Ch 12 - Icing Flashcards

1
Q

Supercooled Water Droplets (SCWD)

A

Only occur below 0C
Where there is no nuclei to freeze onto
Size depends on temp; Large 0-20/25C, Small -20/25-40/45C, Colder than -40 = ice crystals

In CU you can find all of the above

0->-10C is where you will find the largest concentration of SCWD

Size of droplets determine the type of icing

Cirrus clouds = nil icing (ice crystals bounce of airframe)

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2
Q

Dangers of SCWD

A
Decreased thrust
Loss of control surfaces
Increased weight
Decreased lift
Increased drag
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3
Q

Hoar Frost

A

Aligns molecules - Knocks them about to align

Airframe icing but not with SCWD

Happens when parked at night, when there is water vapour in the atmosphere that comes into contact with airframe <0C - sublimation (vapour into ice)

Can also happen in the descent coming down from the cruise into lower levels with increased moisture vapour, cool airframe allows Vapour to sublimate onto airframe

Reduces lift by 10/15% and needs to be de-iced and anti-iced before flight

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4
Q

Rime Ice

A

Caused by SCWD and is the most common form of airframe icing

Forms at temps; -20/25C - -40/45C with small SCWD

From alto-type clouds (stratus as droplet size is smaller)

Will freeze at 1/80th for every 1C below 0 on impact with airframe

  • Bigger droplets freeze far more slowly
  • Small SCWD will freeze almost instantly

Traps air in it and gives it a Milky/White appearance and forms on the leading edges. Will be a problem if nothing is done after about 20 minutes

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5
Q

Clear Ice

A

Also known as glaze ice is caused by contact with Large SCWD in temperatures between 0C and -20/25C from Cumuliform clouds CU/CB

Slow process (large), latent head released as freezing takes place

The SCWD flow over the wing towards control surfaces and freeze as they do it which can leave the control surfaces inoperable

Air escapes before it freezes, hence the transparency

Far more dangerous than rime ice and in less than 20 minutes it will be trouble - difficult to remove

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6
Q

FZDZ

A

Caused by large SCWD falling as rain and being broken up into drizzle on the way down below 0C level. Usually from NS

Far more dangerous than clear ice as they freeze very quickly and can be very intense,

In only a few minutes it can cause complete failure

Avoid at all costs, climb above 0C level, descend to MSA with terrain and ATC clearance, or turn around and fly away

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7
Q

Mixed Ice

A

Caused by a combination of large and small water droplets, usually from NS and creates a combination of clear ice and rime ice on the airframe

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8
Q

Cloudy Ice / Packed Snow

A

If the airframe is wet, ice crystals then stick to the airframe and eventually build up and form a milky white cloudy colour

Also happens from snow flakes

Only happens on a wet airframe

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9
Q

Kinetic Heating

A

Movement generated heating (Friction)

Makes the severity worse as it slows down the freezing process, given the SCWD chance to reach your control surfaces

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10
Q

Orographic Uplift (Intensification)

A

Orographic uplift increases the amount of SCWD in the atmosphere

When it rains, it can evaporate, reduce OAT lowering the freezing level

All of this combines to increase the severity of the icing

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11
Q

Aerofoil Shape on Icing

A

Thicker wing; slower process and is not as severe

More severe with thinner wing

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12
Q

Severity and Reporting of Ice Accretion

A

Trace Icing - Rate of accumulation larger than the rate of sublimation, not a hazard

Light icing - Maybe a problem, use equipment if you have, not that hazardous

Moderate icing - Divert needed potentially, anti/de-icing needed

Severe - Immediate diversion necessary, anti-icing equipment is inadequate reduction/control of problem, obligated to report this

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13
Q

Engine Icing

A

Occurs in the carburettor

Dangerous because you wont expect it (clear and sunny conditions)

Most dangerous at engine idle on the descent/landing and sometimes in the cruise

Use carburettor heaters to reduce the chance of engine icing.

Wet conditions between +10C and -10C are the most dangerous so put on icing system

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14
Q

Turbine Engine Icing

A

Happens in the first stages of the engine intake during the convergence - decreased static pressure, which leads to a decrease in temperature which causes turbine engine icing

Ice on the core then gets sucked through

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15
Q

Ice Crystal Icing

A

Ice crystal icing can occur outside regions of expected

Ice crystals in the engine can lead to a complete engine failure

Most common in the subtropical regions 30N/S can be higher in summer reaching America and japan

  • Alt 20-35,000ft
  • Temp +10 to -10C

To avoid, find the gap and avoid whole bad pressure system by a wide margin, if not an option, divert.

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16
Q

De-Icing and Anti-Icing Order

A

1st - De-Ice

2nd - Anti-Ice for TO

But read operations manual