Electrical Flashcards

1
Q

The AC system is composed of:

A
  • two integrated drive generators (IDGs)
  • one auxiliary power unit generator (APU)
  • one inverter
  • one Ram Air Turbine (RAT)
  • one AC external power unit
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2
Q

The DC system is composed of:

A
  • two NiCad batteries
  • three transformer rectifier units (TRUs)
  • one DC external power input
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3
Q

IDG 1 or 2 Selector Knob AUTO

A

allows automatic operation of the electrical system; closes IDG contactor connecting IDG to the respective AC BUS

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4
Q

IDG 1 or 2 Selector Knob OFF

A

opens IDG contactor isolating the IDG from the respective AC BUS

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5
Q

IDG 1 or 2 Selector Knob DISC

A

must be held for one second to mechanically disconnect the IDG.

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6
Q

APU Generator Button PUSH IN/OUT

A

IN - allows auto operation by connecting APU generator to the AC BUS TIE according to source priority
OUT - opens the APU generator contact

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7
Q

AC BUS TIES Selector Knob 1 OPEN/AUTO/2 OPEN

A

1 OPEN - opens the Bus Tie Contactor 1, segregating AC BUS 1 from AC BUS 2
AUTO - allows auto operation according to system logic
2 OPEN - opens the Bus Tie Contactor 2, segregating AC BUS 2 from AC BUS 1

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8
Q

GROUND POWER UNIT Button PUSH IN/OUT

A

IN - connects the AC GPU to the AC BUS TIE according to source priority
OUT - isolates the AC GPU from the AC BUS TIE

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9
Q

TRU Toggle Switches AUTO/OFF

A

AUTO - allows auto operation by connecting the TRU to their respective DC Bus
OFF - isolates the TRU from their respective DC Bus

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10
Q

BATT 2 Selector Knob AUTO/OFF

A

AUTO - allows auto operation by connecting battery 2 to the DC ESS BUS 2
OFF - the battery supplies power only to the HOT BATT BUS 2

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11
Q

DC BUS TIE Toggle Switch AUTO/OFF

A

AUTO - allows auto operation by controlling the operation of the DC Tie Contactors according to system logic
OFF - opens all tie contactors

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12
Q

BATT 1 Selector Knob ON/OFF

A

ON - the battery is connected to the DC ESS BUS 1

OFF - the battery supplies power only to the HOT BATT BUS 1

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13
Q

IDG and APU gen rating

A

115 VAC, 40 KVA, 400 HZ, three-phase

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14
Q

Can you reconnect an IDG after manual disconnection

A

NO

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15
Q

Describe the inverter

A

the AC/DC inverter converts 28 volt DC power from batteries to 115 volt AC power to supply the STANDBY AC BUS when an AC power source is not available

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16
Q

Ram Air Turbine rating

A

115 V, 15 KVA, 400 Hz, three-phase AC

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17
Q

When is the RAT automatically deployed

A

when the AC ESS BUS loses power

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18
Q

What buses does the RAT power after deployment

A

AC ESS BUS; DC ESS BUSES are powered through the ESS TRU

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19
Q

What hydraulic system does the RAT power after deployment

A

AC motor driven hydraulic pump (ACMP 3A) from primary flight control tasks

20
Q

Min speed for RAT to power AC/DC ESS BUSES

21
Q

What will a DC GPU provide power for

A

APU START BUS

22
Q

TRUs are rated at

A

300 A; convert 115 VAC into 28 VDC

23
Q

TRU 1 provides power to

A
  • DC BUS 1
  • DC ESS BUS 1
  • DC GND SVC BUS
  • HOTT BATT BUS 1
  • Batt 1 charging
24
Q

TRU 2 provides power to

A
  • DC BUS 2
  • DC ESS BUS 2
  • HOT BATT BUS 2
  • Batt 2 charging
25
TRU ESS provides power to
- DC ESS BUS 3
26
Battery rating
NiCad 24 VDC, 27A
27
How are batteries charged
any AC source through the TRUs including the GPU and RAT
28
Battery power will last how long in an emergency with RAT not fully deployed or RAT stalled
10 minutes
29
Minimum temperature for Batt 2 for APU start
-20ºC
30
What provides power for APU start with DC GPU connected
DC GPU and not Batt 2
31
When is the DC GPU used
when batt 2 is not available or temp is below -20ºC
32
What is an ICC
Integrated Control Center is an electrical-electronic integrated device providing power distribution and protection for the airplane electrical loads, the secondary power distribution assemblies (SPDAs) and the circuit breakers that are located on the cockpit sidewall panels
33
Name the four ICCs and their locations
- left integrated control center (LICC) in Center E-BAY - right integrated control center (RICC) in Center E-BAY - emergency integrated control center (EICC) in FWD E-BAY - auxiliary integrated control center (AICC) in AFT E-BAY
34
What is an SPDA
Secondary Power Distribution Assemblies - electrical load management unit that received power from the ICC AC/DC electrical buses and distributes it to the airplane systems
35
Where is SPDA 1 located
FWD E-BAY
36
Where is SPDA 2 located
Center E-BAY
37
Which remote CBs can the flight crew reset?
SPDA; ICC must be reset by Mx on ground
38
Electric source priority
1. Respective IDG 2. APU Gen 3. GPU 4. Opposite IDG
39
BATT 1 or 2 OVERTEMP warning
associated battery temperature is above 70C
40
BATT DISCHARGING warning
batteries are discharging in an electrical emergency with no RAT assistance, or on the ground when the battery is the only power source supplying the airplane
41
ELEC EMERGENCY warning
in flight, AC main buses are de-energized
42
GPU CONNECTED caution
AC or DC GPU connected and parking brake released
43
IDG 1 or 2 OIL caution
high oil temp or low oil pressure; QRH will lead to disconnect IDG
44
REMOTE CB TRIP advisory
remote thermal or electronic CB has been tripped
45
What items are connected to DC HOT BATT BUS 1?
``` Batt 1 Courtesy/Service lights FWD DC Ceiling Lights Engine 1 Oil level indication (in engine oil panel) Engine 1A fire extinguisher Engine 2A fire extingusher Engine 1 Fuel SOV Hydraulic 1 SOV ```
45
What items are connected to DC HOT BATT BUS 2?
``` Batt 2 CMC Engine 1B Fire Extinguisher Engine 2B Fire Extinguisher Engine 2 Fuel SOV Hydraulic 2 SOV Refueling Panel Water/Waste system Controls ```