11.12 Ice And Rain Protection Flashcards

1
Q

What 2 systems are there for rain protection?

A
  • Windshield Wiper

- Rain repellent system

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2
Q

what negative effects does ice have on an aircraft? [3]

A
  • increase in drag
  • decrease in lift
  • weight increase
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3
Q

what range of temperature can water droplets form clear ice on the surface of the aircraft?

A

0 degrees to -10 degrees

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4
Q

what ice is formed when the temperature drops below -10 degrees?

A

Rime-ice

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5
Q

whats is a thermal wing anti ice system?

A

where on the leading egde, heat is used to melt any ice formed

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6
Q

what 2 negative effects can ice have on engine inlets?

A
  • disturbs air flow = a reduction in engine performance and compressor stall
  • damage to fan blades and inlet vanes
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7
Q

what do engine inlets have to prevent ice build up?

A

thermal anti ice system

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8
Q

what is aerofoil de-icing?

A

using rubber boots on leading edges of wings and stabilisers rather than warm air from pnuematics

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9
Q

how do the rubber boots work? (aerofoil de-icing)

A

They inflate for a short time by pressurised air, cracking the ice which is blown away by the airflow

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10
Q

what type of ice detection is a probe on the front of the aircraft that collects ice where its visible to the pilots?

A

Optical Ice detector

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11
Q

what types of ice detection systems are there? [3]

A
  • Optical ice detector
  • rotary ice detector
  • electronic ice detector
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12
Q

how do electronic ice detectors work?

A

Tips of the detector vibrate with a frequency that reduces with ice formation

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13
Q

where are thermal anti-ice systems are installed on the aircraft? [2]

A
  • the wing

- engine

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14
Q

what is the name of the vales that connect the wing anti ice ducts to the pnuematics?

A

wing anti ice valve

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15
Q

where does the warm air come from to anti ice the engine?

A

directly from the engine

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16
Q

what valve connects the engine to the pneumatics to provide anti ice?

A

engine anti ice valve

17
Q

what is found in the wing or engine anti ice ducts to spray them with hot air?

A

small holes

18
Q

what duct is equipped to the leading edge when slats are installed for anti ice?

A

telescopic duct

19
Q

what main valves is used to regulate the air coming from the pnuematics to the anti systems?

A

bleed valve

20
Q

how many switches do the wing anti ice systems have? and why?

A
  • 1

- they must always operate symmetrically as one may have a reduction in lift if not switched on.

21
Q

how many switches are there for the engine anti ice system?

A

1 for each engine

22
Q

when are anti ice systems normally operative?

A

during flight

23
Q

when can you switch on the anti ice systems on the ground?

A

to check operation of the valves before flight

24
Q

when are engine anti ice systems always available?

A

when there is bleed air from the engine

25
Q

what types of valves can be found in the anti-ice system? [2]

A
  • electrical motor operated valves

- solenoid controlled pressure operated valves

26
Q

when would the solenoid controlled valve close by a spring?

A

when there is no pressure

27
Q

how does a solenoid controlled valve operate? [2]

A
  • de-energised solenoid = pressure from airflow fills the lower chamber of the valve cylinder, pushing the piston up, moving air in the top part of the cylinder to ambient. opens valve
  • energised solenoid = brings high pressure to the upper part of the cylinder to equalise the pressure on both sides, but closes under spring pressure
28
Q

what does the engine anti ice solenoid controlled valve do under a fail safe operation?

A

automatically open with no electrical power

29
Q

what monitors valve position?

A

limit switches

30
Q

when will a fault light illumincate on wing anti ice pushbutton?

A

when the pressure doesnt reach 14 psi

31
Q

when does the aircraft only use 50% of AC power?

A

when on the ground