Foul Weather / AC and PX Systems Flashcards

1
Q

Two subsystems

A

Air scoop

Compressor inlet assembly

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2
Q

Prop ice control time

A

160 seconds, 20 seconds each of the cuffs, skirts and islands for 4 engines
76-100 amps in flight, 74-100 on the ground

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3
Q

Diffuser anti ice percent drop

A

9% and 5% increase in FF

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4
Q

Timer motor for emp deice

A

8 seconds per strip with 16 second dead band = total 176 secs

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5
Q

Engine and wing use what kind of heat?

Prop and emp?

A

Air only in normal RPM
Electric low or normal RPM

Memory aid: engines run both on the ground and in the air. Wings only work in the air (norm)

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6
Q

Ice detector

  • when to use
  • power source
  • test perameters
A
  • whenever MEAC is powered
  • MEAC: probe heater, MEDC: icing light
  • N/A
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7
Q

Pitot heat

  • when to use
  • power source
  • test perameters
A

Before start to secure checklist
FEAC: pilot, MEAC(28c fwd lighting): copilot, MEDC: caution lights
N/A

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8
Q

AOA heat

  • when to use
  • power source
  • test perameters
A

Before start to secure checklist
MEDC
N/A

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9
Q

Engine

  • when to use
  • power source
  • test perameters
A

Prior to entering areas where structural icing is likely
MEDC (loss of power)
Normal or low rpm with a TIT increase then TIT decrease and increase

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10
Q

Prop

  • when to use
  • power source
  • test perameters
A

Whenever stuctural icing is evident
BUS B: heater elements, aft lighting trans: GND test, EMDC: control
Reduce voltage; same speed (160 secs for complete cycle)

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11
Q

Wing

  • when to use
  • power source
  • test perameters
A

When ice builds up to .5”
EMDC: mod valves, MEDC: caution lights
10 degrees TIT rise with corresponding wing temp rise

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12
Q

EMP

  • when to use
  • power source
  • test perameters
A

When structural icing is encountered in flight (used with wing deice)
BUS A: parting strips, BUS B: cycling strips, MEAC: timer motor, EMDC: relay control, MEDC: caution lights
Same power; high speed motor; 44 sec vs 176 secs for normal speed

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13
Q

Windshield

  • when to use
  • power source
  • test perameters
A

Before start to secure checklists
MEAC/MEDC: front wiper power control, BUS A/EMDC: side
MEDC: caution lights
N/A

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14
Q

Drive spline shear HP

A

257 HP

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15
Q

Relief valve nominal px

PRESS LOW light

A

100psi

Below 50psi

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16
Q

TEMP HIGH Light

A

Exceeding 121 degrees C

17
Q

Control valves fully open at how many feet?

A

12,000

18
Q

Heat exchanger REFR OVHT light on at

A

Exceeding 166 degrees C

19
Q

Automatic temperature control mode range

A

18-29 C

20
Q

A valve

A

Turbine bypass valve
Air that is partially cooled by heat exchanger to bypass the fregeratuon turbine unit to enter the flight station or cabin risers

21
Q

B valve

A

Turbine shutoff valve

Air passes the expansion turbine driving the secondary compressor

22
Q

C valve

A

Hot air bypass valve (hot compressed air from EDC or multiplier enters the riser)

23
Q

Pressure ratio limiting
Yellow condtion psi
Red condition

A

72psi

50psi

24
Q

Prop and Emp uses what heat?

A

Electrical heat

25
Q

Sources of heat

A

APU, EDC’s, 14th stage bleed air

26
Q

4 functions of the Aux Vent switch placed in the open position

A

EDC’s dumped
Firewall Shut off valve closes
Outflow valve opens electrically
The valve itself opens fully