Challenger 350 TPM UPDATED ACTUAL
Exam Questions and CORRECT Answers
When the engines are running at idle power, the danger area of the exhaust is: - CORRECT
ANSWER - 200 ft
The minimum pavement width for a 180° turn is ______ ft with a 5-ft margin for safety -
CORRECT ANSWER - 58 ft
During towing, nosewheel swivel through the range of ________ of each side of
center is possible, without disconnecting the nosewheel steering torque links. - CORRECT
ANSWER - 120 degrees
Landing gear downlock safety pins (gear pins) are provided for the ________ landing
gear assembly and the left and right ________ landing gear assemblies. - CORRECT
ANSWER - Nose
Main
The passenger door is normally closed by ________ power by utilization of the
pushbutton switches located on the exterior and interior of the aircraft. - CORRECT
ANSWER - Electrical
EICAS displays the amber EMERGENCY EXIT indication if the _______________. -
CORRECT ANSWER - Electronic proximity sensors indicate the emergency exit isnt
closed
When the aircraft is on the ground, the cargo door is not closed and fully locked, and
the left engine run switch is in the RUN position, what indication is displayed on the
EICAS? - CORRECT ANSWER - Amber CARGO DOOR CAS
,What doors are monitored by the door warning system? - CORRECT ANSWER -
Passenger door, emergency exit door, cargo bay door, aft equipment door, battery bay door
T/F: The master CAUTION switches are located on the cursor control panel. - CORRECT
ANSWER - False, its on the glare shield
Pressing the CAS switch once on the CCP hides the caution, advisory, and status
messages. When a new message is generated: - CORRECT ANSWER - the message
appears automatically above the white MSGS icon
The engine indication and crew alerting system (EICAS) provides all of the
following EXCEPT:
A. Automatic system monitoring
B. Aural alert warning messages
C. Integration of system information
D. Integration of standby system instrument information - CORRECT ANSWER -D
The crew alerting system (CAS) provides visual and aural alerts when a malfunction
is detected. T/F - CORRECT ANSWER - True
On the synoptic page presentation, a parameter that exceeds the established limits
changes the indicator to what color?
A. Green
B. Blue
C. Cyan
D. Red - CORRECT ANSWER - Red
, Warning messages require immediate action and are accompanied by:
A. Red indication on the EICAS synoptic page
B. Flashing master WARNING lights
C. Triple chime
D. All of the above - CORRECT ANSWER - All of the above
During a total generator failure, the standby battery provides power to the aircraft
essential buses. T/F - CORRECT ANSWER - False: it supplies power to the ISI
The engine driven generators are normally limited to ________ amps - CORRECT
ANSWER - 400 amps
The aircraft electrical panel and electrical synoptic page provide the following information
A. Indication of how many amps the GPU is providing
B. Indication that GPU voltage is acceptable
C. CAS indicating that EXT PWR has been selected ON
D. All of the above - CORRECT ANSWER - B. Indication that GPU voltage is acceptable
When the aircraft is being powered by only the main batteries in flight, the battery duration is 3.5
hr and includes 3 APU start attempts. T/F - CORRECT ANSWER - False, 1hr
Battery voltage can be read on:
A. Voltage indicator
B. EICAS messages
Exam Questions and CORRECT Answers
When the engines are running at idle power, the danger area of the exhaust is: - CORRECT
ANSWER - 200 ft
The minimum pavement width for a 180° turn is ______ ft with a 5-ft margin for safety -
CORRECT ANSWER - 58 ft
During towing, nosewheel swivel through the range of ________ of each side of
center is possible, without disconnecting the nosewheel steering torque links. - CORRECT
ANSWER - 120 degrees
Landing gear downlock safety pins (gear pins) are provided for the ________ landing
gear assembly and the left and right ________ landing gear assemblies. - CORRECT
ANSWER - Nose
Main
The passenger door is normally closed by ________ power by utilization of the
pushbutton switches located on the exterior and interior of the aircraft. - CORRECT
ANSWER - Electrical
EICAS displays the amber EMERGENCY EXIT indication if the _______________. -
CORRECT ANSWER - Electronic proximity sensors indicate the emergency exit isnt
closed
When the aircraft is on the ground, the cargo door is not closed and fully locked, and
the left engine run switch is in the RUN position, what indication is displayed on the
EICAS? - CORRECT ANSWER - Amber CARGO DOOR CAS
,What doors are monitored by the door warning system? - CORRECT ANSWER -
Passenger door, emergency exit door, cargo bay door, aft equipment door, battery bay door
T/F: The master CAUTION switches are located on the cursor control panel. - CORRECT
ANSWER - False, its on the glare shield
Pressing the CAS switch once on the CCP hides the caution, advisory, and status
messages. When a new message is generated: - CORRECT ANSWER - the message
appears automatically above the white MSGS icon
The engine indication and crew alerting system (EICAS) provides all of the
following EXCEPT:
A. Automatic system monitoring
B. Aural alert warning messages
C. Integration of system information
D. Integration of standby system instrument information - CORRECT ANSWER -D
The crew alerting system (CAS) provides visual and aural alerts when a malfunction
is detected. T/F - CORRECT ANSWER - True
On the synoptic page presentation, a parameter that exceeds the established limits
changes the indicator to what color?
A. Green
B. Blue
C. Cyan
D. Red - CORRECT ANSWER - Red
, Warning messages require immediate action and are accompanied by:
A. Red indication on the EICAS synoptic page
B. Flashing master WARNING lights
C. Triple chime
D. All of the above - CORRECT ANSWER - All of the above
During a total generator failure, the standby battery provides power to the aircraft
essential buses. T/F - CORRECT ANSWER - False: it supplies power to the ISI
The engine driven generators are normally limited to ________ amps - CORRECT
ANSWER - 400 amps
The aircraft electrical panel and electrical synoptic page provide the following information
A. Indication of how many amps the GPU is providing
B. Indication that GPU voltage is acceptable
C. CAS indicating that EXT PWR has been selected ON
D. All of the above - CORRECT ANSWER - B. Indication that GPU voltage is acceptable
When the aircraft is being powered by only the main batteries in flight, the battery duration is 3.5
hr and includes 3 APU start attempts. T/F - CORRECT ANSWER - False, 1hr
Battery voltage can be read on:
A. Voltage indicator
B. EICAS messages
