Electrical Flashcards

1
Q

Where does the AC power normally come from

A

AC ​power ​ can ​ be ​ supplied ​ by ​ two ​engine-driven ​ generators, ​an ​APU-driven ​generator, ​ and ​an ​external ​ power ​source.

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2
Q

Where does the DC power normally come from

A

DC ​power ​ is ​ supplied ​ by ​ Transformer ​Rectifier ​ Units ​(TRU) ​1, ​2, ​ESS, ​and ​Ground ​ Service, ​ which ​ are ​ powered ​ by ​the ​ respective ​AC ​bus.

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3
Q

What buses does the AC normally supply

A

AC buses 1&2, ESS AC BUS, EMER AC BUS, AVIONICS TRANSFER BUS, GALLEY BUSES 1&2, AC GROUND SERVICE BUS

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4
Q

What buses does the DC normally supply

A

DC BUSES 1&2, DUAL DC BUS,ESS DC BUS, EMERDC BUS, DC GROUND SERVICE BUS, DC GROUND HANDLING BUS

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5
Q

If all AC generator power is lost , what power is still available

A

Only battery power is available

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6
Q

What alert is presented in this situation, where will the alert be shown

A

AC supply on the SAP

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7
Q

How long would you expect the batteries to last if you loose all generators

A

30 mins or 60 mins respectively

And 1 APU start attempts

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8
Q

On the ground how can the ground handling and ground service buses be powered

A

DC​ Ground​ Service Bus​ ​​ ​The AC​ ground​ service bus​ supplies, via a ground​ service TRU,​ the​ DC​ ground service bus.​ ​When​ the​ AC​ power is​ not available,​ the​ DC​ ground service bus​ can be​ powered by​ an​ external​ ​DC​ power​ source.​ ​​ ​DC​ Ground​ Handling​ Bus ​​ ​The AC​ ground​ service bus​ supplies, via the​ Ground Service TRU​ the​ DC​ ground handling bus.​ ​When​ no​ AC​ power​ is​ available the​ DC​ ground handling​ bus​ is​ supplied directly​ by​ the batteries.​ ​The ground handling​ bus​ supplies power​ to:​ ​
AC bus 2 supplies AC ground service bus

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9
Q

When external AC is plugged in, but not switched on what is powered and what indications would you get

A

When AC​ external power is​ connected and within​ ​limits,​ the​ AVAIL​ light in the external​ power​ p/b is​ ​on, ​ the​ ​ AC ​ GROUND​ ​ SERVICE ​ light​ ​ at​ ​ the ​connector is on, and​ the AC ground service bus is ​energized.​

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10
Q

On engine start, when do engine generators normally come online

A

When​ voltage​ and​ frequency​ are​ within​predeterminedlimits,theGCUautomaticallyconnects​thegeneratortothelineandautomaticallydisconnects​thegeneratorfromthelineifafailureisdetected.Ifthe​IDGoiltemperaturebecomesexcessive,analertwillbe​presented.Ifthetemperaturecontinuestoriseabove​a​ predetermined​ value,​ the​ IDG​ will​ be​ disconnected​fromtheenginedrive.

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11
Q

What is an IDG

A

Integrated drive generator

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12
Q

What is a GCU and what does it do

A

TheIDGoutputiscontrolled​byaGeneratorControlUnit(GCU)andthegenerator​p/b.​ When​ voltage​ and​ frequency​ are​ within​predeterminedlimits,theGCUautomaticallyconnects​thegeneratortothelineandautomaticallydisconnects​thegeneratorfromthelineifafailureisdetected.

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13
Q

If an IDG overheats, what happens and what indication do you get

A

Ifthe​IDGoiltemperaturebecomesexcessive,analertwillbe​presented.Ifthetemperaturecontinuestoriseabove​a​ predetermined​ value,​ the​ IDG​ will​ be​ disconnected​fromtheenginedrive. You get a level 1 alert and display on MFDU

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14
Q

Is the APU generator equipped with a constant speed drive

A

The​ APU​ generator​ is​ not​equipped​ with​ a​ constant​ speed​ drive​ since​ the​ APU​runsataconstantspeed.

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15
Q

If external AC power is online and parameters go out of limits, what will happen

A

The​ Ground​ Power​ Control​ Unit​ (GPCU)​automaticallydisconnectstheexternalpowerfromthe​electricalsystemifitsparametersarenotwithinlimits.

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16
Q

From which generators do AC buses 1 and 2 normally receive power

A

GEN 1supplies AC bus 1

GEN 2 supplies AC bus 2

17
Q

When is the automatic AC cross-tie inhibited

A

TheautomaticcrosstiefunctionforACbuses1and2is​inhibitedduringautomaticlandings.. Also inhibited when turned off or faulted

18
Q

What buses remain powered after the ESS+ EMER PWR ONLY push button is pressed

A

the​ essential​ AC​ bus​ and​ the​emergencyACbusremainenergized. ESS DC and EMER DC ALSO

19
Q

What are the power source priorities for the ESS AC bus

A

GEN 1 , GEN 2, APU, AC EXTERNAL POWER.

20
Q

From where can the EMER AC bus obtain power

A

Under​ normal​ power​ conditions,​ the​ EMER​ AC​ bus​ is​suppliedbytheESSACbus.IfACsuppliesfailandthe​AC​ buses​ 1​ and​ 2​ and​ the​ ESS​ AC​ bus​ become​ de‐​energized,theEMERACbusissuppliedbythebatteries​viaanEMERinverter.

21
Q

When is the galley power shed automatically

A

In​ flight​ during​ single​ generator​operation,​ the​ galley​ buses​ are​ automatically​ de‐​energized.

22
Q

You are airborne and GEN 1 goes offline. The APU generator is not available, what happens, And if the APU generator is available

A

Gen 2 will supply AC power tho the whole system

If APU Gen is available then it takes the place of Gen 1 and supplies power to AC bus 1

23
Q

What happens if a TRU fault occurs, what might the fault be

A

The TRU’s​ are​ ​automatically​ disconnected in​ case​ of​ overheat or​ reverse​ current.​ ​ If​ TRU​ 1 or​ 2​ should fail​ an​ ​alert​ will be​ presented. MCL DOUBLE CHIME AND AMBER FAULT ON MFDU AND LOCAL ALERT.

24
Q

What does the dual DC bus supply and for what purpose

A

DC​ buses 1​ and​ 2​ supply​ the dual​ DC​ bus. ​ It​ provides an​ uninterrupted​ power source for​ the​ lift ​dumpers,​ anti-skid,​ and​ speed brake in​ the​ event of​ a​ DC bus​ 1 or​ 2​ failure​ during​ landing

25
Q

What can be powered by the batteries alone

A

The ground handling bus. EMER DC , EMER AC

26
Q

How can the DC buses be tied together

A

Manual​ operation ​of the​​ ​DC​ X-TlE​ p/b​ interconnects​ the​ DC​ buses.​

27
Q

If the ESS TRU becomes inop, where does ESS DC get its power from

A

lf​ the​ ESS​ TRU is​ inoperative DC ​bus​ 1 will supply​ the ESS​ DC​ bus.​ ​ lf​ the​ ESS​ DC​ bus​ becomes​ de-energized an​ alert​ will be ​presented

28
Q

Where does EMER DC bus get its power from

A

The ES​ AC​ bus​ supplies,​ via ESS​ TRU,​ the​ EMER DC​ bus.​ ​ lf​ the​ ESS​ TRU​ is​ inoperative ​the​ EMER​ DC​ bus​ is​ automatically​ supplied by​ DC​ bus​ 1.​ ​ When no​ AC​ power​ is​ available​ the​ ​EMER​ DC​ bus​ is​ automatically​ supplied​ by​ the batteries

29
Q

What does DC ground handling bus supply

A

The ground handling​ bus​ supplies power​ to:​ ​​ ​-​ ​ Passenger​ door​ (if​ installed) ​-​ ​ Fuelling​ panel​ ​-​ ​ Towing​ ​-​ ​ Hydraulic​ service​ panel​ ​-​ ​ Engine​ starter​ valve​

30
Q

What can be powered from external DC and what are the indications you get

A

Adjacent​ to​ the​ external​ AC​ receptacle is​ a​ 28​ V DC​ receptacle​ to​ provide​ power to​ the​ DC ​ground​ service bus​ and​ the APU​ starter. ​ There are no​ controls​ or​ indicators in​ the​ flight deck ​related to​ DC​ external power

31
Q

How do you remove power from a PRAM system

A

Cabin Equipment’​ includes​ components of​ the ​ ​MP3​ (PRAM) System​ and the​ Flightdeck​ USB ​ ​Power Outlet System. Power is​ removed​ with ​ ​the checklist item​ “Galley​ PWR……OFF”.​ ​

32
Q

Through which bus is the Flightdeck USB power outlet powered

A

DC BUSES 1&2