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Challenger 350 TPM Questions and Answers

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Challenger 350 TPM Questions and Answers

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  • September 7, 2024
  • 17
  • 2024/2025
  • Exam (elaborations)
  • Questions & answers
  • Challenger 350 TPM
  • Challenger 350 TPM
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CHALLENGER 350 TPM QUESTIONS
AND 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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