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A320 Systems > Electrics > Flashcards

Electrics Flashcards

1
Q

How many generators (including APU) can power all electrical needs?

A

1

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2
Q

In flight, during generator failure, what is automatically shed?

A

Main galley power

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3
Q

What is the main difference between when Gen 1 fails versus Gen 2?

A

Gen 1 is connected to the Essential Bus and Shed while Gen 2 requires the AC ESS FEED button depressed

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4
Q

When RAT deploys, what does it power?

A

AC and DC ESS BUS and SHED

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5
Q

In an emergency what does BATT 1 power?

A

AC ESS BUS through inverter

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6
Q

In an emergency what does BATT 2 power?

A

DC ESS BUS

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7
Q

What are the electrical priorities?

A 
G enerators
E xternal Power
A pu generator
R am air turbine
B atteries
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8
Q

What are the capacities of the generators and the APU?

A

90 KVA
3 phase
115-200 V
400 Hz

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9
Q

What are the capacities of the emergency generator?

A

5 KVA
3 phase
115-200 V
400 Hz

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10
Q

What do the (TR) transformer-rectifiers do?

A

Convert AC to DC

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11
Q

When will you see a green arrow connected to the battery?

A

only when current is >1 amp

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12
Q

What are the limitations for the IDG FAULT buttons?

A

Do not depress more than 3 seconds.
Engine must be running or windmilling
Can be reset on ground only

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13
Q

When will you get the IDG FAULT light on?

A

High IDG oil temp

Low IDG oil pressure

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14
Q

When will the batteries start charging?

A

<26.5V

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15
Q

When will the battery contactors close?

A

AC BUS 1&2 not powered by other sources (no EMER GEN during flight, worst case)

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16
Q

When will the auto batt cut-off?

A 
Ground
BAT in AUTO
AC power source N/A
Batt voltage low
(reset by cycling BAT buttons)
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17
Q

How long are batteries prevented from charging after APU start?

A

30 minutes

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18
Q

During preflight, what white lights should be present on the ELEC panel?

A

None!

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19
Q

When you turn on the battery what is the max charging current allowed?

A

<60A and decreasing within 10 seconds

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20
Q

What tells you that the APU is powering the AC?

A

AVAIL light on the APU START button AND AVAIL light on the EXT POWER button

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21
Q

When you start engine 2, what happens to the bus tie?

A

Opens, APU now powers BUS 1 and Generator powers BUS 2

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22
Q

RAT & EMER GEN FAULT light is on, what does this mean?

A

The RAT takes 8 seconds to spool up before coming on-line, during this time you are running off the batteries.

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23
Q

What is the min speed for the RAT to function?

A

140kts

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24
Q

During landing, at what speed does the EMER GEN become unavailable?

A

125kts

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25
Q

What happens below 50kts during total electrical failure?

A

All displays blank
Braking and engine control
VHF1
NO nosewheel steering

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26
Q

Right side dome light main panel flood lights (left two columns only) and the standby compass light.

A

Which cockpit lighting is available during an emergency electrical situation?

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27
Q

A static inverter transforms DC power from Battery 1 into one KVA of single-phase 115v/400hz AC power which is then supplied to part of the AC essential bus.

A

What is the function of the static inverter?

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28
Q

The aircraft has two types of C/Bs. Monitored (green): When off for more than one minute the C/B TRIPPED warning is triggered on the ECAM. Non-monitored (black).

A

How many types of circuit breakers has the aircraft?

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29
Q

No.

A

Can you reconnect an IDG in flight?

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30
Q

Two engine generators one APU generator and one external power source.

A

AC Power (115v) can be provided by which power sources?

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31
Q

Engines external power APU.

A

What is the order of priority for the different generators?

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32
Q

I have to check that the BAT pushbuttons are on and switch the external power on.

A

If the battery voltages are below the minimum how do you charge them?

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33
Q

Electrical power to both AC BUS #1 & #2 is lost and the aircraft speed is above 100 knots.

A

When does the RAT automatically deploy?

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34
Q

No.

A

Is it possible to connect the engine driven generators in parallel?

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35
Q

External power is supplying the aircraft electrical systems.

A

What does the blue EXT PWR ON light mean?

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36
Q

It is a reminder that the main galley has been shed automatically following the loss of one generator.

A

After IDG disconnection why do you get a GALLEY SHED indication in the SD?

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37
Q

No but some loads are shed in both main galleys.

A

If both engine generators are powering the system and one subsequently fails are any busses unpowered?

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38
Q

The GAPCU controls the frequency and voltage of the APU generator / external power output protects the network by controlling the emergency generator line contactor and controls the emergency generator start-up.

A

What is the purpose of the Ground and Auxiliary Control Power Unit (GAPCU)?

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39
Q

The ground power connector is near to the nosewheel on the right side of the fuselage.

A

Where is the ground power connector?

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40
Q

The contactor of each TR opens automatically in case of overheat or minimum current. The other TR automatically replaces the faulty one. The ESS TR supplies the DC ESS BUS.

A

What occurs in case of a TR fault?

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41
Q

By pushing the EXT PWR Pb thus disconnecting the external power.

A

Having started the APU with external power connected how can you get the APU generator to power the electrical system?

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42
Q

The blue hydraulic via the RAT.

A

What powers the emergency generator?

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43
Q

You have to check that both batteries are off.

A

You enter a dark cockpit what action is necessary before checking the battery voltages?

44
Q

Two main Transformer Rectifiers TR 1 and TR 2 supply the aircrafts electrical system with up to 200 amperes of DC current. A third identical TR the ESS TR can power the essential DC circuit from the emergency generator if the engine and APU generators all fail or if TR 1 or TR 2 fails.

A

What is the purpose of the Transformer Rectifiers (TR’s)?

45
Q

Controls the frequency and voltage of the generator output and protect the network by controlling the associated generator line contactor (GLC).

A

What are the main functions of the Generator Control Unit (GCU)?

46
Q

The AC ESS BUS is normally supplied from the AC BUS 1 it may be supplied be AC BUS 2 through the AS ESS FEED pb.

A

Which bus supplies the AC ESS BUS?

47
Q

Two main batteries have a capacity of 23 ampere-hours each.

A

What is the capacity of the main batteries?

48
Q

Auto:The battery charge limiter automatically closes/opens the corresponding battery line contactor. The batteries are connected to the DC BAT BUS in the following cases:• APU starting until N < 95%. (limited to 3 min when the emergency generator is running)• Battery voltage < 26.5 V (battery charge).• Loss of AC BUS 1&2 when below 100 knots (EMER GEN not supplying).OFF:The battery charge limiter is not operating: the battery line contactor is open.FAULT Light:The charging current for the corresponding battery is outside limits. In this case the battery contactor opens.

A 
BAT 1 (2) pb
(ELEC Panel)
  • Auto
  • OFF
  • FAULT Light
49
Q

Switch spring loaded out.Do not hold > 3 sec.Do not disconnect when engine not windmilling.FAULT Light:- IDG oil outlet overheats (above 185°C), or- IDG oil pressure is low (inhibited at low engine speed: N2 below 14 %)LT extinguishes when the IDG is disconnected.

A 
IDG 1 (2) pb (guarded)
(ELEC Panel)
  • FAULT Light
50
Q

ON:Generator line contactor closes if electrical parameters are normal.OFF:Generator line contactors open. The fault circuit is reset.FAULT Light:- The generator control unit (GCU) trips it.- Line Contactor open with the GEN pb selected ON

A 
GEN 1 (2) pb
(ELEC Panel)
  • ON
  • OFF
  • FAULT Light
51
Q

ON:Line contactor closes if parameters are normal and the EXT PWR line contactor is open.OFF: Line contactor opens. The fault circuit is reset.FAULT LT:- The generator control unit (GCU) trips it.- Opening of the line contactor (except if the APU GEN pb is selected OFF). The light is inhibited when APU speed is too low or if the APU GEN line contactor opens after EXT PWR or ENG GEN takes over.

A 
APU GEN pb
(ELEC Panel)
- ON
- OFF
- FAULT Light
52
Q

AUTO:The bus tie contactors (BTCs) open or close automatically.OFF:Both bus tie contactors open.

A

BUS TIE pb
(ELEC Panel)

  • AUTO
  • OFF
53
Q

NORMAL:The AC ESS BUS is supplied from AC BUS 1. It is automatically supplied by AC BUS 2, when AC BUS 1 is lost.ALTN:Comes on when manually selected. The AC ESS BUS is supplied from AC BUS 2.FAULT LT:AC ESS BUS is not supplied.

A

AC ESS FEED pb
(ELEC Panel)

  • NORMAL
  • ALTN
  • FAULT Light
54
Q

AUTO:Main galley, secondary galley and in-seat power supply are supplied.The main galley and in-seat power supply are shed automatically when:- In flight: only one generator is operating.- On the ground: only one engine generator is operating. (Except APU or EXT power.)OFF:The main galley, secondary galley and in-seat power supply are not supplied.FAULT LT:When the load on any generator is more than 100% of rated output.

A

GALY & CAB pb
(ELEC Panel)

  • AUTO
  • OFF
  • FAULT Light
55
Q

AVAIL light comes on green if:- External power is plugged in, and- External power parameters are normal.Pressed momentarily:Opens/Closes the external power line contactor. The ON light comes on blue when closed.

A

EXT PWR pb
(ELEC Panel)

  • AVAIL Light
  • ON Light
56
Q

ON:All aircraft commercial electrical loads are supplied:- Cabin and cargo lights- Water and toilet system- Drain mast ice protection- Galley- Passengers’ entertainment- Semi-automatic cargo loading (if installed)OFF:Switches off all aircraft commercial electrical loads.

A

COMMERCIAL pb
(ELEC Panel)

  • ON
  • OFF
57
Q

AUTO:RAT deploys when- AC BUS 1&2 is not electrically supplied and speed >100 knots.Pressed:Manual RAT extension.

A

MAN ON pb (guarded)
(EMER ELEC PWR panel)

  • AUTO
  • Pressed
58
Q

FAULT LT:This light comes on red if the emergency generator is not supplying power when AC BUS 1&2 are not powered.

A

RAT EMER GEN
(EMER ELEC PWR panel)

  • FAULT Light
59
Q

Pressed and held:• If AC NORMAL BUSES are supplied:- The EMER GEN is driven hydraulically if the blue electric pump is running.The AC ESS BUS and the DC ESS BUS are connected to the emergency generator.(The DC ESS SHED and AC ESS SHED buses are not powered.)- ECAM displays the ELEC page automatically (only on the ground).• If only the batteries supply the aircraft:- The static inverter powers the AC ESS BUS.

A

EMER GEN TEST pb (guarded)
(EMER ELEC PWR panel)

  • Pressed and held
60
Q

OFF:GEN 1 line contactor opens. AC BUS 1 is supplied from GEN 2 through bus tie contactors. This is used for the avionics smoke condition to isolate GEN 1, but it continues to power one fuel pump in each wing tank.Smoke LT:Avionics smoke

A

GEN 1 LINE
(EMER ELEC PWR panel)
- OFF
- SMOKE LT

61
Q

Blue Hydraulic power from the RAT

A

What powers the emergency generator?

62
Q
  • The system has its own alternator making it independent of the aircraft electrical system when N2 is above a set value- If this alternator fails, the FADEC automatically switches to aircraft electrical power
A

What is the power source for the FADEC?

63
Q

To provide AC power to the AC ESS bus from the battery when the EMG GEN is not online when in Emergency Electrical configuration.

A

What is the purpose of the static inverter?

64
Q
  • Generators (ENG)- EXT PWR (Manually selected)- APU Gen- RAT Emer Gen- Batteries
A

What is the priority sequence for electrical power?

65
Q

25.5 Volts

A

When performing the PRELIMINARY FLIGHT DECK PREPARATION, what is the minimum battery voltage?

66
Q

Select battery switches ON with EXT PWR on aircraft

A

What do you do if it is below 25.5V?

67
Q

No. Battery cut-off logic prevents complete discharge when the aircraft is on the ground and un-powered - 22 VDC

A

Will the batteries completely drain if you leave the BAT switches in AUTO after AC power is removed?

68
Q

DC BUS 1 through a DC tie contactor

A

How is the BATTERY BUS normally powered?

69
Q

During the FLIGHT DECK PREPARATION check of the ELEC Panel

A

When is the battery check performed?

70
Q

Battery charging current is outside limits (BAT contactor opens)

A

What does a Bat Fault light indicate?

71
Q
  • APU Start- Battery charging- AC BUS 1&2 not powered and airspeed below 100 knots
A

What are the 3 times the batteries are connected to the BATTERY BUS?

72
Q

It is illuminated amber if one or more IRs is supplied by the aircraft battery. Also illuminates briefly during the beginning of a full alignment.

A

What does the ON BAT light indicate?

73
Q

ADIRS 2&3 will remain on battery power for 5 minutes to hold alignment until a generator can be restored.ADIRU 1 (ADIRU 3 if captain selected ATT HDG CAPT 3) will remain on battery power until generator power is restored or the batteries fail.

A

How long will each ADIRU stay on battery power?

74
Q
  • ECAM ELEC page - select- Bat 1&2 - OFF then ON- Check BATT charge current is < 60 amps and decreasing within 10 seconds
A

When performing the FLIGHT DECK PREPARATION, what are we looking for on the ELEC panel BAT check

75
Q
  • DMC1: Capt PFD, ND, Upper ECAM DU- DMC2: F/O PFD, ND, Lower ECAM DU- DMC3: Backup
A

What does each of the DMCs normally supply?

76
Q

By fuel from the HP fuel pump drawn in from the fuel manifold and then returned to its respective outer tank. When full, the outer tank spills over to the inner tank.

A

How is the IDG (Integrated Drive Generator) cooled?

77
Q

The center tank pumps turn off until the wing tank quantity reduces by 1100 lbs

A

If the IDG return fuel fills the wing tanks, what occurs?

78
Q

Separate full level switches

A

With full wing fuel what prevents the IDG fuel from overfilling the wings?

79
Q

Integrated Drive Generator

A

What does IDG stand for?

80
Q

Converts variable engine speed to constant speed for optimum generator operation

A

What is the function of the IDG?

81
Q
  • Oil pressure low (inhibited when N2 <14- Oil outlet temperature overheat- Light is inhibited when IDG is disconnected
A

What does an IDG FAULT light indicate?

82
Q
  • Do not disconnect when engine is not operating or windmilling- Do not hold button longer than 3 seconds
A

What precautions must you take when disconnecting an IDG?

83
Q

On the ground by maintenance

A

How can an IDG be reset?

84
Q

90 kVA

A

What is the max continuous load rating of the engine and APU generators?

85
Q

The generator line contactor is open because of a fault detected by the GCU

A

What does the APU GEN FAULT light indicate?

86
Q
  • APU speed to low- Line contactor OPEN after EXT PWR or ENG GEN takes over
A

When is the APU GEN FAULT light inhibited?

87
Q

Allows the BUS TIE CONTACTORS to open and close automatically to maintain power to both AC BUS 1&2:- Allows a single source to power the entire system- Allows connection of the APU GEN or EXT PWR to the system- Inhibits multiple sources to connect simultaneously

A

What is the function of the BUS TIE in the AUTO position?

88
Q

Sheds main galley and in-seat power supply if:- Only 1 generator (APU or ENG) is available in FLIGHT, OR- Only 1 ENG generator is available on the ground

A

How does the GALLEY pushbutton work in AUTO?

89
Q

Allow AC BUS 1 to power the AC ESS BUS

A

What is the function of the AC ESS FEED pushbutton in the normal position?

90
Q

Manually by selecting ALTN on the AC ESS FEED pushbutton

A

How is AC ESS FEED transferred from AC BUS 1 to AC BUS 2?

91
Q

AC BUS 2 is powering the AC ESS BUS

A

What does the AC ESS FEED pushbutton white ALTN light indicate?

92
Q
  • Floor proximity emergency escape path marking system- Overhead emergency lighting- EXIT signs
A

What lights illuminate when the DC ESS SHED BUS fails?

93
Q
  • AC ESS and AC SHED- DC ESS and DC SHED
A

What buses are powered by the emergency generator?

94
Q
  • Loss of AC BUS 1 & 2,- Airspeed above 100 Kts, and- Emergency generator not supplying AC power
A

What does the RAT & EMER GEN red fault light indicate?

95
Q
  • AUTO- RAT will automatically extend if AC BUS 1 & 2 are not powered and airspeed is >100 Kts- MAN- Extend the RAT at any time
A

What is the function of the RAT & EMER GEN pushbutton?

96
Q
  • GEN 1 Line Contactor opens and the white OFF light illuminates- AC BUS 1 is powered by GEN 2 through the BUS TIE CONTACTOR- GEN 1 continues to power 1 fuel pump in each wing tank
A

What happens when you push the GEN 1 LINE pushbutton

97
Q

At least 1 generator load is above 100% rated output

A

What does the amber “FAULT” light in the GALLEY pushbutton indicate?

98
Q
  • A Fault is detected by the GCU -Overload -Over/under voltage -Differential fault (short)And/or:-The generator line contactor is open
A

What does a “FAULT” on the ENG GEN pushbutton indicate?

99
Q

Prior to engine start because the GEN is selected ON by the line contactor is open - normal condition

A

When is it normal to see the ENG GEN FAULT light illuminated?

100
Q

Normal AC is lost and the emergency generator is not supplying power

A

What does the red “FAULT” light on the RAT & EMER GEN push button indicate?

101
Q

During the 8 seconds RAT deployment and power up

A

When should the red “FAULT” light on the RAT & EMER GEN pushbutton be expected?

102
Q

5 kVA

A

What is the output of the Emergency Generator?

103
Q

No. Maintenance function only

A

Do pilots ever use the EMER GEN TEST pushbutton?

104
Q

Smoke procedures

A

When would you select the GEN 1 LINE pushbutton?

105
Q

20 minutes

A

How long will it take to charge the batteries?

106
Q

1 kVA

A

What is the output of the static inverter?

107
Q

Yes, RAT MAN ON from the HYD panel

A

Is there another way to deploy the RAT?

A320 Systems (21 decks)

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