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DFW INSTRUCTORS 300/350 COMPLETE CARD SET QUESTIONS ANSWERED CORRECTLY LATEST UPDATE 2026

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DFW INSTRUCTORS 300/350 COMPLETE CARD SET QUESTIONS ANSWERED CORRECTLY LATEST UPDATE 2026 This deck was created by DFW 300/350 Instructors - Answers What is the maximum ramp weight for the Challenger 350 aircraft? - Answers 40,750 lb (18,484 kg) If the passenger door is open, when does a CAS white PASSENGER DOOR message turn amber? - Answers The left engine run switch is moved from the OFF position to the RUN position. What is the maximum landing weight for a Challenger 350 aircraft? - Answers 34,150 lb (15,490 kg) How many static wicks are installed on the Challenger 350 aircraft? - Answers 26 What is the maximum takeoff weight for the Challenger 350 aircraft? - Answers 40,600 lb (18,416 kg) When the engines are running at idle power, what is the danger area of the exhaust? - Answers 200 ft During towing, nosewheel swivel through the range of ________ of each side of center is possible, without disconnecting the nosewheel steering torque links. - Answers 120° Landing gear downlock safety pins (gear pins) are provided for the ________ landing gear assembly and the left and right ________ landing gear assemblies. - Answers Nose gear, main gear What type of power is normally used by the pushbutton switches on the exterior and interior of the aircraft to close the passenger door? - Answers Left Battery What does the amber EMERGENCY EXIT on the EICAS indicate? - Answers Electronic proximity sensors indicate that the emergency exit is not fully 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? - Answers Amber CARGO DOOR caution CAS What is the minimum flight weight for the Challenger 350 aircraft? - Answers 24,800 lb (11,249 kg) What is the VMO (8000 to 29,475 ft) for the Challenger 350 aircraft? - Answers 320 KIAS What is the maximum zero fuel weight for the Challenger 350 aircraft? - Answers 28,200 lb (12,791 kg) What is the MMO (above 29,475 ft) for the Challenger 300/350 aircraft? - Answers 0.83 MI What is the VMO (up to 8000 ft) for the Challenger 300/350 aircraft? - Answers 300 KIAS What is the VLO RET for the Challenger 300/350 aircraft? - Answers 200 KIAS What is the VLE for the Challenger 300/350 aircraft? - Answers 250 KIAS On the audio control panel, what happens if the EMER/NORM switch is selected to the EMER position? - Answers All audio is routed to the headset, the overhead speaker is deactivated, and the onside COMM is routed directly to the pilot What is the VRA for the Challenger 300/350 aircraft? - Answers 265 KIAS/0.75 MI Can Air Source to Trim Air Only be selected on the ground? - Answers No What happens if the 1/2 button is selected on the display control panel? - Answers The MFD reflects the cross-side radios on the MFD What is the VLO EXT for the Challenger 300/350 aircraft? - Answers 250 KIAS What is the maximum differential pressure on the ground? - Answers 0.1 psi What indicates that the ELT is transmitting? - Answers CAS message ELT ON and external buzzer Which sources provide air for the air-conditioning PACK to operate? - Answers APU, aircraft engines, external ground cart What is the maximum positive differential pressure? - Answers 9.4 psi What indications alert the crew that the emergency locator transmitter (ELT) is transmitting? - Answers CAS message ELT ON and external buzzer What is the maximum negative differential pressure? - Answers -0.5 psi How is a failed NAV radio indicated on the MFD display? - Answers The frequency is indicated in amber instead of green. Where is the outflow valve located? - Answers Front right wing fairing Do audio signals from the aural warning system, TAWS, and TCAS go through the volume control switches of the audio control panel? - Answers No How is the outflow valve actuated? - Answers DC electric motors What is the purpose of the 1/2 button on the display control panel (DCP)? - Answers Enables cross-side radio tuning What computer controls the outflow valve? - Answers IASC To which functions does the Challenger 300/350 MFD COM display provide control capability? - Answers Squelch mode selection, COM test function, frequency tuning What cabin altitude triggers a caution light? - Answers 8500 ft The control display unit is one of two ways to control what? - Answers Communication radios, ATC transponders, ADF receivers, NAV frequencies What cabin altitude triggers a warning light? - Answers 9400 ft Where is the underwater locator device located? - Answers Located on the CVR and FDR How many feet are added to cabin altitude to readjust for a High Alt mode caution light? - Answers 650 ft To what does the CDU provides tuning control? - Answers Both the onside and cross-side radios How many feet are added to cabin altitude to readjust for a High Alt mode warning light? - Answers 1550 ft What indicates that the landing altitude was set automatically? - Answers The landing altitude displays in magenta color Where is the battery voltage indicated? - Answers Electrical and summary synoptic page What is the automatic landing altitude return-to-base criteria? - Answers 6000 or 10 minutes What does the CVR control panel contain? - Answers Headset jack, ERASE button, TEST button/green lamp How many safety valves does the Challenger 300/350 aircraft have? - Answers Two While on the ground, which electrical buses are powered with only the APU online? - Answers All six buses (ESSENTIAL, MAIN, AUX) What is the purpose of the safety valves? - Answers They prevent over and under pressurization of the cabin What is used for anti-icing of the wing leading edge and engine intake cowls? - Answers Engine bleed air What are the limitations for trim air usage? - Answers Do not use trim air on the ground How is the landing altitude normally set? - Answers Automatically by the FMS When power is lost to an engine anti-ice valve, what does the valve do? - Answers The valve fails open How is the landing altitude manually set? - Answers By selecting MAN located on the pressurization panel When does the automatic "Pull up Pull down" function operate? - Answers On the ground with the main cabin door open What does DME compare and decode? - Answers Slant distance to the DME ground station, relative closure rate, time to station Where does the APU obtain fuel for operation? - Answers Right wing collector tank What indicates that the landing altitude was set manually? - Answers The landing altitude displays in cyan color How many IASC computers does the Challenger 300/350 aircraft have? - Answers Two In which mode selection does the Mode S transponder reports neither Mode C nor Mode S? - Answers ALT OFF Where is the cabin zone temperature sensor? - Answers Mid cabin right side How many independent ice detectors/microprocessors are in the ice and rain protection system? - Answers Two What valve divides the left manifold from the right manifold? - Answers XBLEED valve Where is the cockpit zone temperature sensor? - Answers On the left side of the center pedestal next to the pilot's right knee True or false: The bleed valves are pneumatically operated and electrically controlled. - Answers TRUE Where is the CB2 circuit breaker panel located? - Answers Behind the copilot seat What is the guarded EMER DEPRESS PBA for? - Answers For fresh air circulation and if fumes or smoke enter the cockpit While in flight, with all three generators offline, which buses are powered? - Answers ESSENTIAL only For what is high-pressure bleed air used? - Answers Wing anti-ice system What air sources can provide air to the packs? - Answers Engines, APU, ground air cart What is the maximum altitude for APU start? - Answers 30,000 ft MSL (14,000 ft on the ground) Into what manifold does the ground air cart feed? - Answers The right manifold What is the maximum amperage on the GPU? - Answers 1500 amps If the aircraft is down to essential power only, how long will the batteries last? - Answers 1 hr When must the PACK be operating while on the ground? - Answers When the aircraft electrical power is on (BATT or ext power on) for more than 30 minutes with OAT 40°C How long will the standby instrument power the ISI? - Answers 3.5 hrs What is the minimum altitude at which the autopilot may remain engaged during Category 1 ILS operations with glideslope angles between 3.5° and 4.5°? - Answers 160 ft AGL What is the pressurization limitation during takeoff and landing? - Answers 1.0 Under what circumstances should the flight crew attempt to overpower the autopilot? - Answers Never. Do not intentionally overpower the autopilot. While in flight, which electrical buses are powered with only one generator online? - Answers ESSENTIAL and MAIN Does vertical deviation and scale display on the lower part of the PFD? - Answers No What type of air is used for pressurization? - Answers Intermediate air (IP air) What is the minimum battery temperature for takeoff? - Answers Minus 20°C Where is Delta P displayed? - Answers EICAS, Summary page, ECS synoptic page What is the limitation for extraction of bleed air from the APU for engine start and environmental air? - Answers 20,000 ft AGL What is the maximum altitude the aircraft can fly with the yaw damper inoperative? - Answers 31,000 ft What is the maximum amperage for two or three generators? - Answers 400 amps What conditions exist while a pilot is depressing the MSW? - Answers Autopilot disengage, all trims inoperative, stall pusher inoperative (except on EASA aircraft) What is the temperature range in the NORM mode? - Answers 15°C to 35°C True or False: During APU start, the right battery is isolated from the aircraft system and powers the APU starter. - Answers TRUE What is the temperature range in the manual mode? - Answers 10°C to 70°C What is the maximum amperage for one generator while on the ground? - Answers 400 amps What computer controls the anti-ice protection system? - Answers Integrated air system controller (IASC) What is the maximum amperage for one generator while in flight? - Answers 500 amps To what PSI is intermediate pressure regulated? - Answers 50 ±3 Do multifunction displays show synoptic information? - Answers Yes To what PSI is high-pressure bleed air regulated? - Answers 36 ±3 When is the emergency locator transmitter automatically activated? - Answers When excessive longitudinal forces occur What is the transient limit for all generators? - Answers 600 amps for 5 minutes What items in the aircraft are powered by the left and right AUX buses? - Answers Cabin DC and AC power, and the copilot side window and foot warmers What does the PACK provide? - Answers Provides conditioned air for the fuselage compartments Which component controls engine anti-ice functions? - Answers FADEC How is the APU bleed valve controlled? - Answers By the APU ECU What backup information does the ISI supply to the pilot? - Answers Altitude, attitude, airspeed indications What computer monitors the bleed-air leak detection system? - Answers IASC At what speed does the takeoff CAS message inhibit feature activate? - Answers 80 kt How many ozone converters are installed in the Challenger 300/350 aircraft? - Answers Two What does a green AVAIL message on the electrical panel indicate? - Answers GPU is connected and has correct voltage and polarity What is the minimum altitude at which the autopilot may remain engaged during Category 1 precision approach operations? - Answers 80 ft AGL How is rain removal from the windshields accomplished? - Answers Special coating applied to both the windshields and cockpit windows What is the minimum altitude at which the autopilot may remain engaged during nonprecision approach operations? - Answers 200 ft AGL Which buses are powered in flight with a single generator online? - Answers Main and essential Which other generator normally shares the load with the APU generator? - Answers Right side generator At what altitude, or after what duration of time, does the aircraft exit the takeoff CAS message inhibit period? - Answers 400 ft AGL or 60 sec What is the autopilot minimum use height for climb, enroute, or descent? - Answers 700 ft AGL With all three generators operating in flight, if the left generator drops offline, what automatically happens? - Answers The APU generator automatically switches to the left side and powers the buses True or False: Both flight guidance computers must be operational for the autopilot to function. - Answers TRUE What does a cyan ICE DETECTED (A) EICAS message indicate? - Answers Ice is detected, and all of the anti-ice systems are turned on True or False: The autopilot will operate normally in secondary trim. - Answers FALSE What happens when the ENG FIRE switch is pressed? - Answers Fuel SOV closes, IP and HP bleed-air SOVs close, hydraulic SOVs close, generator is selected offline, FADEC commands engine shutdown, both fire bottles arm to the respective engine On a glidepath angle of 3.5° or less, what is the lowest altitude that the autopilot may be used? - Answers 80 ft AGL Why is the right battery turned on first? - Answers To prevent uncommanded APU start At what altitude will the half bank mode automatically engage? - Answers 31,600 ft How many and how much time must elapse between APU start attempts? - Answers Three APU start attempts: 1 minute cooling between, followed by 20 minutes cooling before maximum of two more attempts How many circuit breaker panels are installed on the Challenger 300/350 aircraft? - Answers Seven When does the CAS provide visual and aural alerts? - Answers When a red or amber CAS malfunction is detected What is the main function of the AFCS? - Answers Flight guidance What is the maximum altitude that the APU GEN can be used? - Answers 30,000 ft Why do the flight directors display flight guidance cues on the attitude indicators? - Answers To assist the flight crew in maintaining a specified flight path Is another start attempt permitted after an unsuccessful APU start attempt in the air? - Answers No. Do not attempt another start until after landing. The crew can choose to hand fly the aircraft using "raw data" (flight directors not displayed), hand fly the aircraft using the flight director command bars, or _______. - Answers Couple the autopilot to the flight director How many dual temperature sensors are in each wing in the wing and anti-ice system? - Answers Two What causes the FD command bars to appear on both PFDs? - Answers Any flight director mode selection At what oil temperature range may engines be operated from idle up to but not including CLB power? - Answers Between 5° and 14°C What mode does the FD automatically defaults to when NAV mode is being used and the navigation source is lost? - Answers Basic ROLL mode What is heated using electrical DC power? - Answers Windshields, windows, T2 probes, air data probes, AOA vanes Can the pilot override the yaw damper command? - Answers No What accompanies warning messages, indicating

Content preview

DFW INSTRUCTORS 300/350 COMPLETE CARD SET QUESTIONS
ANSWERED CORRECTLY LATEST UPDATE 2026


This deck was created by DFW 300/350 Instructors - Answers
What is the maximum ramp weight for the Challenger 350 aircraft? - Answers 40,750
lb (18,484 kg)
If the passenger door is open, when
does a CAS white PASSENGER DOOR
message turn amber? - Answers The left engine run switch
is moved from the OFF position
to the RUN position.
What is the maximum landing weight for a Challenger 350 aircraft? - Answers
34,150 lb (15,490 kg)
How many static wicks are installed on the Challenger 350 aircraft? - Answers 26
What is the maximum takeoff weight for the Challenger 350 aircraft? - Answers
40,600 lb (18,416 kg)
When the engines are running
at idle power, what is the
danger area of the exhaust? - Answers 200 ft
During towing, nosewheel swivel through the range of ________ of each side of
center is possible, without disconnecting the nosewheel steering torque links. -
Answers 120°
Landing gear downlock safety pins
(gear pins) are provided for the
________ landing gear assembly and
the left and right ________ landing
gear assemblies. - Answers Nose gear, main gear
What type of power is normally used
by the pushbutton switches on the
exterior and interior of the aircraft
to close the passenger door? - Answers Left Battery
What does the
amber EMERGENCY EXIT
on the EICAS indicate? - Answers Electronic proximity sensors
indicate that the emergency exit
is not fully 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? - Answers Amber CARGO DOOR caution CAS
What is the minimum flight weight for the Challenger 350 aircraft? - Answers 24,800
lb (11,249 kg)
What is the VMO (8000 to 29,475 ft) for the Challenger 350 aircraft? - Answers 320
KIAS
What is the maximum zero fuel weight for the Challenger 350 aircraft? - Answers
28,200 lb (12,791 kg)
What is the MMO (above 29,475 ft) for the Challenger 300/350 aircraft? - Answers
0.83 MI
What is the VMO (up to 8000 ft) for the Challenger 300/350 aircraft? - Answers 300
KIAS

,What is the VLO RET for the Challenger 300/350 aircraft? - Answers 200 KIAS
What is the VLE for
the Challenger 300/350 aircraft? - Answers 250 KIAS
On the audio control panel, what happens if the EMER/NORM switch is selected to
the EMER position? - Answers All audio is routed to the headset, the overhead
speaker is deactivated,
and the onside COMM is routed
directly to the pilot
What is the VRA for
the Challenger 300/350 aircraft? - Answers 265 KIAS/0.75 MI
Can Air Source to Trim Air Only
be selected on the ground? - Answers No
What happens if the 1/2 button is selected on the display control panel? - Answers
The MFD reflects the cross-side radios on the MFD
What is the VLO EXT for the Challenger 300/350 aircraft? - Answers 250 KIAS
What is the maximum differential pressure on the ground? - Answers 0.1 psi
What indicates that the ELT is transmitting? - Answers CAS message ELT ON and
external buzzer
Which sources provide air for the
air-conditioning PACK to operate? - Answers APU, aircraft engines,
external ground cart
What is the maximum positive differential pressure? - Answers 9.4 psi
What indications alert the crew that the emergency locator transmitter (ELT) is
transmitting? - Answers CAS message ELT ON
and external buzzer
What is the maximum negative differential pressure? - Answers -0.5 psi
How is a failed NAV radio indicated on the MFD display? - Answers The frequency
is indicated in amber instead of green.
Where is the outflow valve located? - Answers Front right wing fairing
Do audio signals from the aural
warning system, TAWS, and TCAS
go through the volume control switches
of the audio control panel? - Answers No
How is the outflow valve actuated? - Answers DC electric motors
What is the purpose of the 1/2 button on the display control panel (DCP)? - Answers
Enables cross-side radio tuning
What computer controls
the outflow valve? - Answers IASC
To which functions does the
Challenger 300/350 MFD COM display
provide control capability? - Answers Squelch mode selection, COM test function,
frequency tuning
What cabin altitude triggers
a caution light? - Answers 8500 ft
The control display unit is one
of two ways to control what? - Answers Communication radios,
ATC transponders, ADF receivers,
NAV frequencies
What cabin altitude triggers
a warning light? - Answers 9400 ft

, Where is the underwater
locator device located? - Answers Located on the CVR and FDR
How many feet are added to cabin altitude to readjust for a High Alt
mode caution light? - Answers 650 ft
To what does the CDU
provides tuning control? - Answers Both the onside and cross-side radios
How many feet are added to cabin altitude to readjust for a High Alt
mode warning light? - Answers 1550 ft
What indicates that the landing altitude was set automatically? - Answers The
landing altitude displays in magenta color
Where is the battery voltage indicated? - Answers Electrical and summary synoptic
page
What is the automatic landing altitude return-to-base criteria? - Answers 6000 or 10
minutes
What does the CVR
control panel contain? - Answers Headset jack, ERASE button,
TEST button/green lamp
How many safety valves does the Challenger 300/350 aircraft have? - Answers Two
While on the ground, which
electrical buses are powered with
only the APU online? - Answers All six buses
(ESSENTIAL, MAIN, AUX)
What is the purpose
of the safety valves? - Answers They prevent over and under pressurization of the
cabin
What is used for anti-icing of the wing leading edge and engine intake cowls? -
Answers Engine bleed air
What are the limitations
for trim air usage? - Answers Do not use trim air on the ground
How is the landing altitude
normally set? - Answers Automatically by the FMS
When power is lost to an engine
anti-ice valve, what does the valve do? - Answers The valve fails open
How is the landing altitude
manually set? - Answers By selecting MAN located on the pressurization panel
When does the automatic
"Pull up Pull down" function operate? - Answers On the ground with
the main cabin door open
What does DME compare
and decode? - Answers Slant distance to the DME ground station, relative closure
rate,
time to station
Where does the APU
obtain fuel for operation? - Answers Right wing collector tank
What indicates that the landing altitude was set manually? - Answers The landing
altitude displays
in cyan color
How many IASC computers does the Challenger 300/350 aircraft have? - Answers
Two
In which mode selection does

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