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Challenger 350 TPM Questions and Answers
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Challenger 350 TPM Questions and Answers
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CHALLENGER 350 TPM QUESTIONSAND ANSWERS GRADED A+
s When the engines are running at idle power, the danger area of the exhaust is: - 200 ft
The minimum pavement width for a 180° turn is ______ ft with a 5-ft margin for safety - 58 ft
During towing, nosewheel swivel through the range of ________ of each side of
center is possible, without disconnecting the nosewheel steering torque links. - 120 degrees
Landing gear downlock safety pins (gear pins) are provided for the ________ landing
gear assembly and the left and right ________ landing gear assemblies. - 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. - Electrical
EICAS displays the amber EMERGENCY EXIT indication if the _______________. - 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? - Amber CARGO DOOR CAS
What doors are monitored by the door warning system? - 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. - 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: - 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 - D
The crew alerting system (CAS) provides visual and aural alerts when a malfunction
is detected. T/F - 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 - 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 - All of the above
During a total generator failure, the standby battery provides power to the aircraft
essential buses. T/F - False: it supplies power to the ISI
The engine driven generators are normally limited to ________ amps - 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 - 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 - False, 1hr
Battery voltage can be read on:
, A. Voltage indicator
B. EICAS messages
C. Electrical control panel
D. Electrical synoptic page - D. Electrical synoptic page
The temperature for each battery is displayed on the EICAS. T/F - True
Which of the following is not provided on the electrical synoptic page?
A. Left and right generator temperature
B. Left and right generator voltage
C. Left and right battery voltage
D. All of the above - A. Left and right generator temperature
When the batteries are connected to their corresponding buses in parallel with the
generators, they are charged by the generators. T/F - True
The electronic flight instrument system consists of four adaptive flight displays. T/F - True
Which of the following are displayed as airspeed information on the PFD?
A. Reference speeds
B. Mach number display
C. Low/high/speed cues
D. All of the above - D. All of the above
Primary flight displays are integrated displays of attitude, air data, and navigation information. T/F - True
DME hold can be executed by:
A. Pressing the center of the MENU DATA knob on the DCP
B. CDU via the TUNE page
C. Pressing the DME knob on the audio control panel
D. None of the above - B. CDU via the TUNE page
Navigation data displayed on the lower part of the PFD includes all of the following EXCEPT:
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