Electrics Flashcards

1
Q

What does the electrical system of an airplane generate and distribute?

A

AC and DC power to other airplane systems

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2
Q

What are the main components of the electrical system?

A
  • main AC power
  • backup power
  • DC power
  • standby power
  • flight controls power
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3
Q

How does the system operation function in terms of electrical faults?

A

Electrical faults are automatically detected and isolated

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4
Q

What is the primary source of electrical power in the airplane?

A

The AC electrical system

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5
Q

What is the function of the Electrical Load Management System (ELMS)?

A

Provides load management and protection to ensure power availability

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6
Q

What happens when electrical loads exceed available power?

A

ELMS automatically sheds AC loads by priority

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7
Q

List the order of load shedding by the ELMS.

A
  • galleys first
  • utility busses
  • individual equipment items powered by the main AC busses
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8
Q

What message displays on the electrical synoptic when load shed conditions exist?

A

LOAD SHED

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9
Q

What are the main AC electrical power sources?

A
  • left engine integrated drive generator (IDG)
  • right engine IDG
  • APU generator
  • primary external power
  • secondary external power
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10
Q

How do the main AC power sources normally operate?

A

Isolated from one another

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11
Q

What occurs during power source transfers on the ground?

A

Operating sources are momentarily paralleled to prevent power interruption

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12
Q

What happens when an engine starts with the GENERATOR CONTROL switch ON?

A

The IDG automatically powers the respective main bus

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13
Q

How can the IDG be electrically disconnected from the busses?

A

By pushing the GENERATOR CONTROL switch to OFF

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14
Q

What indicates low oil pressure in an IDG?

A

The DRIVE light illuminates and the EICAS message ELEC DRIVE FAULT L or R displays

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15
Q

What is the function of the APU generator?

A

Can power either or both main busses and may be used in flight as a replacement to an IDG source

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16
Q

What happens when the APU generator becomes available?

A

It automatically connects to both main AC busses if no other power source is available

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17
Q

What does the PRIMARY EXT PWR switch do?

A

Connects primary external power to both main busses

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18
Q

What is the purpose of the secondary external power source?

A

Can power the left and right main busses

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19
Q

When is the ground service bus powered?

A

Normally powered by the right main bus

20
Q

What does the ground handling bus provide power for?

A
  • cargo handling
  • fueling/defueling operations
  • engine turning system
  • other equipment during ground operations
21
Q

What is the function of the backup electrical system?

A

Automatically provides power to selected airplane systems

22
Q

What are backup generators used for?

A

Provide backup power and supply power to the flight control DC electrical system

23
Q

What is the role of transformer-rectifier units (TRUs) in the DC electrical system?

A

Produce DC power from AC transfer busses

24
Q

What does the main battery provide?

A

Standby power to other busses

25
Q

What happens if the main battery charge is below the level required for dispatch?

26
Q

What does the hot battery bus provide power to?

A

Standby power to other busses

See Standby Electrical System

27
Q

What maintains the main battery fully charged?

A

The main battery charger

28
Q

What message is displayed if the main battery charge is below the required level for dispatch?

A

MAIN BATTERY LOW

29
Q

How long can battery charging take with one or both engines running or with external power?

A

5-10 minutes

30
Q

What happens to battery charging time when the APU is running?

A

It goes to a slower charging mode and can take up to 18 minutes

31
Q

What does the APU battery power?

A

The APU electric starter

32
Q

What is the purpose of the TOWING POWER switch in BAT position?

A

Permits towing operations without AC power

33
Q

What does the standby electrical system provide power to?

A

Selected flight instruments, communications and navigation systems, and the flight control system

34
Q

What components make up the standby electrical system?

A
  • The main battery
  • The standby inverter
  • The RAT generator and its associated generator control unit
  • The C1 and C2 TRUs
35
Q

What does the standby inverter do?

A

Converts DC power to AC power

36
Q

What does the RAT generator provide standby power to?

A

The C1 and C2 TRUs

37
Q

Does the RAT generator have operating time limits?

38
Q

When is the RAT deployed automatically?

A

If both AC transfer busses lose power in flight

39
Q

What systems can electrical power to some cabin and utility systems be controlled from?

A

The flight deck

40
Q

What does the IFE/PASS SEATS switch control?

A
  • In-Flight Entertainment (IFE) system
  • Passenger seat systems
  • Video surveillance cameras
  • Flight deck personal electronic device (PED) power outlets
41
Q

What happens when the IFE/PASS SEATS Power switch is selected to OFF?

A

Power is removed from all IFE components and passenger seats

42
Q

What does the CABIN/UTILITY Power switch control?

A

Power to cabin and utility systems

43
Q

When the CABIN/UTILITY Power switch is OFF, what systems still receive power?

A
  • Night lights
  • Reading lights
  • Attendant work lights
  • Some galley and crew rest lights
44
Q

What does the Passenger Wi-Fi switch allow?

A

On-board Wi-Fi functionality to be available to the flight crew and passengers when ON

45
Q

Fill in the blank: The standby inverter powers the AC standby bus if the _______ is not powered.

A

left transfer bus