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Checklist > Safety Check And Power Up > Flashcards

Safety Check And Power Up Flashcards

1
Q

IESS needs how long to initialize

A

90 seconds

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2
Q

When the batteries turn the airplane on what screens come on?

A

Only 2 and 3. If more come on call MX

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3
Q

What voltage must be verified after turning on the batteries

A

22.5

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4
Q

What do you do if the voltage is below 22.5 but above 21.0?

A

You need to recharge the batteries using generators on taxi out or any AC Source. Using the time chart in SOPM

If voltage is below 21 call MX no dispatch

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5
Q

Prior to performing the Fire Extinguisher Test what ECAS messages must not be preset

A

No Fire Protection test messages

EICAS fire protect fail or APU fire protect fail, its amber.

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6
Q

When must an originating check be performed

A
  1. Crew or Airplanes first flight
  2. Air plane came back from Max
  3. If left unattended just flow the switches
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7
Q

What and when does the Flight Control Power Up Build in Test occur PBIT

A

The test occurs as soon as AC source is introduced.

The Electrical PBIT

  • starts as soon as ac power is introduced
  • if interrupted you may get a No dispatch msg.
  • the test is interrupted with any hydraulic pump turned on
  • loss in AC Power
  • flight control panel switches.
  • A Status message tells you the test is in progress.
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8
Q

When the batteries are turned off what is still powered

A

HOT BATT BUS, fire protection, Fuel panel

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9
Q

On the first flight of the day, with temperatures below -18°C (0°F), or when the smart probes are frozen what must you do?

A

Run a ADSP Heater test, to remove frozen contaminates from the Smart Probes

Run The hydraulic Warm up test.

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10
Q

When do you accomplishlish the Hydraulic system warm up?

A

when hydraulic resovour is below -18c

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11
Q

Can you continue if you interrupt a Flight Control PBIT

A

yes as long as you don’t have an expire message displaying.

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12
Q

What will interrupt the E-PBIT

A
  1. Loss of AC Power.
  2. Turning on Hydraulics
  3. Moving Flight controls
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13
Q

When does the H-PBIT begin

A

When all 3 hydraulic systems are powered. Moving flight controls will interrupt the test.

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14
Q

What do you do if the E-PBIT is interrupted ?

A

You may continue as long as you don’t have a FLT CTRL BIT EXPIRED message.

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15
Q

BATT 1 - On

BATT 2 - Auto

What buses are being powered

A

DC ESS BUS 1,2,3

AC STBY BUS - via the inverter

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16
Q

Why is BATT placed on AUTO

A
  1. It isolates APU bus for APU start
  2. Acts as a back up to DC ESS BUS 1,2,3
  3. If Using a DC GPU it allows GPU to Power the APU Bus
17
Q

With only the batteries on. What do you see

A
  1. Screens 2,3
  2. CCD1
  3. IESS
  4. Clock
  5. MCDU2
  6. DCU
  7. Compass Light
18
Q

Why is it important for the DCU to be powered by DC power

A

It allows the airplane to navigate using the DCU

19
Q

When you check the emergency lights what lights come on. How many lights for how long. ?

A

4 lights for 10 minutes

  1. Pod lights
  2. Emergency signs
  3. Placards
  4. Door escape
  5. Tracking lights - luminescent powered.
20
Q

What can interrupt the E-PBIT

A
  1. Turning on the hydraulic pumps
  2. Flight control panel switches are cycled
  3. AC Power is interrupted.
21
Q

Once you Turn the batteries On and AUTO what Items do you check next

A
  1. 90 for IESS
  2. Screens 2 and 3 only
  3. 22.5V
22
Q

what is the normal procedure to start the APU

A

BATT 1 must be ON and BATT 2 must be in AUTO for the APU to start.

Step 1
EMER STOP Button ……………………………………………………………………..Guarded
Step 2
APU SELECTOR KNOB ………………………………………… ON, START then release

23
Q

How do you transfer electrical power from GPU to APU?

A
  1. Start APU - Make sure APU Button is pressed in.
  2. Verify Electrical Page
  3. Deselect GPU button
24
Q

How do you transfer power from APU to GPU?

A

Once Available light comes on, press in GPU button and shutdown the APU.

25
Q

Why do we check for the 22.5 Voltage when turning on the batteries?

A

22.5v will give us 10 minutes of emergency power

26
Q

Why do we do the safety and power up Checklist?

A

To make sure power can be applied to the aircraft

27
Q

If you are recharging the batteries because they were below 22.5. Does taxi time count towards this charge?

A

Yes

28
Q

What happens if you hold the FIRE TEST BUTTON for more than 10 seconds?

A

APU will shutoff

29
Q

Emergency Equipment Cap side

A
  1. Circuit Breaker Panel
  2. Rope
  3. Life Vest
  4. Jumpseater Life Vest
  5. Flash Light
30
Q

Emergency Equipment FO Side

A
  1. Circuit Breakers
  2. Rope
  3. Life Vest
  4. Flash Light
  5. Behind Seat Rat pins
31
Q

Door way Emergency Equipment

A
  1. Crash Axe
  2. Fire Extinguisher
  3. PBE
  4. Jump Seater Headset and seat condition
32
Q

MX Status check? What are you looking for?

A

Verify No Write ups that you;d prevent us from adding power to the airplane.

33
Q

Once you have established AC power, what is the last thing that needs to be done?

A

Turn on NAV lights

34
Q

After how many seconds do the EICAS Messages populate?

A

After 30 seconds of adding DC power.

35
Q

When you add DC power the only screen you should see are?

A

STATUS and EICAS

36
Q

Can you access the synoptic pages with DC power only?

A

No, only EICAS and Status pages only.

37
Q

To view battery temperature what source of power do you need?

A

You need AC power. So you need AC power to start charging the batteries if they are below 22.5 volts.

38
Q

When checking the Slats/Flaps in the Safety and power up what are you checking?

A
  • Handle position matches EICAS position and outside position.

Checklist (14 decks)

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