carries
limiting factor
30
operate only after? (fluid de-icing system)
after ice has formed
31
If another plane is waiting to come into that gate, deicing a departing plane will?
only slow down that process
32
deicing fluids deplete?
the oxygen from water
33
deicing fluids deplete the oxygen from water, and airports don't want the fluids going into the?
storm water drains
34
where do the fluids drain into a special tank or reservoir?
deice pad
35
also known as Glycol
Heated orange fluid called Type 1
36
is sprayed evenly over the affected areas, melting whatever was sticking to it
Heated orange fluid called Type 1
37
whatever was sticking to it. Type I is mixed with? and what ratio?
water, usually at a ratio from 40% to 60%
38
Heated orange fluid called Type 1 smells a lot like?
maple syrup
39
The mixture can be ___ or ____ based on the outside air temperature
diluted or thickened
40
are designed to remain on the wings of an aircraft during ground operations, thereby providing anti-icing protection
Type II fluids
41
Type II fluids should be used on aircraft with rotation speeds (Vr) above?
above 100knots unless otherwise specified by the aircraft manufacturer.
42
are designed for aircraft that have a shorter time to rotation
Type III fluids
43
Type III fluids should make it acceptable for some aircraft that have rotation speeds (Vr) of?
less than 100knots unless otherwise specified by the aircraft manufacturer.
44
green, thicker, not heated, and is used to protect the critical surfaces from accumulation of frozen precipitation
Type IV
45
Type IV fluids is used to protect the?
critical surfaces from accumulation of frozen precipitation while the plane waits to take off
46
This fluid slides off the wings as the plane takes off
Type IV