2000 RKAs Flashcards
Which doors does the warning system monitor?
Passenger/crew door, emergency exit, baggage compartment, forward compartment, aft compartment
Which test is not located on the Test Synoptic Page?
The Fire Test
How is the ELT controlled in flight?
Via the ELT Remote Controls on the right side instrument panel.
How is the CVR tested?
By clicking the CVR soft key on the TEST Synoptic and listening for a tone in the headset.
How is the passenger DOOR LIFT system operated?
By pressing two push buttons, one located inside the main door and the other on the exterior of the aircraft.
How is the passenger/crew door normally operated?
Typically, it is electrically-lifted and manually-lowered.
How many power supplies does an MAU have?
Each MAU uses two power supplies.
If the right engine fails in the clean configuration in flight, how is the electrical system configured?
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.
Maximum continuous generator amperage with one generator inop during flight.
400 amps
Normal electrical rating of an external power cart.
28 Volts, 1000 Amps
Where does the CVR get its power?
Essential Bus
When will the generator witch trip off?
When there is an over voltage or over amperage.
What is the electrical configuration when the left engine fails in flight?
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.
What does pushing the MINI LOAD MASTER button do?
MINI LOAD MASTER provides power to the Essential Bus.
When do orange colored circuit breakers need to be pulled?
When all generators fail.
Which battery supplies power for starting the APU?
Battery 1
How long can the Landing light be in operation on the ground?
The landing lights can be on for a maximum of 15 minutes each time with a 45 minute cooling period between use.
Where are the dimming controls located for the display units?
On the Reversion Control Panel
How should the switch for the emergency lights be positioned during flight?
In the ARM position.
How is the emergency lighting powered?
By three independent batteries
How can the emergency lights be tested?
By switching the emergency light switch on the overhead panel to ON.
How are the Master Warning lights tested?
By pressing the lights soft key on the TEST SYNOPTIC.
What does the amber STBY status light mean if the BOOST 2 push button I depressed?
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.
What does the white advisory CAS “FUEL LEVEL 1/2” mean?
The fuel tanks have reached 1000lbs.
How is the cross feed X-BP valve operation verified?
By monitoring indications on the fuel synoptic page.
What happens with the X-BP valve when the Left X-TK pushbutton?
If the X-BP is not open (status light is off) and the Left X-TK pushbutton is pushed, the X-BP opens automatically.
What does the Amber CaS message LOW FUEL 1 indicate?
250 lbs remaining in the left feeder tank
What is the X-TK button used for?
To transfer fuel from one tank group to the other tank group.
