Electrical, page 07-10-1 Flashcards

(40 cards)

1
Q

Primary electrical us on the CL650 is AC or DC

A

115 volts AC

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2
Q

How many sources of AC power

A

2 engine driven AC generators, I APU driven AC gen, ADG, and an AC cart

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3
Q

Were is the AC receptacle

A

Right side of the forward fuselage (right nose section)

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4
Q

What is the primary source of DC power

A

4 Transformer Rectifier Units (TRU)

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5
Q

Were are the TRU’s located

A

Nose compartment

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6
Q

How many batteries for provide DC power

A

2

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7
Q

Were are the DC batteries located

A

Main battery in the nose and APU battery in the aft equipment bay

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8
Q

Were is the DC electrical receptacle

A

Rear fuselage below the right engine

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9
Q

How many circuit breaker panels are there

A
  1. Four on the flight dick, one in the aft equipment bay and forward avionics bay
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10
Q

How many AC buses are there

A

6

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11
Q

Name the AC buses

A

AC Ess
AC utility 1/2
AC bus 1/2
ADG bus

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12
Q

Each AC gen is protected by a GCU. When will they trip

A

Over/under voltage
Over/under frequency
Over current

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13
Q

What does the AVAIL annuciator mean on the APU EXT POWER switch/light mean

A

That an AC GPU is connceted, with proper voltage, frequency and phase

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14
Q

What bus supplies power to equipment essential for flight

A

The AC ESS Bus

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15
Q

What buss normally powers the AC ESS Bus

A

AC Bus 1

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16
Q

Can the AC ESS Bus be powered by other sources

A

Yes, AC Buss 2 and the ADG

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17
Q

What do the AC Utility Buses power

A

Nonessential cabin equipment

18
Q

Were do the AC Utility Buses receive their power source

A

From their respective AC Bus

19
Q

What indication is there if a Utility Bus has be load shed

A

On the overhead panel, the AC UTILITY switch/light and the AC synoptic page SHED next to the respective Bus

20
Q

The ADG provides power to what

A

The AC ESS Bus and 3B hydraulic pump

21
Q

During Pre-flight of the ADG unit what does the lamp test do

A

Test the lamp

22
Q

During testing of the ADG Unit what must be operational

A

Both AC Gen must be operating and both AC Bus 1/2 must be powered

23
Q

On the ADG Control Panel what does the PWR TXFR Override button do

A

If AC power is restored by one of the Gens or APU this reestablishes normal AC distribution

24
Q

What produces DC power

A

Transformer-rectifier units (TRUs)

25
How many TRUs
4
26
Name the TRUs
TRU 1, TRU 2, ESS TRU 1, ESS TRU 2
27
What powers TRU 1
AC Bus 1
28
What Buses are powered by what TRU
TRU1...DC Bus 1, TRU2... DC Bus 2, ESS TRU2... DC ESS Bus, ESS TRU 1...DC ESS Bus
29
What is the rating of each TRU
100 amps cont
30
If either TRU1 or TRU2 fail can their Buses be powered
Yes, by pressing the MAIN BUS TIE switch light on the over head panel closing the Bus TIE between the Buses.
31
What happens to the Utility Buses when the MAIN BUS TIE is closed
The Utility buses are shed to reduce electrical load
32
Can the UTIL buses be disconnected manually
Yes, by pressing the AC/DC UTILITY switch/light
33
What does the DC ESS BUS power
Equipment essential for safe flight
34
What are the sources of DC power to the DC ESS BUS
ESS TRU 1/2 or APU BAT DIR BUS
35
If the ADG is operating what TRU does it power
ESS TRU 1
36
Can the DC ESS BUS be powered by the APU or Main Batteries
Yes, through the Emergency DC transfer contact
37
What does the BAT MASTER switch do when turned on
Controls the APU and MAIN BATT contacts to supply electrical power to the BATT BUS
38
Why is the BATT BUS important
Powers essential equipment for flight
39
What normally powers the BATT BUS
ESS TRU 1/2
40
If using DC external power source how do you know it is connected
Over head electrical panel light is on (IN USE) and on the synoptic page EXT DC appears