06 Electrics Flashcards

1
Q

What is initiated by selecting the Battery switch to ON?

A

The L CCR start-up sequence

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2
Q

In the Generator Control (GEN CTRL) switch, what does the amber OFF light indicate?

A

The generator breaker is open

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3
Q

In the external power switches: -

a. What does the AVAIL light indicate?
b. What doest he ON light indicate?

A

a. External power is plugged in and power quality is acceptable
b. External power is selected ON

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4
Q

With an engine running, what is indicated when the generator DRIVE light illuminates?

A

A generator drive malfunction has occurred

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5
Q

In addition to traditional electrically powered systems, what other systems are electrically powered?

A
  • Engine start
  • Pressurization
  • Wing ice protection
  • Stabilizer trim
  • Wheel brake systems
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6
Q

How many engine driven generators are there to power the main AC buses?

A

Four variable frequency engine starter/generators

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7
Q

What other aircraft power source for the main AC buses is available in flight?

A

Two variable frequency APU starter/generators

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8
Q

What AC power sources are available on the ground before engine start?

A

Three external AC power receptacles as well as the two APU generators

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9
Q

Can any of these AC power sources normally be connected to run together?

A

No

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10
Q

What electrical sources can be used for engine start?

A
  • External A/C power
  • APU generated power
  • The opposite engine’s generated power
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11
Q

What electrical sources can be used for APU start?

A

Forward external power, APU battery, or engine generated power

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12
Q

On the ground, how many APU generators are available to power the main AC buses?

A

Both

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13
Q

If the APU is not available, how many external power sources are required for optimal engine start performance?

A

Three, both forward and one aft receptacle

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14
Q

How many primary batteries does the aircraft have?

A

Two, the Main and APU batteries

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15
Q

Can the Main battery be used to start the APU?

A

Yes, it assists the APU battery

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16
Q

What are the primary sources of power for the flight control electronics?

A

Three engine driven Permanent Magnet Generators (PMGs)

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17
Q

If PMG power is lost, what secondary sources of flight control power are available?

A

The 28Vdc bus distribution system, and the main battery

18
Q

How are higher amperage loads distributed throughout the airplane’s electrical system?

A

They are distributed directly by the bus systems which are located in the forward & aft E/E bays (Primary)

19
Q

How are lower amperage loads distributed throughout the airplane’s electrical system?

A

Via Remote Power Distribution Units (RPDUs) located throughout the airplane (Remote)

20
Q

What is the purpose of the power conversion devices?

A

They change power from one voltage or current type (AC/DC) to another

21
Q

How many main AC buses are there?

A

Four 235v AC buses, designated L1, L2, R1 & R2

22
Q

What do the main AC buses provide power to directly?

A

A limited number of high voltage AC systems

23
Q

How do the main AC buses provide power to other (lower voltage) bus systems?

A

Through power conversion devices

24
Q

On the ground, with only forward external power selected ON, how are the main AC buses powered?

A

Via the 115v AC bus distribution system through the power conversion devices

25
With both engines running, if an engine generator is not available, how is its respective main AC bus powered?
By another main AC bus
26
In flight, what is the primary power source for the 115v AC and 28v DC buses?
The main AC buses through the power conversion devices
27
Which units condition variable frequency power to energize the large motor loads?
Motor controllers
28
Which system energizes these motor controllers?
The Large Motor Power System (LMPS) located in the aft E/E bay
29
List the large motor loads theses motor controllers convert power for?
- Hydraulic Pumps - Cabin Air Compressors - Ram Fans - Engine & APU Start - Center Tank Fuel Pumps - Nitrogen Generation System
30
What system provides flight deck control/indication, power transfer functions, electrical load management and protection?
The Bus Power Control Unit (BPCU)
31
How many of these units does the aircraft have?
Two
32
When is Ground Handling mode active?
When the first forward external power receptacle is connected (not selected ON) and there are no other power sources
33
How is the Ground Service mode activated?
Selecting the GROUND SERVICE switch to ON while in Ground Handling mode
34
Which additional loads are energized in the Ground Service mode?
Limited cabin systems & lighting
35
Can the packs run when the aircraft is in External Power On mode?
Only if forward and aft external power is ON
36
In flight, when would the Ram Air Turbine (RAT) deploy automatically?
Loss of all electrical power to the Captain’s and First Officer’s flight instruments
37
The RAT provides Standby Power for which systems?
Captain’s flight instruments and other essential equipment for flight controls, navigation, and communication
38
What supplies Standby Power until RAT deployment?
The Main battery
39
List where Load Shed indications are displayed?
1. A full list on the Electrical synoptic | 2. The AIR, FUEL & HYD synoptics (shown in white), additionally, LOAD SHED text next to affected equipment symbol
40
What is the purpose of the Circuit Breaker Indication and Control (CBIC) system?
It provides indication and control for Electronic Circuit Breakers (ECB), and indication-only for Thermal Circuit Breakers (TCB