900 Electrical Flashcards

1
Q

Each IDG consists of

A

A constant speed drive and a generator

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2
Q

The IDG automatically disconnects when

A

tempurature or torque limits are exceeded.

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3
Q

The ADG continues to operate and supply power to the ADG bus until what airspeed?

A

Approximately 140 kts

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4
Q

Can the ADG deployed on the ground?

A

Automatic deployment is inhibited on the ground by a wait on wheels switch.

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5
Q

The power supply priority for AC electrical is

A

On side generator

APU

Off side generator

Ground power

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6
Q

What power sources are available for the service configuration

A

Either external power or the APU generator

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7
Q

What buses are powered in the service configuration

A

AC service bus

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8
Q

The ADG is automatically deployed if

A

there is a loss of power to both AC bus 1 and 2.

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9
Q

The ADG bus supplies power to

A

The AC Essential bus

Hydraulic pump 3b

Flaps and slats at half speed

Pitch trim channel 2

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10
Q

Main battery amp and volt

A

17 amp hour /24 volt nickel cadmium battery

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11
Q

APU battery amp and volt

A

43 amp hour. 24 V nickel cadmium battery

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12
Q

From what source is each battery charged?

A

The main battery is charged by AC bus one.

The APU battery is charged by AC service bus.

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13
Q

The APU generator is driven by

A

Directly by the APU gearbox

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14
Q

What powers the DC emergency bus

A

The DC battery bus and the APU batt direct bus (Continuously)

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15
Q

Failure of one Essentil TRU?

A

ESS tie connector closes

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16
Q

What will occur if we lose both Essential TRU’s

A

Cross tie closes

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17
Q

If complete loss of AC power Will The essential tie close?

A

Yes… To connect the DC essential bus to the battery bus for emergency power

18
Q

If the DC service which is selected on,

A

The DC service bus is powered from the APU battery direct bus

19
Q

EMER POWER ONLYmsg?

A

Indicates the ADG has deployed

20
Q

AC service bus is normally powered from AC bus two.. On the ground?

A

Powered from the APU or external power

21
Q

If power is restored by pressing thePWR XFR OVERRIDE button..what happens?

A

Restored IDG willpower AC bus one and two However the ADG will continue to power The critical flight controls and the ADG bus

22
Q

DC power is supplied by

A

4 TRU’s and two batteries

23
Q

What’s feeds the DC emergency bus

A

Both the battery bus and the APU battery direct bus

24
Q

Which is on the emergency bus

A

Hydraulic SOV Engine fuel SOv APU fuel SOV Firex

25
Power for starting the APU is provided by
APU battery
34
How many AC buses
4
35
How many DC buses
9
36
The APU. Generator is driven?
Directly by the APU gearbox (At a constant speed) (W/its own GCU)
37
Failure of an IDG Will automatically transfer the load from the failed IDG to the remaining operative IDG For any reason other than?
A fault on its associated
38
Max TRU load in flight
120 Amps
39
Maximum time with DC power only for CRT displays
Five minutes
40
What is the constant speed drive depicted as on the synoptic page?
IDG
41
Can the AC ESS bus transfer happen both automatically and manually?
Yes
42
What does the AC service bus provide power for
Passenger cabin and lavatory cleaning
43
When does the DC utility bus shed?
When the main Tie closes
44
ADG Will continue to operate and supply power until
135 kts
45
Where are thTRUs located?
In the nose.
46
On EMER PWR you will have electrical power for approximately
30 minutes
47
The voltages of the AC and DC electrical systems are
115V and 28V
48
The constant speed drive in the IDG is cooled by,
An air/oil heat exchanger Using N1 fan air
49
What are the 4 AC buses
AC bus 1 AC bus 2 AC essential bus AC service bus
50
Bus protection is provided by the?
ACPC, GCU and other electrical relays