Systems CBT Flashcards
(100 cards)
(1) What actions trip the autopilot?
All answers are correct. (a) The manual trim or quick disc switches activated, column shakers are activated, (b) A column and control wheel force monitor sensor trips, & (c) The fly-by-wire system in direct mode, aileron and elevator system disconnects.
(2) Which system provides information and alerting to detect a potentially hazardous terrain situation in order to prevent CFIT?
EGPWS
(3) With the Ice Detection Mode Selector knob set to ON, when will the engine anti ice systems operate?
Whenever the engines are running
(4) Which flight controls does Hydraulic System 3 power?
Rudder, right elevator and both ailerons
(5) What is the max thrust of one engine?
14,200 lbs
(6) How many igniters are energized for each engine start?
One on the ground and two in flight
(7) Which electric hydraulic pumps are automatically switched on for takeoff and landing?
System 1 and 2
(8) The emergency ram air valve is commanded open:
If Pack1 and Pack2 are commanded⁄failed OFF, and the altitude is less than 25,000 ft
(9) Where is the crew oxygen pressure indication?
On the status synoptic page on MFD
(10) What color are EICAS status messages displayed in?
White
(11) How many service doors provide access for service access?
2
(12) During normal operation, air data readouts on the Captains PDF are from which ADS?
ADS 1
(13) TCF (terrain clearance floor) function is based on airplane present position, radio altitude, and:
Glideslope deviation distance to the nearest runway on database
(14) What is the maximum altitude for conditioning air operation from the APU?
15,000 ft
(15) The cabin zone temperature control:
Can be transferred from a cockpit control panel to the flight attendant control panel
(16) Above what cabin altitude will the NO SMOKING and FASTEN SEAT BELT signs automatically illuminate?
14,000 ft
(17) Pushing the test button on the fire extinguisher panel in the cockpit will:
Test the engine- and APU-fire detection system, as well as the cargo smoke detection system
(18) The STBY AC BUS is normally powered by the ESS AC BUS. It will be powered by the inverter:
When the aircraft is powered by batteries only
(19) What does pressing the back up trim switch while the autopilot is engaged do?
The autopilot disconnects
(20) In the event of a failure in the PSEM electronics, the landing gear should be extended by means of:
The electrical override switch
(21) In case of a single electric motor failure within the flap PDU, how will the system operate?
The flap⁄slat system will operate at low rate speed
(22) How long is the wingspan of the aircraft?
26 m or 85 ft 4 in
(23) The Air Data System comprises which components?
4 ADSPs, 2 TAT probes, 3 ADAs and the Baro Set on the GP
(24) When are the ADSP and TAT probe heaters powered?
Whenever the engines are running