Electrical System

What are the electrical power generation sources on the ATR 72-600 aircraft?
Two AC wild frequency generators.
Two engine-driven DC starter/ generators.
Main and emergency batteries.
All of the above.
What are the voltage requirements on the DC system?
24V
26V
28V
25V
What type of batteries is used on the ATR 72-600 aircraft?
24V Ni-CD 43 Ah (main BAT), 24V Ni-CD 17Ah (emer BAT)
28V Ni-CD 43 Ah (main BAT), 28V Ni-CD 17 Ah (emer BAT)
26V Ni-CD 43 Ah (main BAT), 26V Ni-CD 17Ah (emer BAT)
30V Ni-CD 43Ah (main BAT), 30V Ni-CD 17Ah (emer BAT)
Where is the DC starter generator located?
On the LP spool through the reduction gear box
On the LP spool through the accessory gear box
On the HP spool through the reduction gear box
On the HP spool through the accessory gear box
When is the DC starter generator a Starter?
0-25% NH
0-45% NH
0-41.5% NH
0-66% NH
When is the DC starter generator a Generator
Above 66% NH
Above 65% NH
Above 61.5% NH
Above 66.5% NH
Can the DC generators provide power when the GPU is connected and in the ON position?
Yes
No
With Dual DC Gen Loss is DC power still available?
Yes through the TRU
Yes through the Hot battery bus with the TRU inoperative.
No
Both a+b
What is the purpose of the BIC?
Allows INV 1 and 2 to be online when only one generator is operating or EXT power connected.
Allows DC BUS 1 and 2 to be online when only one generator is operating or EXT power connected.
Allows DC GENI and 2 to be online when only one generator is operating or EXT power connected.
Allows MAIN BAT and EMER BAT to be online when only one generator is operating or EXT power connected.
The source of constant frequency AC power consists of?
Two batteries
Two ACW generators
Two DC generators
Two STATIC inverters
What is the output of the inverters?
115V
110V
120V
124V
Where are the ACW generators located and when is it a generator?
On the reduction gear box and at 61.5% NP
On the accessory gear box and at 66% NP
On the reduction gear box and at 66% NP
On the accessory gear box and at 61.5% NP
On the ground with one ACW generator online and BC closed what BUS is shed?
ACW BUS 1
ACW BUS 2
DC GND Service Bus
ACW GND Service Bus
On the ground with an EEC or PEG fault with the fuel governing mode lost is that specific ACW generator available?
Yes
No
In Flight with one ACW fault which BUS is shed first?
ACW BUS 1
ACW BUS 2
DC GND SERVICE BUS
ACW GND SERVICE BUS
Is the ACW BTC automatic or manual
Automatic
Manual
With the AC GPU ON which BUSES are supplied with power through the BTC?
ACW BUS 1
ACW BUS 2
ACW GND SERVICE BUS
All of the Above
With the ACW GPU connected and in the ON position with Both ACW online which source is powering the BUSES?
ACW 1
ACW 2
ACWGPU
Both a + b
In the event of DUAL DC GEN LOSS the TRU partially energizes the DC system through which BUS?
ACW BUS 1
ACW BUS 2
ACW Service BUS
ACW GND POWER
What is the function of the ACW BPCU?
Control and protection of the EXT PWR
Control and protection of the BUS TIES/BTC
Control and protection of the SVCE BUS
All of the above
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