2000 RKAs

Question 1

Which doors does the warning system monitor?

Answer 1

Passenger/crew door, emergency exit, baggage compartment, forward compartment, aft compartment

Question 2

Which test is not located on the Test Synoptic Page?

Answer 2

The Fire Test

Question 3

How is the ELT controlled in flight?

Answer 3

Via the ELT Remote Controls on the right side instrument panel.

Question 4

How is the CVR tested?

Answer 4

By clicking the CVR soft key on the TEST Synoptic and listening for a tone in the headset.

Question 5

How is the passenger DOOR LIFT system operated?

Answer 5

By pressing two push buttons, one located inside the main door and the other on the exterior of the aircraft.

Question 6

How is the passenger/crew door normally operated?

Answer 6

Typically, it is electrically-lifted and manually-lowered.

Question 7

How many power supplies does an MAU have?

Answer 7

Each MAU uses two power supplies.

Question 8

If the right engine fails in the clean configuration in flight, how is the electrical system configured?

Answer 8

When the Essential (ESS) and Median (MD) buses are untied, GEN 1 supplies the Left Hand (LH) bus, BAT 2 supplies the Median (MD) and Right Hand (RH) bus.

Question 9

Maximum continuous generator amperage with one generator inop during flight.

Answer 9

400 amps

Question 10

Normal electrical rating of an external power cart.

Answer 10

28 Volts, 1000 Amps

Question 11

Where does the CVR get its power?

Answer 11

Essential Bus

Question 12

When will the generator witch trip off?

Answer 12

When there is an over voltage or over amperage.

Question 13

What is the electrical configuration when the left engine fails in flight?

Answer 13

Before any corrective action, if the Essential (ESS) and Median (MD) buses are untied, BAT 1 supplies the Left Hand (LH) bus, GEN 2 supplies the Right Hand (RH) bus.

Question 14

What does pushing the MINI LOAD MASTER button do?

Answer 14

MINI LOAD MASTER provides power to the Essential Bus.

Question 15

When do orange colored circuit breakers need to be pulled?

Answer 15

When all generators fail.

Question 16

Which battery supplies power for starting the APU?

Answer 16

Battery 1

Question 17

How long can the Landing light be in operation on the ground?

Answer 17

The landing lights can be on for a maximum of 15 minutes each time with a 45 minute cooling period between use.

Question 18

Where are the dimming controls located for the display units?

Answer 18

On the Reversion Control Panel

Question 19

How should the switch for the emergency lights be positioned during flight?

Answer 19

In the ARM position.

Question 20

How is the emergency lighting powered?

Answer 20

By three independent batteries

Question 21

How can the emergency lights be tested?

Answer 21

By switching the emergency light switch on the overhead panel to ON.

Question 22

How are the Master Warning lights tested?

Answer 22

By pressing the lights soft key on the TEST SYNOPTIC.

Question 23

What does the amber STBY status light mean if the BOOST 2 push button I depressed?

Answer 23

During normal operations with the engines running, if the BOOST 2 push button is depressed, the STBY Amber status light means the normal RH BOOSTER PUMP has stopped, and the stand-by RH booster pump is running. There is no operational impact.

Question 24

What does the white advisory CAS “FUEL LEVEL 1/2” mean?

Answer 24

The fuel tanks have reached 1000lbs.

Question 25

How is the cross feed X-BP valve operation verified?

Answer 25

By monitoring indications on the fuel synoptic page.

Question 26

What happens with the X-BP valve when the Left X-TK pushbutton?

Answer 26

If the X-BP is not open (status light is off) and the Left X-TK pushbutton is pushed, the X-BP opens automatically.

Question 27

What does the Amber CaS message LOW FUEL 1 indicate?

Answer 27

250 lbs remaining in the left feeder tank

Question 28

What is the X-TK button used for?

Answer 28

To transfer fuel from one tank group to the other tank group.