Electrical Flashcards

(54 cards)

1
Q

The sources of AC power include:

A

GPU; APU; IDG1; IDG2; RAT; Inverters

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2
Q

Once mechanically disconnected, an IDG cannot be re-connected in flight. T/F

A

“True”

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3
Q

The APU generator:

A

Can power the entire electrical system

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4
Q

Before an engine is started, based on these indications, you know that:

A

N/A WITHOUT IMAGE

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5
Q

Before engine start, according to this ELECTRIC control panel:

A

N/A WITHOUT IMAGE

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6
Q

In the event of a loss of AC power, the Ram Air Turbine (RAT) MUST be manually deployed using the RAT MANUAL DEPLOY handle. T/F

A

“False”

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7
Q

Under normal operating conditions, ____ Transformer Rectifier Units and ____ batteries provide DC power.

A

3, 2

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8
Q

On battery power only, batteries will supply essential loads for how long?

A

10 minutes

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9
Q

Under what circumstances would we use a DC GPU?

A

For starting APU with BATT2 unavailable

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10
Q

System logic provides electrical power for the aircraft according to the following source priority:

A

RAGO - Respective IDG; APU; GPU; Opposite IDG

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11
Q

How many networks make up the electrical system, and why?

A

2 - segregation and fault isolation

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12
Q

Which AC source has priority, the APU or GPU?

A

APU

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13
Q

You receive the aircraft at the gate, and the AC GPU powers it. You start the APU; once it is up and running, how can you tell that the APU generator has automatically taken over the electrical load?

A

AVAIL light shows on GPU button; APU shows on MFD electrical page

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14
Q

During “normal operation,” will a failed IDG de-power the respective AC BUS?

A

No

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15
Q

How many Display Units (DUs) come to life when you bring the batteries on line and which ones are they?

A

2: DU2 and DU3

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16
Q

Can one IDG supply the entire electrical system?

A

Yes

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17
Q

What are the two lights next to the IDGs?

A

Tells you which IDG relates to EICAS message received

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18
Q

When would the amber IDG oil indicator light illuminate?

A

HOTLOP: High oil temperature; Low oil pressure

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19
Q

When the IDG 1 (2) OIL EICAS message displays, what should the pilot do?

A

Run the QRH - disconnect affected IDG

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20
Q

If an IDG is mechanically disconnected, can the flight crew reconnect it on the ground or in flight?

A

No

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21
Q

What is the primary purpose of the IDGs?

A

Provide AC electrical power

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22
Q

What is a TRU?

A

Transformer Rectifier Unit

23
Q

What is the purpose of the Transformer Rectifier Units?

A

Converts AC to DC

24
Q

TRU transforms AC to DC, is there a way to change DC to AC?

25
What is the purpose of the inverter?
Converts DC to AC
26
Can the APU fully replace a failed IDG?
Yes
27
Does the APU generator have the same rating as the IDGs?
Yes
28
At the gate, ground power is connected. What does it mean when the GPU button says AVAIL?
AC ground power connected and voltage, amperage and frequency are good
29
How is it known that an AC GPU is hooked up to the aircraft and ready to provide electricity?
AVAIL light shows on GPU button; GPU shows on MFD electrical page
30
With AVAIL displayed on the GPU button, what happens when the GPU button is pushed in?
IN USE shows on GPU button and AC GPU is connected to the AC BUS TIE according to system priority
31
If the aircraft is using the AC GPU and the APU is started, what should the pilot be sure to do?
Deselect trhe AC GPU button so that it can be selected next time
32
What happens with the BATT 1 selector OFF?
BATT1 supplies power to HOT BATT BUS 1
33
What will charge BATT 1 and BATT 2?
Any AC power source
34
When is the HOT BATTERY BUS powered?
It is always powered
35
What are some items on the HOT BATTERY BUSES?
Engine fire extinguishers; fuel SOV; hydraulic SOV; Engine oil level indication; courtesy/service lights; refueling panel; water and waste system; CMC
36
What happens when the battery 2 switch is OFF?
BATT2 powers HOT BATT BUS 2
37
How many batteries are required for a normal APU start?
2
38
How is Battery 1 used for APU start?
Powers FADEC and EICAS
39
How is Battery 2 used for APU start?
Powers APU start bus
40
Is battery 1 necessary to start the APU?
Yes
41
Why does battery 1 have ON but no AUTO setting?
BATT1 does not require automation for APU start
42
Why does battery 2 have an AUTO setting?
To allow it to power the APU start bus
43
What is the purpose of the DC Ground power?
Provides DC power to start the APU if BATT2 is unavailable
44
Can the DC GPU charge the batteries? T/F
No
45
When will the RAT deploy?
Automatically if AC buses are not powered (electrical emergency); manually if pilot pulls handle
46
Is there an altitude restriction for operation of the RAT?
No
47
Will the RAT supply power immediately after automatic deployment?
No
48
Is there a total power loss during the 8 seconds while the RAT deploys?
No, the batteries supply power
49
Are the power ratings the same for the APU, IDG and RAT?
No - RAT provides lower power
50
The RAT icon is only displayed on the electrical synoptic page when it is deployed. T/F
"TrUE"
51
Can the remote electronic CBs in the forward electronics bay be monitored?
Yes, via the MCDU
52
If an engine is started at the gate with the GPU IN USE, is the electrical system split?
Yes
53
What is available during an electrical emergency?
DU2/DU3; guidance panel; CCD1; MCDU2; Compass backlight; IESS; both audio panels; clock
54
Whenever the electrical load increases beyond the system limit, what happens?
Load sheds galleys and right windshield heating