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Electrics Flashcards

(22 cards)

1
Q

Q.The EBHA Flight Control Battery amber ON legend is illuminated. What does that indicate?

A

A.The EBHA Battery is selected ON while the Main Batteries are switched Off and providing power

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2
Q

Q.When will the Electrical backup of an EBHA become active?

A

A. When all actuators on the same flight control surface loose normal hydraulic pressure.

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3
Q

Q.What does the cabin window heat system use to provide heat to the cabin windows?

A

A.Electrical power

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4
Q

Q.What will selecting the L Bus Tie switch to the ISLN position do?

A

A.Isolate the L Main AC bus from all power except the L IDG

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5
Q

Q.How are the Main Battery Chargers powered?

A

.From the respective Main AC bus

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6
Q

Q.What will occur if the L Main TRU switch is selected to the R AC position?

A

A.The L Main TRU receives power from the R AC Main bus.

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7
Q

Q.The AUX TRU is capable of providing power to which busses?

A

A.Left or Right Main DC busses, Left or Right Essential DC Busses and the Left and Right Auxiliary DC Busses

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8
Q

.What is the Power Supply for the Cabin Pressurization Control System (CPCS) channels 1 & 2?

A

A.Channel 1: LESS DC via an Inverter. Channel 2: R MAIN AC

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9
Q

Q.What are the possible power sources for the Ground Service bus?

A

A.RH Main Battery, External DC cart or Right Main DC bus

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10
Q

Q.What is the power supply for the BFCU?

A

A.The FCC UPS bus

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11
Q

Q.What powers the Emergency Vision Assurance System (EVAS)?

A

A.Each EVAS has its own battery.

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12
Q

Q.When does the ARM position of the Emergency Power System switches allow the emergency power system to activate?

A

A.If the Essential DC bus voltage becomes too low.

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13
Q

QWhat happens if all four FCC channels are unpowered or failed?

A

A.The BFCU becomes active. FCS is in Backup mode.

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14
Q

Q.From which bus does the Inverter receive its power?

A

A.Left Essential DC

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15
Q

Q.How is the EBHA Battery charged?

A

By (a) dedicated EBHA Battery Chargers).

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16
Q

Q.What items are capable of being powered from a Battery bus?

A

A.The auxiliary hydraulic pump, the APU starter, and the Essential DC buses.

17
Q

Q.During normal operations (IDGs powering the aircraft), the ground service bus receives power from which bus?

A

A.Right main DC bus.

18
Q

Q.What can power the Emergency AC bus?

A

A.Left Main AC Bus or RAT generator

19
Q

Q.If the R Gen switch indicates an amber off light, what is indicated?

A

.The IDG has been isolated from its respective Main AC bus automatically or has been selected off manually

20
Q

Q.How is the horizontal stabilizer powered?

A

A. Aircraft electric system

21
Q

Q.If the RAT is deployed due to inoperative engine and APU generators, what buses will it power (direct & indirect)?

A

A.Emergency AC Bus, EBHA and FCC UPS Busses, Left and Right Essential DC Busses

22
Q

Q.What powers the inverter?

A

A.Left Essential DC.