Beechjet 400A Computer Training Systems (CTSys) Practice Test

These questions are part of the practice quiz. Start practicing

• How many airstarts are permitted when an engine has been shut down due to obvious mechanical difficulties?
• If No.1 inverter fails, what does No.2 inverter do?
• The aft baggage load limit is less than the maximum landing weight. Which statement is true?
• Which statement correctly describes the wing anti-icing switch location and system?
• When landing with ice accumulation on the wings, what is the recommended airspeed after final flap extension?
• Which statement best describes nose wheel steering?
• Per engine oil replenishment limit per 400 hours
• The maximum N2 for takeoff is:
• With flaps at 0 degrees, what are the maneuvering load factors?
• If the crew notes RPM decay, slower acceleration and increased travel for a given power setting, this indicates which subsystem failure is most likely?
• The L or R FUEL TRANS PRESS LO light indicates that:
• If the LH engine fire light remains on after moving the thrust lever to IDLE, which sequence should the pilot perform?
• How many filler ports are used for refueling Beechjet 400A?
• Which annunciator indicates a clogged fuel filter?
• Which statement about Synthetic Type II replenishment is true?
• For an approach climb on a one-engine go-around, what is the designated initial flap setting?
• The quick dump valve, located on the bottom left edge of the right instrument panel provides a means for rapid and complete cabin depressurization.
• If the engine does not light off within 10 seconds during start, which action should be taken?
• Which condition triggers the emergency pressurization valve to open?
• When using the autopilot, nav captures, including localizer captures, must be accomplished with an intercept angle of:
• What is the first crew action in response to an electrical fire or smoke?
• Which gauge has a yellow arc indicating 1200 to 1350 psi?
• With flaps at 0 degrees, the maneuvering load factors are within the range of:
• Flight in visible moisture without pitot heat may result in erratic operation of which instruments?
• The nonessential buses are protected by what type of device on the main circuit breaker panel?
• Which of the following is/are protected by a heating system?
• Which unit is used for weight on the Beechjet 400A?
• The refrigeration air conditioning OFF for Takeoff and Landing.
• The maximum N1 at transient is:
• Which of the following is true about the Beechjet 400A's fuel system configuration?
• Which statement correctly matches the JT15D-5 engine’s thrust values on a standard day?
• The high compressor section of the JT15D engine consists of which component?
• No-flap approach and landing will cause landing distance to
• Which condition will illuminate the L or R FUEL LEVEL LO lights?
• The Pratt & Whitney JT15D-5 turbofan engine operating limit for engine start if the ITT is 550 to 600 degrees C is a maximum of:
• The cabin press LO light may illuminate during takeoff at airports above what elevation?
• In a false start, what is the first action you should take?
• Which four positions are marked on the engine thrust levers?
• During an aborted takeoff, if engine fire indications exist, should you deploy the reverser on the affected engine?
• Pressure above 53 PSIG or temperature above 400 F will close both pressure-regulator and shutoff valves, and open the emergency pressurization valve. Which values are these thresholds?
• If the L FUEL PRESS LO annunciator illuminates, the correct crew action is:
• The ITT gauge yellow arc indicates temperatures between which range?
• Normally, from which source is the No.2 inverter powered?
• Which indicator shows the left gear is not locked when the gear handle is down?
• Which of the following is NOT a marked thrust lever position?
• The load limit for the aft cabin baggage compartment is
• What is the status of the NOSE and RH gear lights when the left gear is unlocked?
• The maximum differential pressure is:
• Which combination constitutes proper normal operation of the inverter and its control in the AC electrical system?
• Inadvertent overspeed, the crew should first:
• If the FIRE DET FAIL annunciator illuminates following an ENG FIRE PUSH switch illumination, the fire should be considered to be:
• On the ground with gear down and anti-skid ON, anti-skid protection is active under which condition?
• Which light indicates aft fuselage tank depletion?
• The maximum wing tank imbalance for takeoff is 100 pounds. Which of the following reflects that?
• During smoke removal procedures in flight, to what altitude should the aircraft descend?
• Which of the following sequences correctly describes the overspeed recovery steps?
• If the speedbrakes are extended and you need to retract them, which procedure should you use?
• If stabilizer ice is suspected and the anti-ice/deice switches are off, what is the recommended flap limit?
• If operation of the vent blower fan is desired prior to starting engines, how long must you wait after turning off the vent blower before opening the cabin door or emergency exit?
• How many positions does the AC voltage selector switch have?
• Which annunciator indicates wing tank overpressure?
• If the LH engine fire light remains on after moving the thrust lever to IDLE, which action should be performed next?
• In case of failure of the horizontal stabilizer anti-ice or deice system, with both switches off and ice suspected, the maximum flap deflection is limited to:
• If you cannot isolate the electrical fire source and both generators are switched to EMER, what should the crew do?
• The anti-ice system on the Beechjet 400A should be used at ram air temperatures of at most what, unless icing conditions are indicated?
• Unless icing conditions are indicated by the ICING annunciator or airframe ice accumulation, at ram air temperatures above what value should anti/deice systems not be operated?
• Rudder boost must be operable and:
• What is the total usable fuel in the Beechjet 400A?
• What is the biggest hazard of turning on wing anti-ice when ice is on wings?
• Which statement about elevator trim tabs is true?
• If the thrust reverser ARM annunciator remains illuminated after corrective actions, what is the recommended course of action?
• If the yaw damper fails in flight and cannot be re-engaged, the flight may be continued below 28,000 feet.
• Under normal operation, which statement is true about the inverter control settings?
• During cruise flight, the electrical boost pump switches should be selected:
• Before opening the cabin door after turning off the vent blower, how long must the vent blower be off?
• What is the effect of placing the battery switch in the EMER position?
• Which pair of buses are connected by the LH BUS TIE RCCB to allow power routing?
• If the speedbrakes fail in the extended position, EMER RET retracts.
• How many fuel tanks are in the Beechjet 400A fuel storage system?
• Maximum takeoff weight is described as being limited by
• Which statement is true regarding the engine compartment fire extinguishing system?
• The maximum ITT temperature for continuous operation is:
• The Beechjet 400A fuel storage system consists of which tanks?
• Which statement is true about manual cabin pressure control?
• An adjustable gust lock immobilizes the elevators when attached to the what?
• Which sequence correctly describes the left fuel system action when the L FUEL PRESS LO annunciator is lit?
• What is the maximum continuous thrust of the JT15D-5 engine?
• Which of the following represents the proper switch positions for normal operation of the AC electrical system?
• Engine oil is cooled by means of which device?
• If the landing gear handle is down but the left gear does not lock, which indicator configuration is shown?
• What is the usable fuel capacity of the Beechjet 400A?
• Which statement about cooling the engine oil is true?
• If FUEL XFEED is set to L TANK, the left tank fuel is available to which engines?
• When the electric boost pump is operating, the crew is informed by means of:
• To disconnect the LH Main bus from the battery charge bus, pull the:
• What is the recommended action if the battery temperature does not decrease after switching OFF, according to the procedure?
• Which of the following is the correct value for the maximum N1 redline?
• If gear is raised after takeoff with a flashing master warning and thrust reverser ARM annunciators, what is the probable cause?
• What is the maximum fan RPM (N1) percentage?
• The mistrim warning horn will sound during takeoff if pitch trim is not within the takeoff range.
• What is the maximum operating altitude?
• Illumination of the L or R WG TK OV PRESS annunciator indicates pressure in the wing tank in excess of 3.5 psid and also causes:
• The maximum time for continuous reverse thrust above reverse idle is?
• During approach in icing conditions, wait at least how many seconds after selecting 10 degrees flaps before selecting 30 degrees flaps?
• Each Beechjet 400A generator is rated at:
• If the battery temperature reaches 150°F and does not decrease after turning the battery OFF, what is the recommended action?
• In the event of a jet pump failure, what action should the crew take for the affected engine?
• The exhaust section delivers thrust by what mechanism?
• Which component limits cabin altitude to approximately 12,500 +/- 1,500 feet?
• The Beechjet 400A's maximum differential pressure is:
• If the oil pressure is 50 PSI and the OIL PRESS LO light does not illuminate, the pilot should:
• What does the engine fire detector test switch enable the crew to check?
• What maximum airspeed should be maintained after cutoff due to inadvertent reverser not stowing?
• During icing approach, after selecting 10 degrees flaps, wait how many seconds before selecting 30 degrees flaps?
• Which caution light indicates engine inlet bleed air temperature is too low?
• Under icing conditions, if icing is encountered for more than 10 minutes after selecting 10-degree flaps, should you land with 10-degree flaps?
• If wing tank overpressure occurs and the respective transfer switch is in AUTO, what happens to the transfer pump?
• An engine synchronization system automatically synchronizes the engines to reduce noise level and enhance passenger comfort.
• What is the maximum redline N1 percentage?
• As the spoilers on one wing extend, what do the spoilers on the other wing do?
• With the electric boost pumps in Auto, the crew can expect the respective pump to operate:
• If after corrective action the reverser will not stow and UNLOCK/DEPLOY annunciators and EMER STOW are illuminated, the crew should move the thrust lever to which position?
• Environmental system smoke or odor: after the crew dons oxygen masks and selects Mic to OXY MASK, the next action is to isolate the cabin pressure source by selecting L ENG or R ENG.
• During overspeed, if the aircraft is nose down, what action should be taken?
• What is the maximum engine oil temperature specified for the Beechjet 400A?
• On which panel does the L or R OIL PRESS LO warning light appear?
• The windshield heat must be used during flight under which condition?
• The fuel system is designed to operate between sea level and how many feet, with a temperature range from -40 °C to what °C?
• In OEI conditions with a reverser deployed, the landing distance is expected to increase by about what percentage?
• How many mid fuselage tanks are in the fuel storage system?
• Which option states manual cabin pressure control using the MAN PRESS CONT valve?
• The VMO airspeed limit at 19,000 feet is 320 KIAS.
• Nav captures with the autopilot must have an intercept angle of:
• Which annunciator action occurs when EMER BUS FAIL is indicated?
• In a power brake failure, the pilot will break the safety wire and remove the guard clip on the emer brake handle, then pull that handle. Approximately how many applications are available with a full system?
• If the airplane is equipped with a battery temperature light and the temperature continues to rise and reaches 150 degrees F, the crew should:
• The maximum generator load limit before attempting a generator assisted start is
• What type and labeling do the generator master switches have?
• When testing the stall warning system before starting the engines, the master test switch must remain in which position until the column shaker and stall annunciator lights/horn actuate twice?
• Which statement best describes the Beechjet 400A fuel system's per-engine fuel supply?
• When the trim interrupt switch is pushed, the autopilot is disengaged and:
• What do control column shaking and an angle-of-attack display on cockpit indicators warn you of?
• If a one engine inoperative approach and landing is conducted with a reverser deployed, how does landing distance change?
• How many forward fuselage tanks does the fuel storage system include?
• In turbulent air penetration, what airspeed should be maintained?
• Maximum takeoff weight for the Beechjet 400A is
• Which option completes the LH engine fire sequence after the initial step of moving the thrust lever to IDLE if the LH engine fire light remains on?
• In non-icing conditions, the anti-ice system should be used only at ram air temperatures of:
• In flight, if an inadvertent thrust reverser deployment occurs and UNLOCK/DEPLOY annunciator illuminates, the pilot should first perform which action?
• Which component is used to increase bleed air flow through the venturi of the ACM?
• What is the red line maximum on the ammeter for RK1 through RK97 not modified by one of the appropriate kits?
• When the L or R F FLTR BYPASS annunciator indicates a clogged filter, what is the recommended crew action?
• If UNLOCK/DEPLOY annunciator and EMER STOW illuminated after thrust reverser deployment, what does this indicate?
• The maximum fuel imbalance permitted for landing is:
• Above 60% N2, the normal engine oil pressure is within which PSIG range?
• Fuel flow to the engine is controlled by which system?
• The minimum oil pressure at idle when N2 is below 60% is which PSIG?
• The fuel transfer switches are three position switches labeled:
• The aft filler tank is located in which part of the aircraft?
• To start the right engine, the crew should first perform which action?
• What would the thermal discharge indicator on the aft left fuselage show if one or more fire bottles had been discharged?
• If the RH load bus DC power fails, what happens to the No.2 Inverter relay?
• The Beechjet 400A is approved to operate up to:
• During normal operation, which buses are powered by No.1 inverter?
• During takeoff, thrust setting must be attained by which indicated airspeed?
• The thrust reversers can be deployed under which conditions?
• Which subsystem carries the load to the electrical loads?
• The aural tone that sounds when the autopilot disengages can be cancelled by a second actuation of which control(s)?
• Ignition switches on the Beechjet 400A are which type?
• If cabin altitude cannot be corrected and exceeds 14,000 feet, what procedure should be initiated?
• The ram air duct includes a check valve to provide ventilation when conditioned air is unavailable.
• What is the minimum voltage required to attempt a battery start?
• Maximum takeoff weight is limited by
• The temperature control system for air conditioning is operated by which power source?
• FMS navigation data base updates must be loaded at the end of which period?
• If the CABIN PRESS LO light illuminates and cabin decompression is not rapid, when should emergency descent procedures be initiated?
• How is the turbine section of the JT15D engine described?
• The cabin pressurization controller can vary cabin altitude from which range?
• When the right load bus loses power and No.1 inverter has failed, No.2 inverter is powered from which bus?
• What is the purpose of the water separator of the air cycle machine?
• What does the NORM T.O. marking on the thrust lever indicate?
• What is the first pilot action if experiencing an engine failure above V1 during a takeoff?
• Which power distribution system provides the connection between the main buses and the respective load buses?
• If the right load bus loses power and No.1 inverter has also failed, from which source does No.2 inverter receive power?
• When operating above 41,000 ft with both generators operating, current is limited to per generator
• Do the elevators have trim tabs?
• The maximum fuel temperature is:
• At what altitude is the VMO specified as 320 KIAS?
• The function of the altitude pressure regulator is to limit cabin altitude to what value range?
• Under icing conditions indicated by the ICING annunciator or airframe ice accumulation, the anti-ice system should be used at ram air temperatures of:
• The L FUEL LEVEL LO annunciator corresponds to fuel quantity in which tank?
• How many hydraulic actuators does each main gear employ?
• What is the minimum voltage allowable for a battery start?
• The ambient air temperature limitation for landings is:
• Which action completes the LH engine fire procedure after initial steps?
• Where is the wing leading-edge anti-icing switch located?
• In the event of pitch trim runaway, the crew's first action should be:
• Which statement about the Beechjet 400A is true?
• The windshield anti/deice switch to HI mode is prohibited during which phase?
• The maximum continuous ITT temperature is:
• During engine start, move the thrust lever to IDLE when N2 reaches what percent?
• If the LH engine fire ON light illuminates and the fire bell audible warning sounds, the pilot should first do what?
• The windshield heat guidance for flight is:
• Which are not buses in the secondary power system?
• The white light above the wing deice switch illuminates when the wing temperature sensor senses approximately what temperature?
• Igniters are located in which engine section?
• The minimum oil temperature for starting is:
• Which condition allows anti-ice operation above 10 °C?
• Autopilot disengagement will initiate an aural tone. The tone can be cancelled by a second actuation of the:
• When should fuel crossfeed occur?
• Should the pilot attempt to use the normal pitch trim system after pitch trim runaway?
• Which statement best describes when the battery feeder fail light will illuminate?
• In the Beechjet 400A, a jammed stabilizer in a nose-down position requires following normal landing procedures.
• When the STAB anti ice control switch is turned on, the system's light will:
• Which statement about battery feeder fail light is true?
• What does the AUTO position do for the fuel transfer pump?
• If the engine does not light off within 10 seconds during start, which sequence should be followed?
• During a false start, what is the correct sequence of actions to purge fuel and attempt a restart?
• FMS navigation data base updates must be loaded each:
• If the EMER BUS FDR FAIL annunciator comes on, the emergency relay opens and the emergency bus receives power from which bus?
• If the GEN OFF light illuminates and cannot be reset, the operating generator N2 should be:
• Which is true regarding the autopilot?
• During stall warning system testing, the master test switch must remain in which position until the column shaker and stall annunciator lights/horn actuate twice?
• Which statement is true regarding in flight operation of the ice protection systems?
• What color is the indicator light that shows the electric boost pump is operating?
• If electrical fire results in switching both master generator switches to EMER, which systems will not be available?
• If external power is used to start the aircraft, what should the battery switch be?
• Refueling of the Beechjet 400A is accomplished through?
• Describe the DC voltage selector switch.
• The L or R ENG ICE TEMP LO caution light indicates engine inlet bleed air temperature is:
• During takeoff, if an inadvertent thrust reverser deployment occurs below V1, what is the first pilot action?
• Which statement about takeoff and fuel configuration is true?
• What is the maximum tailwind component allowed for landing?
• What is the maximum wing tank imbalance allowed for takeoff in the Beechjet 400A?
• Which option correctly represents the normal oil pressure range above 60% N2?
• What is the first action the crew should take in an emergency descent?
• Which component is responsible for producing thrust by mixing bypass air with core exhaust?
• The correct type of oil for the Beechjet 400A engines is
• During hydraulic operation, which color band on the hydraulic pressure gauge indicates 1850 psi?
• The engine anti-ice system requires the engine anti-ice switch to be ON to regulate bleed air pressure to 16 PSI. True or False?
• In an inadvertent icing encounter, turning wing anti-ice ON with significant wing ice accumulation could result in engine ice ingestion.
• What is the minimum duration the standby power system can supply emergency power?
• If a thrust reverser ARM annunciator remains illuminated in flight after corrective actions, what should the crew do?
• The MAN PRESS CONT valve is located on which panel?
• The yellow arc of the Nitrogen pressure gauge indicates a range of:
• Regarding the EFIS, which statement must be true for takeoff?
• A GPU start is recommended at ambient temperature below approximately minus 15 degrees C with a DC voltage minimum of how many volts?
• The yellow arc on the ITT gauge indicates temperatures between which range?
• The red line on the oxygen pressure gauge indicates a pressure of what value?
• All generator power is distributed through which components?
• The statement 'In turbulence, maintain 200 KIAS' is true.
• When does the L or R OIL PRESS LO warning light illuminate?
• During emergency braking, is it advisable to use the normal braking system for optimal braking power?
• In a pitch trim runaway, the initial action is to:
• What energy source powers the wing leading-edge anti-icing system?
• The primary power distribution system consists of the left main bus and:
• Engine anti-ice systems must be on for taxi and takeoff when in visible moisture at what temperature?
• Which statement accurately describes the relationship between the cabin pressure controller and the altitude regulator?
• What is the probable cause for a flashing master warning after gear retraction?
• The heating system protects which items?
• In the event of high engine oil temperature, what procedure should the crew follow?
• Which statement correctly describes the role of the primary power distribution system?
• For ditching, what is the flap setting during the approach?
• Which indicator illuminates to indicate inadvertent thrust reverser deployment in flight?
• A rotating-disc-type assembly in each main gear provides:
• How long should crew wait before attempting a second external power assisted start after the first start attempt fails?
• The L FUEL LEVEL LO annunciator indicates approximately how much fuel remains in the left tank?
• In an engine failure during landing configuration, what is the recommended action regarding thrust?
• The landing gear warning horn sounds when the gear is retracted and:
• If No.1 inverter fails and No.2 inverter takes over, what happens to the secondary buses?
• Which statement describes the low-pressure turbine in the JT15D engine?
• A flow increase valve operates to increase the volume of bleed air flowing through the venturi of the ACM when the engine thrust lever is set:
• During an inadvertent overspeed, which phrase may be used to establish crew communication?
• In a false start, after purging fuel for 15 seconds, what action should follow?
• The DC electrical power distribution system has four subsystems. Besides power source distribution and primary power distribution, which are the other two?
• How many stages are in the low compressor section of the JT15D engine?
• What is the maximum fuel temperature value in degrees Celsius?
• A hydraulic pressure reading of 1850 psi would be indicated on the hydraulic pressure gauge at the:
• With speed brakes extended in flight, which statements are true?
• The JT15D-5 engine starting limit when ITT is 550 to 600 degrees C is a maximum of:
• Where is the indicator for electric boost pump operation located?
• For a jammed spoiler, the indicated approach speed should be VREF + 10 KIAS.
• In the event of a loss of both generators, the crew's first step is to:
• The takeoff mistrim warning horn will sound when thrust levers are advanced to takeoff position if the pitch trim is not in the takeoff range.
• The ambient temperature range for landings spans from:
• To have pressure regulator shutoff valve open and regulate bleed air pressure for engine anti-ice at 16 PSI, engine anti-ice switch must be in which position?
• What is the primary purpose of engine synchronization?
• Autopilot operation: which statement is true?
• When conditioned or emergency air is no longer being supplied, ventilation is supplied from which source?
• What is the static thrust of the JT15D-5 engine on a standard day at sea level?
• When FLOOR/DEFOG is set to DEFOG, defog air is directed to which area?
• Selecting the FUEL XFEED L TANK switch allows fuel from the left tank to supply which engines?
• For an approach with one engine go-around, what initial flap setting should be used?
• During takeoff, the CABIN PRESS LO light may be illuminated at airports above which elevation?
• Which valve provides manual cabin pressure control?
• When selecting the right generator on the DC voltage selector switch, which position is used?
• For a GPU start at ambient temperatures below approximately -15 C, the DC voltage minimum should be what value?
• What is the rating of each Beechjet 400A generator?
• The maximum landing weight is
• When the EMER BRAKE handle is pulled, how many brake applications can the air bottle provide?
• Which inverter is responsible for powering the primary buses when No.1 inverter fails?
• If a landing must be made with a jammed rudder, the guidance indicates that:
• The ON position of the fuel transfer pump switch is used:
• Oil pressure warning light illuminates when oil pressure falls below what value?
• If the FLAP ASYM light illuminates, the flaps can be moved from the position where asymmetry occurred.
• For Beechjet 400A, the maximum allowable fuel unbalance for landing is:
• When performing a one engine inoperative approach and landing, when should the flaps be set to 30 degrees?
• Which tank feeds the left engine during normal operation?
• If the same brand of oil is not available for replenishment, Synthetic Oil Type II may be added provided the total quantity added does not exceed
• Where is the standby power system mounted?
• During normal operation, to what position should the Inverter selector switch be set?
• The cabin pressure controller provides the crew with a means to control the pressurization system.