King Air 200/B200 Practice Exam

These questions are part of the practice quiz. Start practicing

• Which of the following is electrically powered?
• When using maximum reverse power at HI IDLE and full increase rpm, you would expect a maximum propeller rpm of
• The two transponders in Collins Proline 2 operate how?
• What is the maximum operating pressure limit of the pneumatic system?
• Electric gear - When full up or down position achieved, gear travel is limited by?
• If the TEST SWITCH is in LEFT EXT or RIGHT EXT during testing and the green OK light does not illuminate while the amber D light illuminates, what does this mean?
• What triggers the door between the aft blower duct and the warm duct to open?
• The wing and horizontal stabiliser leading edges are de-iced by which system?
• From sea level to 15,000 feet MSL, what is the normal vacuum range of the vacuum system?
• If the wing flaps are beyond the 40% (APPROACH) position, the warning horn will sound if:
• What is the maximum takeoff weight of the Super King Air?
• What is true about auto feather after liftoff?
• Where are the recognition lights mounted?
• When is cross feed use authorised?
• If a chip detector light illuminates, you must do?
• Which surfaces are de-iced by the pneumatically inflated boots?
• What is the switch labeled MASTER PANEL LIGHTS used for?
• When the AUTO IGNITION switch is in the ARM position, ignition is
• With the fuel loading from Question 8 added, will the takeoff weight and moment / 100 be within limits?
• Fuel is heated prior to entering the fuel control unit by:
• What are the starter limits?
• According to older specification, once manual control of the ice vanes has been used, what is required for the rest of the flight?
• If a bleed air system leak occurs, which statement about ITT is true?
• Where are the generator switches located?
• The two transponders are controlled by which panel?
• Which statement about the PT6A engine power section is true?
• What procedure closes the air-to-air heat exchanger valves?
• During an automatic de-ice cycle, how long does the wing boot stay inflated?
• In the CABIN TEMP MODE selector set to MAN COOL, how is the cabin temperature lowered?
• In the electric gear system, which component is used to decelerate gear movement as it approaches travel limits?
• The reduction gear system provides gear reduction for which component?
• If the cockpit temperature is too hot while the plane is being heated, which control adjustments are recommended?
• ALT WARN annunciator light illuminates when the cabin pressure altitude reaches?
• Which action specifically tests the cockpit annunciator lighting system?
• What is the required action to ensure the air-to-air heat exchanger valves are closed when using cooling mode?
• Which mechanism locks the nose gear down?
• Which statements are applicable to flight in icing conditions?
• What is the minimum number of static wicks required for the Super King Air?
• In heating mode, which action best reduces the cockpit temperature?
• Where is the external power connector located?
• If the BATTERY CHG light does not extinguish in flight when the BAT control switch is OFF, what action should be taken?
• What is the maximum duration brake de icing can operate after wheels retract before extending gear again?
• Which indicator signals DME Hold status on NAV radio?
• What senses windshield glass temperature for regulation?
• The EXT PWR indicator serves to alert the operator that which of the following is connected?
• During preflight, which action confirms stall warning functionality?
• How is the rudder boost system checked for proper operation during engine run up?
• The GND COMM PWR button on Collins Proline 2 is used to communicate through which COM when the battery switch is off?
• During normal operation, which indicator signals discharge of the supply cylinder?
• Electric gear - Electric motor torque is transmitted to the gear actuators by?
• The negative pressure for the cockpit vacuum originates from which source?
• When a generator is off line, what indication is present?
• Electric gear - In the event of electrical failure, the landing gear is extended by using what?
• When is the yaw damper required?
• Why must current requirements of the propeller boots be monitored?
• The extension handle is located where?
• After a bleed air warning with the bleed air valve set to INST and ENVIR OFF, which engine instrument changes are monitored?
• The function of the reduction gear system is to provide gear reduction for which component?
• External power must not exceed what voltage for more than two minutes to avoid battery damage?
• Which switch would you use to control all cockpit panel lighting?
• What protects the engine compressor inlet screen from ice particles?
• The auto deployment system operates at which cabin altitude?
• What bus powers the air stair floodlight?
• What action must be performed to arm the auto deployment oxygen system?
• On airplanes with optional elevator electric trim, how is trim initiated?
• Where is the inverter switch located?
• What is the maximum cabin pressure differential for the Super King Air airplane?
• What is the basic weight of the described airplane?
• During ground operation at LO IDLE, ITT is exceeding 750 degrees C. Which actions would you consider best to reduce ITT?
• What is the cooling capacity of the aircraft without the aft evaporator?
• What is the moment / 100 value before loading in the described scenario?
• Which factor is used to determine whether the airplane is within weight and balance limits?
• What happens to the electricity driven hydraulic pump when the landing gear is fully retracted?
• Which indicator reflects the rate of cabin pressure altitude change?
• If the amber Battery CHG annunciator illuminates in flight, what is the initial action?
• Windshield wipers may be used under which circumstances?
• In conditions with an outside air temperature of +38°C, the right engine N1 is decreasing and ITT is rising rapidly. What is the best action?
• Which condition automatically activates the threshold and aisle lights?
• If the boots are held inflated too long, what could happen to ice on the surfaces?
• After takeoff how are the landing lights extinguished?
• The AUDIO EMERG NORM switch is used to bypass which amplifiers?
• If the propeller de-ice current exceeds the green arc but the circuit breaker does not trip, what is the recommended course of action?
• The PT6A engine power section consists of?
• Where is the battery located on the aircraft?
• During manual operation of the propeller de-ice system, what is observed on the ammeter?
• How can the annunciator lights be tested?
• What action causes the CAUT LGNG OFF light to illuminate on 200 models?
• Which value represents the continuous current capability the external power unit must provide?
• How much continuous current should the external power unit be capable of supplying?
• What is the rating of an individual generator?
• What limitation applies to operation with aviation gas?
• What is the frequency of the inverter outputs?
• Collins Proline 2 - The ACT annunciatior on the COMM radios:
• To obtain proper bearing information from the ADF on Collins Proline 2, the selector must be set to which position?
• Prior to B.B.-1444 except 1439, the manual control of the ice vanes:
• Operation of the engine with the FUEL PRESS light illuminated is limited to how many hours between main engine fuel pump overhauls or before replacement?
• In normal operation, which indicator signals that the supply cylinder has been discharged?
• If the wing and horizontal stabiliser boots are inflated with only a thin coating of ice on them, what would happen to the ice?
• What opens the mask dispenser doors during automatic deployment of the passenger oxygen masks?
• If during icing conditions the propeller de icing system draws excessive current ( higher than green arc) but does not trip the circuit breaker:
• When the rudder pedals are deflected with the airplane stationary, which condition occurs?
• How is the stall warning system normally tested prior to flight?
• What is the primary function of the engine inertial vane system?
• Which control is used to modulate the volume of air delivered to the cabin floor registers?
• The door between the aft blower duct and the warm duct opens when which condition occurs?
• A bleed air leak could cause which change in engine performance?
• How is the generator turned ON on BB88 and later?
• Where is the INVERTER switch located?
• Which statement about brake de-ice load on the bleed air system is true?
• On the Super King Air B200, which control governs the air volume through the floor registers?
• Where are the ice lights mounted?
• When the engine speed falls below 62% N1 the compressor clutch disengages and the green advisory annunciatior illuminates.
• Inverter system consists of how many inverters and what outputs do they provide?
• Which mechanism locks the main gear down?
• During external power use, what is the primary reason for keeping the BAT switch ON?
• Which statement is true regarding the weight limits for the Super King Air family?
• In the manual plug-in system (BB-2 through BB-54), when are the crew oxygen outlets activated?
• When an engine started, in what position should its GEN switch be?
• In icing conditions during flight, the stall warning is?
• To extinguish a MASTER WARNING flasher, which action must be taken?
• Where are the generator switches located?
• Where are the majority of cockpit lighting controls located?
• What is the purpose of the static wicks?
• Engine Torque Readout indicates which of the following?
• In case of bleed air failure from either source:
• Where are the crew oxygen masks stowed in the auto deployment system for BB-55 and later?
• The rate of change on RATE control knob may be from approximately what rpm?
• When will a red annunciator light extinguish?
• During a ground start of the right engine, the IGNITION ON light should illuminate
• What percentage of recirculated air passes through the ceiling outlet ducts?
• When the door between the aft blower duct and the warm duct opens, what happens to the heated air flow to the aft floor registers?
• What is the maximum allowable altitude with yaw dumping inoperative?
• Why should the rudder control lock be removed prior to towing the airplane?
• What is the voltage rating of the larger inverter output?
• When is cross feed use authorised?
• If brake de icing is used with boot inflation, at what engine N1 must be maintained?
• Collins Proline 2 - The GND COMM PWR button is used to?
• Collins Proline 2- The AUTO-COMM switch:
• If bleed air failure occurs, which system cannot be used?
• Hydraulic gear – The landing is held retracted by:
• When the propeller deice system is operated manually,
• In icing conditions, what is the minimum indicated airspeed necessary to keep the bottom of the wing leading edges ice-free?
• Which component is designated as a backup pump for use if the primary boost pump fails?
• Which position on RATE control knob provides the most comfortable rate of climb?
• Prior to entering the fuel control unit, what heats the fuel?
• The de ice boots should not be operated when the OAT is below:
• The fuel panel check tests electrical continuity to which item?
• When the landing gear is fully retracted, the electricity driven hydraulic pump:
• How many inverters are installed in the aircraft?
• When the PARKING BRAKE handle is pulled, which action takes place?
• Each of two fuel vent systems is kept ice free by:
• When should the sliding knife valve on a Monogram toilet be open?
• The inverter system provides which outputs?
• Which item is NOT a destination for bleed air from the pneumatic system?
• For BB88 and later, which is the correct method to turn the generator ON?
• Between supply cylinder recharges, how many times can the fire extinguishing system be fired per engine?
• Approximately at what temperature will the plastic pneumatic turbine of the bleed air warning system fail?
• Which statement describes brake de-ice and bleed air relationship?
• During unpressurized flight with the PRESS switch in DUMP, what is the source of fresh air?
• What is the maximum zero fuel weight for the Super King Air 200?
• DME Hold function is indicated by which annunciator on the NAV radio?
• Just prior to brake release with OAT +5 degrees C or less and visible moisture, what action should the pilot take?
• Before using an external power unit, what is the minimum battery voltage required?
• Which moment / 100 figure should be checked within limits on every flight?
• What is the purpose of the static wicks on the aircraft?
• During a fire detection system TEST, which signal is produced by the TEST SWITCH?
• Which statement correctly describes the ACT annunciator on the Collins Proline 2 COMM radios?
• Which mechanism describes how the boots de-ice the leading edges on the wing and horizontal stabiliser?
• With the airplane airborne, placing the LDG GEAR CONT switch handle UP, which occurs?
• The upper temperature limitation for safety using the engine anti icing vanes is
• What is the rating of the aircraft battery?
• Why must the PULL ON-SYS READY handle be pulled out prior to flight, arming the system?
• What is the rating of an individual generator?
• After starting the right engine and enabling the right generator, to what load meter reading should it fall before starting the left engine?
• Which statement correctly describes the Engine Torque Readout?
• Which function remains unaffected when the cross feed switch is repositioned?
• Why is it important to monitor propeller boot current requirements?
• In icing conditions, what is the combined effect on fuel consumption, propeller efficiency, and stall speed?
• Which statement correctly describes the two cooling capacities depending on aft evaporator presence?
• In 100% mode, how should the number of crew masks be used?
• Which lights illuminate when there is a failure in the pneumatic system?
• On airplane with serial number BB88 and subsequent, how is generator turned ON?
• What is the zero fuel weight of the described airplane with basic weight 8,087 LBS and loading as specified?
• What is the zero fuel moment / 100 after loading?
• At what cabin pressure altitude will the auto deployment system operate?
• What is the zero fuel weight for the Super King Air B200?
• Where are the ice lights mounted?
• Which instrument is associated with the right pitot mast?
• What is the total weight of two pilots and four passengers?
• Which indicator alerts the operator that an external power plug is connected to the airplane?
• What is the primary source regulating windshield temperature?
• What does the BRAKE DE ICE ON indication imply?
• What instrument does the right pitot mast apply?
• How is the air stream adjusted at the eye-ball outlets?
• Which components receive bleed air from the pneumatic system?
• The fire detection system TEST SWITCH provides which signal during testing?
• Which statement correctly describes cross feed authorization?
• Where is the switch for the strobe light located?
• The gear nose actuator is driven by which transmission component?
• How are the threshold and aisle lights turned on?
• After lift off, if an auto feather is initiated, the immediate requirement is to?
• When selected to the 100% mode, the number of crew masks in use should be for computing oxygen duration?
• Prior to B-1444, except 1439, what backup operation must be used for the engine inertial vanes in case of electromechanical failure?
• When the LDG GEAR CONT switch is moved UP, which of the following occurs?
• Recirculated air passes through which ducts?
• In a pneumatic system failure, which possibilities may illuminate the warning lights?
• Which statement about the de-ice boots is true?
• Prior to B.B.-1444, except 1439, radiant heating should be used in which mode?
• Opening ambient air valves gradually, one at a time, is done to avoid what?
• What action is recommended when ITT exceeds 750 degrees C at LO IDLE?
• If the fuel gages read a total of 603 LBS after the previous flight, how many gallons of fuel can be added for the next flight?
• What is the cooling capacity of the aircraft with the aft evaporator installed?
• If there is a loss of electrical power to the timer of the wing and horizontal stabiliser boots while they are inflated, what will happen?
• What voltage is used to start the landing gear pump motor when the LDG GEAR CONT is UP?
• When the de-ice boots are automatically cycled, what is the timer sequence?
• Where is the baggage area light switch located?
• What happens when the FLAP handles are moved from DOWN to the APPROACH position?
• What heats the engine air intake lips during engine operation?
• Where is the switch for the strobe light located?
• Which of the following is a function of the electric stand by boost pump?
• What is the combined weight of baggage and refreshments?
• If a chip detector light illuminates and engine instruments show normal readings, what is the recommended action?
• To illuminate the CAUT LGNG OFF light on 200 models, what action must be taken?
• Which of the following is not affected when the cross feed switch is moved to the right or left?