Ice & Rain Flashcards

(43 cards)

1
Q

What ice protection does pneumatic air provide?

A
  • wing leading edges
  • horizontal stabiliser leading edges
  • engine air intakes
  • gas paths
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2
Q

Where are the chordwise boots used?

A

Leading edges and gas paths

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3
Q

Where are the annular boots used?

A

Engine intakes

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4
Q

What happens when the boot is deflated?

A

It is held to the structure by Venturi effect

The Venturi effect is created by the bleed air

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5
Q

What controls the inflation of the boots?

A

The associated distribution valve

There are seven distribution valves

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6
Q

What uses electrical power for deicing?

A
  • prop blades
  • windshields
  • probes
  • static ports
  • flight control horns
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7
Q

Where is the ice detector located?

A

Rosemont Ice detector probe - Under the left wing

Provides crew with visual and aural alert when ice is accreting on the probe

Powered by AC Wild bus 2

As ice accumulate the vibration freq changes

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8
Q

Where is the Ice Evidence Probe located?

A

Located outside and below the Captains left side window

Visible to both pilots and provides a visual indication of ice accretion

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9
Q

When will the amber icing light illuminate?

A

When 0.5 mm of ice has accumulated on the probe

Probe will initiate a heat cycle to remove accretion and start again

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10
Q

What does it mean if the ICING light extinguishes on its own?

A

Indicates that ice is no longer accumulating

Does not indicate that airframe is clear of residual ice

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11
Q

What is the delivery pressure of the de-ice valves?

A

20.3 psi

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12
Q

What distributes air to the wing and horizontal stabiliser distribution valves?

A

The common manifold

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13
Q

What controls the boots?

A

The associated MFC

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14
Q

How long is the boots inflation cycle?

A

If SAT is greater than -20 cycle is set at 60 secs with 20 sec dwell

If SAT is less than -20 cycle is set at 180 secs with 140 sec dwell

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15
Q

What happens if you press in the DE-ICE MODE SEL pb?

A

SLOW caption is the pb is illuminated and cycle is forced to 180 secs

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16
Q

What is electrically anti-iced?

A
  • props
  • flight control horns
  • probes
  • windshields
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17
Q

What anti-ices the flight control horns?

A

AC Wild electrical power

115 VAC

Horn anti-icing is inhibited on the ground

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18
Q

Why does the ICING AOA illuminate green when anti-icing is on?

A

The AOA threshold is lowered by selection of anti-ice

Serves as a reminder to the crew to set speed bugs and observe minimum icing speeds

Light can only be extinguished manually by pressing the pb after both horn anti-icing buttons have been selected OFF

19
Q

What powers the propeller heat?

20
Q

When is the low power propeller cycle used?

A

Between 0 and 10 degrees celcius

Heating time is 10 seconds

Normal cycle when the pb is in the out position

21
Q

What is the high power propeller cycle?

A

Heating time is 20 secs and there is no pause between cycles

22
Q

Why are the two front windshields heated?

A

To prevent anti-icing and defogging

The side windows are heated to prevent fogging only

23
Q

What powers the windshield heat?

A

The associated AC Wild bus

24
Q

What does the temperature controller maintain the windshields at?

A

Outside ply maintained at 2 degrees

Maintains inner ply above 21 degrees to prevent fogging

25
What heats the side windows?
Heated by the 28 VDC bus Temp regulated to maintain the inner temp over 20 degrees
26
Why is the aft portion of the side windows not heated?
The heating element is designed to warm the whole plane Ice build up aft of the heated portion is usually an indication of severe icing and/or freezing rain
27
What is the probe heat source?
AC power used to heat: - pitot probes - alpha probes - TAT probe
28
How is static port heat controlled?
Static port heat controlled by the associated probe heat pb
29
What happens to TAT probe heat on the ground?
Automatically inhibited and the condition of the probe is not monitored
30
What is the windshield wiper speed limit?
160 kt
31
When does the ICING light illuminate?
When ice accretion is detected It will be steady if both horn anti-icing and airframe de-icing are selected on It will flash if either is off
32
What is the icing test?
Test button pressed and held for 3 seconds During the test the ICING amber light flashes and a single chime will sound FAULT will illuminate if a fault is detected during the test
33
When will the blue DEICING light flash?
If the de-icing system is still on 5 minutes after the last detection of ice accretion
34
When will the FAULT light on the airframe air bleed pb light?
If the pressure downstream of the de-ice valves is below 14 psi for more than 10 secs or when air temp of the bleed air exceeds 230 degrees
35
When will the airframe pb FAULT light illuminate?
When a distribution valve is commanded closed but bleed air pressure still exists downstream or if a valve is commanded open but no pressure is sensed
36
When does the MODE SEL AUTO FAULT light illuminate?
- failure of the 1B or 2B MFC - ADC failure
37
What is the de-icing emergency mode?
- timing cycle of 60 secs - OVRD caption illuminates white - all de-icing lights extinguish Used when a fault light illuminates
38
When will the FAULT light in the DEICING OVERRIDE pb illuminate?
If there is a failure in both MFC modules
39
What is level 1 anti-icing?
Must be selected on before each flight Probe and forward windshield anti-ice are turned on
40
What is anti-icing level 1.5?
Take off in ground icing but flight into non-icing conditions Continuous relight selected Prop anti-ice selected on
41
What is anti-icing level 2?
Operating or taking off in icing conditions - prop anti-ice - horn anti-ice - side window anti-ice - engine de-ice Continuous relight selected
42
What is anti-ice level 3?
Flight where ice is accreting - prop heat - horns and side window anti-ice - engine de-icing - airframe de-icing Continuous relight selected
43
With the MOD SEL pb in AUTO, what system determines the de-icing cycle?
The MFCs and the ADCs