Icing Flashcards

1
Q

What are the two main types of icing?

A
  1. Airframe
  2. Engine
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2
Q

What conditions are required for ice to form?

A
  • Visible moisture
  • Temp +10 to – 40°C
  • Airframe must be <0°C
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3
Q

What is the freezing level?

A

The altitude at which the temperature is 0°C

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4
Q

Do snow an ice crystals in flight typically adhere to an aircraft?

A

No

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5
Q

Where is the worst icing found?

A
  • Near the Freezing Level
  • Heavily stratified clouds (St, Ns)
  • Cumulus or Cumulonimbus clouds with strong updraughts
  • In freezing rain beneath a NS
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6
Q

What are the types of airframe ice?

A
  • Clear
  • Rime
  • Mixed (Clear and Rime)
  • Frost
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7
Q

Elements of clear ice?

A
  • Most dangerous of all
  • Hard to see
  • Tenacious
  • Heavy
  • Smooth
  • Can flow back over wing
  • Caused by super-cooled water droplets freezing on contact.
  • Latent heat released as water freezes delays freezing and allows water to spread
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8
Q

Elements of Rime Ice

A
  • Supercooled tiny droplets freeze on a surface <0°C
  • Mixture of ice and air
  • Rough, opaque, crystalline, brittle
  • Can form between 0°C and -40°C
  • Most common -10°C to -20°C
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9
Q

Elements of mixed ice?

A
  • Due to droplets of varying sizes
  • Most common form of icing
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10
Q

Where is pure rime ice most likely to occur?

A

High AS or AC

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11
Q

Where is pure clear ice most likely to occur?

A

Freezing rain below NS

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12
Q

Elements of Frost (Hoar)

A
  • Occurs when moist air condenses on a freezing surface.
  • A white crystalline coating that easily brushes away.
  • Typical conditions:
    —– Clear night
    —– Calm wind
    —– High humidity
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13
Q

Dangers of frost?

A
  • Separation of Laminar flow over wing
  • Obscure vision
  • Freeze controls
  • Increase weight
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14
Q

CU are predominantly liquid water droplets until __________

A

-23C

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15
Q

At what temperatures is the highest risk of icing found in CU?

A

0°C to -15°C

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16
Q

Types of Ice/Temperature ranges within CU?

A

Clear - 0°C to -5°C

Clear and Rime - -5°C to -15°C

Moderate Rime - -15°C to -23°C

Light Rime -23°C to -40°C

Doubtful - lower than -40°C

17
Q

Stratiform clouds can contain water droplets to _________

A

-15C

18
Q

Rain, showers or drizzle will freeze on contact with an airframe _____________

A

below 0°C

19
Q

What is the relationship between risk of clear ice and droplet size?

A

Risk of clear ice increases with droplet size.

20
Q

Hazards to aircraft from ice on the airframe?

A
  • Weight and Centre of Gravity changes.
  • Adverse aerodynamic effects; wing and propeller:
  • Loss of lift
  • Increase in drag
  • Unbalancing of control surfaces/ propeller.
  • Loss of visibility.
  • Degradation of COM/NAV if antennae ice.
21
Q

Hazards to aircraft from ice in the intake?

A
  • Can disrupt engine sensors resulting in incorrect engine settings - B737 Potomac
  • Builds around turbine or jet intakes - Scandinavian Airlines Flight 751
  • Engine surging & failure
  • Disrupted running & reduced power
22
Q

Hazards to aircraft from ice in the pitot?

A
  • Block pitot and static ports - Air France
  • Causes instrument (ALT/ASI/VSI) Errors
  • Freeze angle of attack sensor (Stalling)
  • Blocks TAT sensor (Mach/TAS Air-data Computer)
  • Block engine EPR sensors
23
Q

What are the two different systems for removing ice?

A
  1. De-Icing
  2. Anti-Icing
24
Q

Elements of anti-ice?

A
  • Prevents ice from occurring.
  • Heating most common.
  • Heat is either
    —– Electric (pitot, propeller, windscreen)
    —– Bleed Air (leading edges, intake)
  • Anti-icing fluids (Ethylene glycol) used in very old aircraft.
  • Fluids still used for ground de-icing.
25
Q

Elements of De-Ice

A
  • Allows ice to form and then breaks it off.
  • Usually performed by pneumatic boots.
  • Used for:
    —– Leading edges
    —– Engine intake (Turboprops with inertial separators)
26
Q

Elements of Ground De-Ice

A
  • In very cold climates aircraft need ice removed from areas other than leading edges before take-off.
  • De-icing fluids and heat are used.
  • Some airports have a de-ice bay near the threshold.
27
Q

Elements of Induction Icing

A
  • Applies only to piston-engine aircraft.
  • Carburetted engines more susceptible than fuel-injected.
  • Can occur at temps >35°C in high humidity.
  • Can result in:
    —– Rough running
    —– Engine failure
28
Q

Elements of Carburretor Ice

A
  • Venturi effect lowers temp
  • Fuel evaporation lowers temp
  • Ice restricts flow.
  • Anti/De-ice allows hot air in but reduces efficiency.
29
Q

True or False. Hoar Frost can develop when an aircraft passes quickly from sub-zero dry air to warm moist air.

A

True