Browse all practice questions for the DFW Instructors 300/350 Practice Test. Search by topic, open any question and review its full explanation, then test yourself in the practice quiz.

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Challenger 300/350's IASC Configuration: Why Two Is Better Than OneHow many IASC computers does the Challenger 300/350 aircraft have?Discover How Special Coatings Improve Rain Removal from WindshieldsHow is rain removal from the windshields accomplished?Discover the Essential Role of APU in Aircraft OperationsHow does the APU assist in aircraft functionality during flight?Discover the Essential Role of the Fuel Heater/Oil Cooler in Engine SystemsWhere is oil filtered and cooled in the engine system?Discover Why Carbon Brakes Are Essential for the Challenger 300/350What type of brakes does the Challenger 300/350 aircraft use?Exploring the Role of Fuel Pumps in Aircraft EfficiencyHow many fuel pumps are typically installed in this aircraft?Fire Extinguishers and Their Role in Aircraft Safety: What You Need to KnowCan both fire extinguisher containers be discharged into the APU when required?How Fuel is Heated in Challenger 300/350 AircraftHow is fuel heated in the Challenger 300/350 aircraft?How Long to Wait Before Discharging a Fire Bottle After Engine Shutdown?How long should elapse before discharging the first fire bottle after engine shutdown if the fire warning persists?How Multifunction Displays Revolutionize Data VisualizationDo multifunction displays show synoptic information?How TCAS Displays Climb and Descent Rates Matters to PilotsAn up or down arrow on the TCAS page appears when a target aircraft is climbing or descending at what rate?How the Crew Alerting System Alerts Pilots to MalfunctionsWhen does the CAS provide visual and aural alerts?Let’s Talk Flight Spoilers: The Role of SECU 2 in Your TrainingWhich flight computer is responsible for controlling the outboard flight spoilers?Navigating Cold Weather Operations: The Essential Manual for PilotsWhich manual contains comprehensive procedures for operating in cold weather?Possible indications of ELT transmission in aviationWhich of the following is a possible indication of ELT transmission?Strategies for Safe Ground Spoiler Deployment During LandingWhat conditions must be met for ground spoiler deployment?Understanding Aircraft Hydraulic Systems: The Role of Multifunctional SpoilersAre all multifunctional spoilers operative after a right hydraulic system failure?Understanding Aircraft Nosewheel Steering: The Role of the Steering TillerWhich component provides nosewheel steering in an aircraft?Understanding Aircraft Power Sources for Passenger Door OperationsWhat type of power is normally used to operate the pushbutton switches for closing the passenger door?Understanding Aircraft Tire Speed Limits: Why 182 Knots MattersWhat is the maximum tire speed for aircraft operations?Understanding Altitudes in Category 1 Precision Approach OperationsWhat is the minimum altitude at which the autopilot may remain engaged during Category 1 precision approach operations?Understanding Amber ICE DETECT CAS Messages: A Key to Safer FlightsWhat does an amber ICE DETECT CAS message indicate?Understanding APU Generator Functionality During Generator FailuresWhat happens if the left generator drops offline while all three generators are operating in flight?Understanding APU Generator Limitations: What You Need to KnowWhat is the maximum altitude for APU generator use?Understanding APU Operations and Altitude Limits for Bleed AirWhat is the maximum altitude at which the APU can provide bleed air?Understanding APU Start and Battery Isolation in AviationIs the statement true or false: During APU start, the right battery is isolated from the aircraft system and powers the APU starter?Understanding APU Start Cooling Times for Ground OperationsWhat are the cooling time limitations for APU starts on the ground?Understanding Autopilot Usage During Glidepath ApproachesWhat is the minimum altitude the autopilot may be used during a glidepath angle of 3.5° or less?Understanding Battery Temperature Guidelines for Safe Takeoff ProceduresWhat does a minimum battery temperature of -20°C signify for takeoff procedures?Understanding Brake Cooling Times: A Crucial Pre-Takeoff CheckWhat must be calculated regarding wheel brakes before takeoff following a rejected takeoff?Understanding Cabin Lighting Control: The Role of the Main Entryway PanelWhich of the following is the primary method for cabin light control?Understanding CDU Tuning Control and Its Role in AviationWhat does the CDU provide tuning control for?Understanding Differential Pressure: Why 0.1 psi is CrucialWhat is the maximum differential pressure on the ground?Understanding EICAS Alerts: What That Amber Square Means for Your Gear PositionWhat does an amber square with amber diagonal lines on the EICAS indicate regarding gear position?Understanding Electrical Power Sources in Aircraft SystemsWhich electrical source provides power to the right DCMP?Understanding Emergency Light Power Duration: What You Need to KnowWhat is the approximate power duration provided by the emergency lights?Understanding Emergency Lights in Aviation: What Happens When Power Fails?Do emergency lights automatically illuminate when the right main bus loses electrical power?Understanding Engine Anti-Ice Valve Behavior During Power LossWhen power is lost to the engine anti-ice valve, what position does the valve assume?Understanding FADEC and Engine Anti-Ice FunctionsWhich component is responsible for controlling engine anti-ice functions?Understanding Fire Extinguisher Use for APU FiresWhich fire extinguisher bottle is designated for use in APU fire situations?Understanding Flight Director Command Bars on PFDs: What You Need to KnowWhat causes the flight director command bars to appear on both Primary Flight Displays (PFDs)?Understanding Flight Spoiler Control Systems for Aspiring PilotsWhich flight computer controls inboard flight spoilers?Understanding Generator Load Sharing in Aircraft: A Closer LookWhich generator typically shares the load with the APU generator?Understanding GPS Integration in Aviation SystemsWhich systems receive information from the GPS?Understanding How the APU Bleed Valve is ControlledHow is the APU bleed valve controlled?Understanding How to Select a Pump for Fuel TransferWhat action must be performed to select a pump for fuel transfer?Understanding Hydraulic System Pressure: What You Need to KnowIn what condition is the hydraulic system's pressure not adequate?Understanding Ice Detection on the Challenger 300/350 AircraftHow many ice detectors are installed on the Challenger 300/350 aircraft?Understanding Left Engine Fire Indications in AircraftWhat indications illuminate with a left engine fire?Understanding MACH HOLD Adjustments for Optimal Flight PerformanceWhen will MACH HOLD adjust N1 within a ±3% of thrust lever position?Understanding Maximum Gear Retraction Speed in AviationWhat is the maximum landing gear retraction speed?Understanding N1 Monitoring with Nacelle Heat OnMust the minimum N1 be monitored with nacelle heat ON?Understanding Nosewheel Steering Authority in AircraftHow much nosewheel steering authority does the pilot have through the rudder pedals?Understanding Oxygen Bottle Gauges for Aviation and Medical UsesWhen oxygen bottles are full, what does the gauge next to the outside filler port indicate?Understanding Oxygen System Storage Procedures for AircraftWith temperatures at or below what value should oxygen system recommended storage procedures be followed if the aircraft is parked for an extended period?Understanding Pressurization Limitations During Takeoff and LandingWhat is the pressurization limitation during takeoff and landing?Understanding PRI and SEC Trim in Aviation: Why They Don’t Travel at the Same RateDo PRI and SEC trim travel at the same rate?Understanding Reduced Oxygen Pressure in Passenger MasksWhich passengers receive a reduced rate of oxygen pressure?Understanding Routine SRSL Callouts During ApproachWhat are routine SRSL callouts during approach?Understanding Selectable Flap Positions for AircraftWhat are the selectable flap positions for the aircraft?Understanding Smart Landing Function Alerts for PilotsWhat type of messages does the Smart Landing (SL) function generate during approach and landing?Understanding Spoiler Functionality in Aircraft After Hydraulic FailureHow many multifunctional spoilers are operational after a hydraulic failure?Understanding System Initialization Data for Inertial Reference UnitsWhich sources provide system initialization data for each IRU unit?Understanding the APR Function in Aviation and its ImportanceWhat does the APR function stand for in aviation?Understanding the APU Bleed Valve and Its Role in Aircraft OperationsThe APU bleed valve controls airflow to the aircraft bleed-air system and protects the APU from what condition?Understanding the APU's Role in Aircraft Anti-Ice ApplicationsCan the APU be used to heat the aircraft during anti-ice application?Understanding the Bulk Fuel Temperature Limitation for Jet A TakeoffAt what bulk fuel temperature is takeoff prohibited for Jet A?Understanding the Conditions for Wing Anti-Ice Usage During FlightWhat temperature and moisture conditions must be met for the use of wing anti-ice in flight?Understanding the Critical 5% in Thrust Lever SynchronizationWith thrust levers in CRZ or CLB, the engines will sync to N1 or N2 when they are within _______.Understanding the Critical Locations of Fire Extinguishers on AircraftWhere can fire extinguishers typically be found on the aircraft?Understanding the Critical Role of Emergency Brakes in Hydraulic SystemsWhat role do the emergency brakes serve in the hydraulic system?Understanding the Critical Role of Gear and Hydraulic Motor-Driven Generators in Aircraft SystemsWhich hydraulic system component is critical for gear operation?Understanding the Danger Area of Exhaust During Aircraft Idle PowerWhat is the danger area of the exhaust when the engines are running at idle power?Understanding the Differences Between AUTO and DEPLOY Positions in Oxygen SystemsWhat distinguishes the AUTO position from the DEPLOY position in the oxygen system?Understanding the EICAS System: What It Reveals About Aircraft PerformanceWhat does the EICAS system provide information about?Understanding the EMER Mode: Key Limitations for Flight SpoilersWhat is a key limitation of using EMER mode for flight spoilers?Understanding the Fuel Capacity of the Challenger 300/350What is the fuel capacity with gravity refueling for the Challenger 300/350?Understanding the Fuel Tank System of the Challenger 300/350 AircraftHow many fuel tanks are there in the Challenger 300/350 aircraft?Understanding the Impact of Airspeed on Rudder Travel LimitsThe rudder travel limit constraints depend on which factor?Understanding the Importance of Dual Flight Management Systems in AviationHow many FMSs must be available to utilize performance speeds?Understanding the Importance of Parking Brake Functionality and Fluid ManagementWhat actions should be taken to prevent hydraulic fluid migration while setting the parking brake?Understanding the Importance of Static Wicks on AircraftWhat is the significance of the static wicks on the aircraft surface?Understanding the Importance of the Configuration Deviation List in AviationWhen the main landing gear door is missing, which document provides guidance on remarks or exemptions that must be followed?Understanding the Importance of the FCOM in Aircraft OperationsWhich manual contains information on de-icing fluid?Understanding the Importance of Trim Settings for V2 SpeedWhat result does the calculated trim setting achieve?Understanding the Indicators of SLD Icing Conditions in AviationWhat indicates SLD icing conditions?Understanding the Integrated Air System Controller and Its Role in Anti-Ice ProtectionWhich system is primarily responsible for providing anti-ice protection?Understanding the Jet Pump: No Moving Parts, No Problem!How many moving parts are present in a jet pump?Understanding the Key Components of the CVR Control PanelWhat components are included in the CVR control panel?Understanding the Key Functions of the Auxiliary Power Unit in AircraftWhat is one function of the APU in an aircraft?Understanding the Location of the Cockpit Zone Temperature SensorWhere is the cockpit zone temperature sensor situated?Understanding the Maximum Certified Operating Altitude for the APUWhat is the maximum certified operating altitude for the APU?Understanding the Maximum Landing Weight of the Challenger 350What weight threshold is crucial for the maximum landing weight of the Challenger 350?Understanding the Maximum Negative Pressure During DefuelingWhat is the maximum negative pressure allowed when defueling?Understanding the Maximum Operational Altitude for FMSWhat is the maximum operational altitude for FMS according to the guidelines?Understanding the Maximum Ramp Weight for the Challenger 350 AircraftWhat is the maximum ramp weight for the Challenger 350 aircraft?Understanding the Minimum Altitude for Autopilot Engagement in Category 1 ILSWhat is the minimum altitude for autopilot engagement during Category 1 ILS operations with glideslope angles of 3.5° to 4.5°?Understanding the Minimum Height for Autopilot Use During FlightWhat is the autopilot minimum use height for climb, enroute, or descent?Understanding the Operation of Engine Fire Detection SystemsHow does the engine fire detection system operate?Understanding the Primary Function of the Automatic Flight Control SystemWhat is the primary function of the AFCS?Understanding the Role of Antiskid Systems and Parking Brakes in AircraftIs antiskid operational when using the park/emergency brake?Understanding the Role of APU in Aircraft Engine Start-UpWhat is the primary purpose of the APU regarding engine start?Understanding the Role of APU in Starting Aircraft EnginesWhat additional function does the APU provide besides operating the gearbox-mounted generator and supplying bleed air?Understanding the Role of Elevators in Aircraft Pitch ControlWhich flight control is responsible for changing the aircraft's pitch?Understanding the Role of Engine Bleed Air in Aircraft Anti-IcingWhich method is used for anti-icing of the wing leading edge and engine intake cowls?Understanding the Role of FADEC in Challenger 300/350 AircraftWhich component is responsible for controlling engine power levels in the Challenger 300/350?Understanding the Role of High-Pressure Bleed Air in AircraftWhat is high-pressure bleed air primarily used for in aircraft?Understanding the Role of Inertial Reference Systems in Fuel ReadingsWhich unit provides an accurate fuel reading when the aircraft is not in level flight?Understanding the Role of Multifunction Spoilers in Flight DynamicsWhat is the primary function of the multifunction spoilers during flight?Understanding the Role of PACK in Aircraft: Why It MattersWhat is the primary function of the PACK in an aircraft?Understanding the Role of PMA in Engine Performance: Why 45% N2 MattersThe permanent magnet alternator (PMA) provides power to the FADEC at and above which percentage of N2?Understanding the Role of Safety Valves in the Challenger 300/350How many safety valves does the Challenger 300/350 aircraft have?Understanding the Role of Scavenge Ejectors in Fuel SystemsWhat assists the collector tanks in maintaining a full level of fuel?Understanding the Role of Static Wicks on the Challenger 350 AircraftWhat is the primary function of static wicks on the Challenger 350 aircraft?Understanding the Role of the AUX Hydraulic Pump in Challenger 300 AircraftWhat is the primary function of the AUX hydraulic pump in the Challenger 300 aircraft?Understanding the Role of the Electropneumatic Actuating Valve in Aircraft Oxygen SystemsWhat is the purpose of the electropneumatic actuating valve in the oxygen system?Understanding the Role of the Hydraulic System in Landing Gear OperationsWhich hydraulic system normally extends and retracts the landing gear?Understanding the Role of the Nosewheel Steering ActuatorWhich hydraulic component assists with nosewheel steering?Understanding the Temperature Range in Manual ModeWhat is the temperature range in manual mode?Understanding the Temperature Range in NORM ModeWhat is the temperature range in the NORM mode?Understanding the Thrust Characteristics of the Challenger 300's Auxiliary Power UnitWhat percentage of thrust does the APR provide compared to maximum thrust at ISA+20°C on the Challenger 300?Understanding the Vertical Deviation on Your Primary Flight DisplayDoes vertical deviation and scale display on the lower part of the PFD?Understanding the When and How of Wing Anti-Ice ControlWhen can wing anti-ice be used without restrictions related to temperature?Understanding the Yaw Damper System: The 5-Degree RuleHow many degrees of rudder deflection is the yaw damper system mechanically limited to?Understanding VLE for Challenger 300/350 Aircraft: A Pilot's GuideWhat is the VLE for the Challenger 300/350 aircraft?Understanding VLO RET Speed for Aircraft PerformanceWhat is the VLO RET speed for the aircraft?Understanding Vmcg Speed: Why 115 KIAS Matters for Flaps 10What is the Vmcg speed for flaps 10?Understanding Warning Messages: Why Audio and Visual Indicators MatterWhat accompanies warning messages indicating immediate action is required?Understanding What Triggers the Auxiliary Hydraulic System in AircraftWhat triggers the auxiliary hydraulic system to power the lower rudder PCU?Understanding When the DC Fuel Pump Activates in FlightIn flight, when does the DC fuel pump come on automatically?Understanding When to Activate the Engine Anti-Ice System in FlightWhat condition necessitates turning the engine anti-ice system ON in flight?Understanding When to Take a Generator Offline in AviationIn what scenario would the generator be selected offline?Understanding When to Use the Wing Anti-Ice System in FlightWhen is the wing anti-ice system not needed in flight?Understanding When Yaw Damping is Disabled: Key Airspeeds for PilotsAt what airspeed is the yaw damping function disabled until the aircraft's weight is off the wheels?Understanding Where Delta P is Displayed in Aviation SystemsWhere is Delta P displayed?Using the APU during Anti-Icing and De-Icing: What You Need to KnowCan the APU be used during anti-icing/deicing procedures?What Does Magenta Mean in Aviation? A Quick Guide for Future PilotsWhat denotes that the landing altitude was set automatically?What Happens When Navigation Fails? Understanding BASIC ROLL ModeWhat mode does the flight director automatically default to when NAV mode is used and the navigation source is lost?What Happens When You Press the CAS Switch on the CCP?What occurs when the CAS switch is pressed once on the CCP?What Happens When You Pull the Roll Disconnect on the Left Yoke?Which flight control does the left yoke operate when pulling the roll disconnect?What Makes Up the Inertial Reference Unit?What components are contained within each IRU to measure inertial motion?What to Do if the Autopilot Fails: A Pilot's GuideWhat should be done if the autopilot fails?What to Do When a Fire Extinguisher is Discharged in the Flight CompartmentWhat must the crew do if a fire extinguisher is discharged in the flight compartment?What to Know About Discharging the APU Fire Suppression BottleWhich bottle should be discharged to the APU when performing the fire emergency procedure?What You Need to Know About APU Monitoring: Fuel, Electrical, and ECSWhich components are monitored by the synoptic pages for the APU system and services?What You Need to Know About Flap Extension AltitudeWhat is the maximum altitude at which the flaps can be extended?What You Need to Know About Generator AmperageWhat is the maximum amperage for two or three generators?What You Need to Know About Hydraulic Pumps in DFW Instructors 300/350 SystemsHow many hydraulic pumps are typically installed in the system described?What You Need to Know About Smart Landing Functions During ApproachesWhat does the Smart Landing (SL) function monitor during an approach?What You Need to Know About the Challenger 350's Typical Cruise SpeedWhat is the typical cruise speed for the Challenger 350 aircraft?Where Does the FADEC Get Its Power During Startup and Shutdown?From where does the FADEC obtain power during startup and shutdown?Where to Find Oxygen Duration Tables for Flight SafetyWhere can you find oxygen duration tables?Which Systems Use Electrical DC Power for Heating in Aircraft?What systems are heated using electrical DC power?Why Accumulators Matter in Challenger 300/350 Hydraulic SystemsAre normal brakes operational during a left and right hydraulic failure in the Challenger 300/350?Why Engine Oil Temperature Matters for Optimal PerformanceWhat is the minimum oil temperature required to operate the engines above ground idle?Why Monitoring Engine Performance Parameters is Crucial for Flight SafetyDuring normal operations, what should be monitored regularly to ensure safety?Why the Main Landing Gear's Downlock Safety Pin is Crucial for Aircraft SafetyWhich component's safety mechanism involves a downlock safety pin?Why Two Ice Detectors Are Better for Aircraft SafetyHow many independent ice detectors/microprocessors are in the ice and rain protection system?Why You Shouldn’t Use Trim Air on the Ground, SeriouslyWhat is a key limitation regarding the use of trim air?
More practice questions

These questions are part of the practice quiz. Start practicing

  • What does the EFIS consist of?
  • Can the pilot override the yaw damper command?
  • At what cabin altitude will the electropneumatic actuating valve deploy passenger masks in AUTO?
  • Which flight control surface(s) are locked with the gust lock?
  • Where is the outflow valve located?
  • Which selectable modes can be found in the ATC radio submenu?
  • To what altitude are crew oxygen masks certified for use?
  • In which mode is the mode S transponder unable to send replies?
  • How does the APU contribute to aircraft operations?
  • At what cabin altitude will the crew oxygen masks automatically deliver 100% oxygen under pressure?
  • Which areas of the Challenger 300/350 aircraft are monitored with fire detection?
  • Can the Challenger 300/350 aircraft take off or land from a gravel runway?
  • What is the consequence of pressing the ENG FIRE switch?
  • What is the primary function of the outboard brakes?
  • What is indicated by a CAS message in relation to the nosewheel steering (NWS)?
  • How many minutes of cooling must elapse between APU start attempts when the initial attempts fail?
  • What is the significance of brake cooling times before takeoff?
  • In which situation are ALT flaps needed?
  • What are the components of the oxygen system?
  • What is the transient limit for all generators?
  • What happens if the cargo door is not closed and locked while the left engine run switch is in the RUN position?
  • What component divides the left manifold from the right manifold?
  • If the elevator split is greater than what degree, an amber caution message is displayed?
  • Which of the following is NOT a limitation regarding the use of flight spoilers?
  • What is the function of the power transfer unit in the hydraulic system?
  • In case of failure of both the left and right hydraulic systems, how many brake applications can the accumulators provide pressure for?
  • When must all flight crew wear oxygen masks with EMERGENCY selected?
  • What will occur when the ENG FIRE switch is activated?
  • How many stick shakers does the Challenger 300/350 aircraft have and where are they located?
  • What happens when APU is turned on during an anti-ice application?
  • What is the immediate action required if the ICE DETECTED CAS message is presented during flight?
  • APR power initiated by the AUTO system is limited to how many minutes?
  • What is the maximum landing weight for the Challenger 300 aircraft?
  • Is prolonged use of passenger masks recommended above 25,000 ft?
  • What is the minimum bulk fuel temperature allowable when using Jet A fuel?
  • What is the VMO for the Challenger 300 at altitudes up to 8000 ft?
  • What are the thrust reverser limitations regarding ground operations?
  • Where does air from the right wind NACA scoop in the fuel venting system originate?
  • How many ozone converters are installed in the Challenger 300/350 aircraft?
  • What should be done if an equipment alert system signals during takeoff?
  • What components does the MultiScan radar utilize to create threat displays?
  • What happens if the yaw damper is engaged improperly?
  • If the Mach trim is inoperative and the autopilot is engaged, what is the speed limitation?
  • What indicates that the landing altitude was set manually by the pilot?
  • What is indicated by a combination of an up and down arrow on the TCAS page?
  • Is another start attempt permitted after an unsuccessful APU start attempt in the air?
  • Which function of the Smart Landing does NOT pertain to runway monitoring?
  • What power source is necessary to use the SPPR?
  • If an aircraft is operating on essential power, roughly how long will the batteries last?
  • To what maximum angle do multifunction spoilers extend when activated?
  • What is the purpose of the APU bleed valve?
  • What is indicated if the gear is not down and locked, and disagrees with the gear handle commanded position?
  • How many feet are added to cabin altitude to readjust for a High Alt mode caution light?
  • Are the leading edges of the horizontal stabilizer designed to be heated?
  • What is the thrust provided by the Automatic Power Reserve (APR) on the Challenger 300 up to ISA+20°C?
  • On the Challenger 300/350, which areas are equipped with a fire extinguishing system?
  • How many smoke detector(s) are installed on the Challenger 300/350 aircraft?
  • What is the maximum ramp weight for the Challenger 300 aircraft?
  • Which computer monitors the bleed-air leak detection system?
  • In what scenario is the takeoff configuration warning system activated?
  • Where is the hydraulic engine-driven pump (EDP) typically located?
  • What does PTU stand for in aviation?
  • What is the VLO EXT for the Challenger 300/350 aircraft?
  • What is the maximum altitude for starting the Auxiliary Power Unit (APU)?
  • What items are heated when selecting the PROBES pushbutton annunciator ON?
  • At what bulk fuel temperature is takeoff prohibited?
  • Can the stick pusher be overpowered by the pilot?
  • Which flight controls does the right yoke operate when the pitch disconnect handle is engaged?
  • Which unit do the dual detection loops in the APU enclosure connect to?
  • What occurs when the L or R ENG FIRE switch is activated?
  • What is the minimum pavement width required for a 180° turn with a 5-ft safety margin?
  • Under what condition does the PTU operate?
  • What occurs during the maximum differential pressure limit?
  • What is the maximum allowable bulk fuel temperature?
  • What functions are lost when PRI stab trim is switched to SEC trim?
  • What limit exists for single-point pressure refueling in the Challenger 300/350?
  • Are normal braking and nosewheel steering available in flight?
  • What is the maximum landing weight for a Challenger 350 aircraft?
  • Which spoiler panels move on the ground?
  • What limitations apply to engine anti-ice usage on the ground?
  • Which of the following weights is the Challenger 300 NOT designed to exceed during landing?
  • What is the required action if the APU does not start after two attempts?
  • Which items are monitored by the takeoff configuration warning system?
  • What symbols are used on the TCAS page to represent TCAS supplemental information?
  • What is the maximum speed at which the Challenger 300/350 can operate without exceeding VLE?
  • What is the purpose of a bent tab on aircraft control surfaces?
  • Where does the APU obtain fuel for operation?
  • Which control surfaces are powered by the right hydraulic system?
  • What is required for the FMS to calculate a navigation solution?
  • When considering the Challenger 300, what does the acronym ISA refer to in general aviation?
  • Where is the underwater locator device located in an aircraft?
  • Why is there typically more fluid in the left hydraulic reservoir than in the right?
  • What is the VLO RET speed for the Challenger 300/350 aircraft?
  • What cabin altitude triggers a caution light?
  • What type of air is used for pressurization?
  • What function does the right battery serve during APU start?
  • What indicates that a Nav radio has failed?
  • Why can engines only operate for 30 minutes with less than 1000 lb of fuel per side?
  • What is the limitation for left engine start on the ground using APU bleed air?
  • Which function is available in Manual mode?
  • During which phase of flight are oxygen systems most commonly utilized?
  • Under what circumstances must the wing anti-ice system be turned ON?
  • Which electrical source powers the left direct current motor pump (DCMP)?
  • What displays when the IRS alignment process is complete?
  • Is there an artificial feel to the rudder controls?
  • In which areas are maintenance interphone panels located?
  • What is the maximum speed at which the gear may be in the down-and-locked position?
  • How can the landing altitude be manually set?
  • What indication is displayed on the EICAS when the cargo door is not fully closed and locked on the ground?
  • What type of information is displayed as airspeed on the PFD?
  • Which electrical buses are powered when only the APU is online while on the ground?
  • Automatic power reserve (APR) on the Challenger 350 provides 7323 lb of thrust up to what temperature?
  • During a flight, what is the recommended approach speed to avoid a flight spoiler extension?
  • What is the condition under which fuel transfer is not allowed?
  • What occurs when the EMER/NORM switch is set to the EMER position on the audio control panel?
  • What should be monitored on the EICAS during critical phases of flight?
  • Is the flight path vector tuned through the REFS 4/4 menu?
  • What happens to the hydraulic SOVs when the ENG FIRE switch is activated?
  • Which flight control does the right yoke operate when pulling the roll disconnect?
  • Which sources are capable of providing air to the aircraft's packs?
  • Do audio signals from the aural warning system, TAWS, and TCAS go through the volume control switches of the audio control panel?
  • What is the engine designation for the Challenger 300 aircraft?
  • At what altitude does the half bank mode automatically engage?
  • At what altitude or after what duration of time does the aircraft exit the takeoff CAS message inhibit period?
  • What is the maximum altitude that the APU GEN can be utilized?
  • True or False: The autopilot operates normally in secondary trim.
  • What are the limitations with flight spoiler use?
  • At what PSI is the intermediate pressure regulated?
  • How is slant distance to the DME ground station calculated?
  • Can a second start attempt of the APU be made in flight after a hung start without waiting?
  • How is the landing altitude typically set in an aircraft?
  • Under what conditions does the automatic APR activate?
  • What does a cyan ICE DETECTED (A) EICAS message indicate?
  • How many stick pushers are in the Challenger 300/350 aircraft and where is it located?
  • What is the maximum zero fuel weight for the Challenger 350 aircraft?
  • What is the VRA for the Challenger 300/350 aircraft?
  • Where is the CB2 circuit breaker panel located?
  • What action is prohibited regarding emergency spoilers?
  • What is the maximum takeoff weight for the Challenger 350 aircraft?
  • Which system powers the inboard multifunctional spoilers?
  • Is the engine spinner equipped with anti-ice features?
  • What is the required cooling time between APU start attempts?
  • To what degree can the multifunction spoilers extend with control wheel input?
  • Landing gear downlock safety pins are provided for which landing gear assembly?
  • What range activates the automatic MFD map mode for terrain awareness alerting?
  • What is the maximum speed for VLO EXT?
  • What indicates that the nosewheel steering limit has been exceeded?
  • True or False: Both fire extinguishing bottles are equipped with two squibs each.
  • What is the minimum altitude at which the autopilot may remain engaged during nonprecision approach operations?
  • What does a green AVAIL message on the electrical panel indicate?
  • For takeoff, a fuel system icing inhibitor must be used when bulk fuel temperatures are below what temperature?
  • When does a CAS white PASSENGER DOOR message turn amber if the passenger door is open?
  • Which system is powered by the auxiliary hydraulic system?
  • If a series of defective components causes the available hydraulic pressure to decrease to 0, how can the rudder be controlled?
  • Flight spoilers must not be extended in flight below which approach speed?
  • For how long do the PCUs provide rudder dampening against gust loads after hydraulic pressure is removed?
  • What computer controls the outflow valve?
  • Can Air Source to Trim Air Only be selected on the ground?
  • When does the APU surge valve extract air from the APU?
  • What panel is responsible for selecting the APU as the bleed-air source?
  • What should pilots ensure about the yaw damper before proceeding with flight?
  • What is the purpose of the guarded EMER DEPRESS PBA?
  • What component prevents fuel from traveling outboard during low-wing maneuvers?
  • What color indicates a parameter that exceeds the established limits on the synoptic page presentation?
  • What is the limitation for extraction of bleed air from the APU for engine start and environmental air?
  • What is the significance of the 1/2 button on the display control panel?
  • What component is responsible for providing fuel to the APU?
  • Which buses are powered in flight with a single generator online?
  • What signifies the activation of the R ENGINE FIRE pushbutton?
  • What happens when the LG PULL handle is raised in flight?
  • What conditions exist while a pilot is depressing the MSW?
  • What is the minimum fuel quantity required to perform a go-around?
  • What system provides landing gear position monitoring?
  • What are the VFE airspeeds for flaps 10°, 20°, and 30°?
  • At what speed does the takeoff CAS message inhibit feature activate?
  • In the event of an engine failure, what function does the AUX hydraulic pump serve on the Challenger 300?
  • What is the normal operating pressure for the hydraulic system in the Challenger 300/350?
  • What does the acronym SLD stand for?
  • What is the minimum battery temperature for takeoff?
  • What component is used to detect ice in the aircraft?
  • What type of air is used for anti-ice purposes?
  • What is the cooling period required after three consecutive engine start cycles?
  • Is it permissible to operate the APU during fluid de-icing or anti-icing procedures?
  • What happens to the CAS message when the left engine switch is activated while the passenger door is open?
  • What is the primary function of the FIREX-CU?
  • At what latitude is FMS navigation prohibited?
  • At what oil temperature range may engines operate from idle up to but not including CLB power?
  • What is the normal takeoff power duration limit?
  • What is the typical flow rate of oxygen in the DEPLOY position?
  • During which conditions are ground spoilers armed?
  • What maintains fuel pressure during operation?
  • How is the APU remotely shut down while on the ground?
  • What color does the red beacon light turn to when the aircraft senses weight off wheels?
  • In the event of a red NORM BRAKES FAIL EICAS message, how can braking be achieved?
  • What is the primary purpose of the APU load control valve?
  • What type of message is displayed when emergency lights are activated?
  • What is the purpose of the 1/2 button on the display control panel (DCP)?
  • What is the maximum degree of nose gear rotation left or right of center with the torque link connected?
  • Pushing the R ENGINE FIRE pushbutton arms which extinguisher bottles for discharge?
  • Why are balance tabs installed on the aircraft's wings?
  • Under what condition can the flight spoilers be extended to EMER?
  • At what altitude is prolonged use of passenger oxygen masks not recommended?
  • What conditions must be met to erase data from the cockpit voice recorder?
  • How many APU start attempts are allowed before a cooling period is required?
  • When must the PACK be in operation while on the ground?
  • How long will standby instrument power support the ISI?
  • Is the travel time the same using ALT flaps compared with using normal flaps?
  • Is it necessary to open the fuel transfer valve to refuel?
  • What is the maximum amperage for one generator while on the ground?
  • What role do static wicks play on the Challenger 300 aircraft?
  • What computer controls the anti-ice protection system?
  • What are the four cockpit lighting zones in the Challenger 300/350 aircraft?
  • Can the Challenger 300/350 aircraft hold in icing conditions with flaps extended?
  • What is the maximum positive differential pressure?
  • What is the maximum amperage rating for the Ground Power Unit (GPU)?
  • What does RVDT stand for?
  • How many water sumps are installed in the aircraft?
  • When does the automatic "Pull up Pull down" function activate?
  • What might a failure to correctly manage cabin pressurization lead to?
  • Under what circumstances should the flight crew attempt to overpower the autopilot?
  • What is the primary source of power for heating the windshields?
  • What is the heat source for the wings of the aircraft?
  • While in flight, with all three generators offline, which buses are powered?
  • Where is battery voltage indicated in an aircraft?
  • With both engine run switches off, what EICAS message should appear if both fuel pumps are in automatic mode and the APU knob is selected to RUN?
  • When does the DC fuel pump supply fuel to the engine-driven pump during a normal start?
  • Which trim type is known to adjust more rapidly during takeoff?
  • What are the three modes of operation for the mask oxygen system?
  • What happens if the 1/2 button is selected on the display control panel?
  • Can the autopilot be re-engaged after pulling the roll disconnect?
  • What is the primary function of flapper valves in fuel systems?
  • Where is the anti-ice control panel located?
  • What is the VLE speed, which is important for aircraft performance?
  • Can the autopilot function be engaged independently of the yaw damper?
  • What is the function of the CAS message ELT ON?
  • Which spoilers are used for lift dumping during flight?
  • Where is the APU remote cutoff switch located?
  • In which manual are the brake cooling times charts located?
  • What is the maximum operating altitude for the APU?
  • When should the anti-ice systems be turned on?
  • How many feet are added to cabin altitude to readjust for a High Alt mode warning light?
  • What is the typical maximum takeoff weight used for flight planning?
  • What is the VMO for the Challenger 350 aircraft at altitudes between 8000 to 29,475 ft?
  • What is the maximum time limit for normal flap extension from 0 to 30 degrees?
  • What is the maximum operating altitude for JP-4 or JET B fuel?
  • What does the PTU primarily power?
  • What options does the crew have for flying the aircraft if not using flight directors?
  • What type of backup information does the ISI provide to the pilot?
  • Which of the following describes the limitation for the use of FMS performance speeds?
  • What must be done if flaps are extended in icing conditions?
  • Which window is heated by ESS power only?
  • In RNP airspace, how often should the FMS position error be less than the RNP value?
  • What is the consequence of exceeding the normal takeoff power duration limit?
  • True or False: In the event of an APU FIRE in flight, the crew receives indication of a fire, but no automatic action occurs.
  • True or False: Both flight guidance computers must be operational for the autopilot to function.
  • Which flight control surface does the right yoke operate when pulling the pitch disconnect handle?
  • What feature uses an up arrow and down arrow to communicate altitude changes of targets?
  • What is included in the emergency equipment of the Challenger 300/350 aircraft?
  • During normal operation, what is the primary source of air for the air-conditioning PACK?
  • Where do the left and right DCMPs obtain their power?
  • What is the purpose of the multifunction displays in an aircraft?
  • Which state deters a takeoff due to high fuel temperature?
  • What happens if no fuel transfer is initiated on takeoff?
  • What are the primary flight control components?
  • What is the consequence of extending flight spoilers below the minimum approach speed?
  • What types of displays are integrated into the primary flight displays?
  • What is the minimum flight weight for the Challenger 350 aircraft?
  • How many dual temperature sensors are located in each wing's anti-ice system?
  • What is the MMO for the Challenger 300/350 aircraft when flying above 29,475 ft?
  • When should the APU be restarted if the RPM is under 30%?
  • With the spoilers in the MAX position and flaps set to what degree, may the aircraft show a slight wing dip?
  • Which primary flight controls are hydraulically powered?
  • What is the maximum altitude permitted to extend the landing gear?
  • What are the pressure limits for SPPR?
  • Which component commands the roll spoilers to move in an aircraft?
  • In addition to generating power, what is another purpose of the APU?
  • Where are the spoiler RVDTs located?
  • What happens to the yaw damper system during an autopilot disengage?
  • Which phase of flight requires special attention to hydraulic systems for landing gear operation?
  • What is the maximum airspeed to start the APU?
  • When is the emergency locator transmitter automatically activated?
  • What is the maximum amperage for one generator while in flight?
  • How is a DME hold executed?
  • Which fire bottle has two squibs?
  • How does the Challenger 300 handle thrust in high-temperature conditions?
  • From where does the refueling panel obtain its power?
  • What advantage does the GPS have when used with the satellite-based augmentation system (SBAS)?
  • While in flight, which electrical buses are powered with only one generator online?
  • How many static wicks are installed on the Challenger 300 aircraft?
  • Where is the oxygen service point located on the aircraft?
  • When extended, to what degrees do the ground and multifunction spoilers extend?
  • Which of the following is a primary concern of the proximity sensing system?
  • Which sources provide air for the air-conditioning PACK to operate?
  • Why do flight directors display flight guidance cues on the attitude indicators?
  • How long do the PBEs generate oxygen when activated?
  • If primary trim is inoperable, is configuration trim still available?
  • What is the fluid capacity of the left reservoir?
  • What is the proper condition for accurately checking the brake wear indicator pins during preflight?
  • What is the VMO for the Challenger 300/350 aircraft at altitudes up to 8000 ft?
  • Which two subsystems make up the proximity sensing system (PSS)?
  • How many circuit breaker panels are there on the Challenger 300/350 aircraft?
  • True or false: The bleed valves are pneumatically operated and electrically controlled.
  • What cabin altitude triggers a warning light?
  • From where does the PTU obtain its pressure?
  • Which feature of the Challenger 300 ensures it can operate safely if an engine fails?
  • What does the crew mask supply at cabin altitudes above 35,000 ft?
  • Which altitude is critical for the deployment of crew cigarette oxygen masks in emergencies?
  • What is a primary requirement for operating thrust reversers on paved surfaces?
  • The control display unit is one of two ways to control what?
  • How many fire bottles are installed on the Challenger 300/350 aircraft?
  • What is the primary purpose of the electronic control unit in the spoiler system?
  • What powers the emergency lights on an aircraft?
  • What is the essential role of the integrated air system controller?
  • What is the maximum altitude the aircraft can fly with the yaw damper inoperative?
  • What position must the XFER switch be set to for fuel transfer?
  • To which functions does the Challenger 300/350 MFD COM display provide control capability?
  • What does the abbreviation KIAS stand for in aviation?
  • Which flight control surface is operated by the left yoke when the pitch disconnect handle is pulled?
  • How many static wicks are installed on the Challenger 350 aircraft?
  • What is the purpose of the Power Transfer Unit (PTU) in the Challenger 300/350?
  • Which mode of TAWS is associated with the windshear function?
  • Which items are powered by the left and right AUX buses?
  • What are the fuel temperature limitations for operation?
  • Under what conditions does the anti-ice system generally operate?
  • Why is it important to turn on the right battery first?
  • What is the purpose of the % MAC figure after weight and balance is completed?
  • What is the maximum speed for starting the APU?
  • What type of maintenance is indicated by a required check of electrical buses?
  • During which phase of flight must the fuel XFER PBA be selected closed?
  • What action should be avoided regarding trim air while on the ground?
  • What is the minimum flight weight for the Challenger 300 aircraft?
  • In which mode selection does the Mode S transponder report neither Mode C nor Mode S?
  • What is the automatic landing altitude return-to-base criteria?
  • How is the wing anti-ice air discharged?
  • How is a failed NAV radio indicated on the MFD display?
  • What does DME compare and decode?
  • What unusual sound might indicate an issue with the surge valve in the APU area?
  • What is the total fuel capacity with single-point pressure refueling?
  • Which of the following are considered secondary flight controls?
  • When the EMER/NORM switch is set to EMER, which audio is prioritized?
  • During towing, how many degrees can the nosewheel swivel through without disconnecting the steering torque links?
  • What happens when the autopilot is engaged if the Mach trim is inoperative?
  • Into which manifold does the ground air cart feed?
  • What are the limitations in reference to the aircraft terrain awareness and warning system (TAWS)?
  • What color indicates EICAS engine limits?
  • How is the outflow valve actuated?
  • What indicates that the ELT is transmitting?
  • Can the yaw damper be engaged independently of the autopilot?
  • To what PSI is high-pressure bleed air regulated?
  • From which location is the primary cabin lighting controlled?
  • Which system does the GPS NOT provide information to?
  • Where is the cabin zone temperature sensor located?
  • What can cause the PTU to activate?
  • Where is the crash ax located in the aircraft?
  • Which landing gear have weight-on-wheels proximity sensors?
  • When the emergency light switch is set to ON, what is displayed?
  • When is fuel transfer prohibited?
  • What type of hydraulic fluid is approved for use in the Challenger 300/350 aircraft?
  • What does the amber EMERGENCY EXIT indication on the EICAS represent?
  • How much steering authority does the pilot have through the tiller?
  • What is the maximum negative differential pressure?
  • How does manual reversion operate in the aircraft system?
  • What is the outside air temperature limit for using wing anti-ice on the ground?
  • What is the minimum oil temperature limit for takeoff with air temperatures below -30°C?
  • The HTF 7350 (AS907-2-1A) is flat rated at what weight?
  • What auxiliary system powers the lower rudder PCU during a right system failure?
  • What is the primary purpose of safety valves in an aircraft cabin?
  • For how long can the engine be motored (cranked)?
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