C208 Caravan Multiple Choice Questions

151 Questions | Total Attempts: 1208

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Aircraft Quizzes & Trivia

The Cessna 208 caravan is an American single engine turboprop, fixed with tricycle landing gear and seats nine passengers with a single pilot although with the FAR part 23 waivers it can seat up to 14 passengers. Take the C208 caravan multiple-choice questions below and learn more about it.


Questions and Answers
  • 1. 
    Vortex Generators on top of the Horizontal stabilizer serves what purpose?
    • A. 

      The vortex generators enhance the nose down elevator trim authority.

    • B. 

      Increases effectiveness of controls.

    • C. 

      Increases STOL/MTOW

    • D. 

      Provide enhaced lateral stability

    • E. 

      All of the above

  • 2. 
    When a Caravan is equipped with a lead acid Battery. How many volt/Amperes is the Battery rated as? 
    • A. 

      40 volt 40 Ampere-hour

    • B. 

      24 Volt 45 Ampere-hour

    • C. 

      24 Volt 40 Ampere-hour

  • 3. 
    The starter-Generator is rated as how many ampere-hour?
    • A. 

      28 volt, 200 Ampere-Hour

    • B. 

      24 volt, 200 Amper-Hour

    • C. 

      24 volt, 150 Ampere- Hour

  • 4. 
    How many General Buses AND Avionics buses does a C208 have?
    • A. 

      2

    • B. 

      4

    • C. 

      6

  • 5. 
    How many Nav lights does a C208 Have?
    • A. 

      1

    • B. 

      2

    • C. 

      3

  • 6. 
    • A. 

      Decreases speed of aircraft

    • B. 

      Improves lateral control of aircraft at Low airspeed

    • C. 

      Primarily turns the aircraft

  • 7. 
    The CSU and Brakes is actuated how?
    • A. 

      Pneumatically

    • B. 

      Hydraulically

    • C. 

      Cable

  • 8. 
    How is rudder trimming achieved?
    • A. 

      Through Cabling that goes directly to the rudder

    • B. 

      Through cabling that goes to the Rudder trim tab

    • C. 

      Through the nosewheel steering bungee(not a tab)

  • 9. 
    • A. 

      Higher service life

    • B. 

      It absorbes voltage spikes

    • C. 

      Cheaper

    • D. 

      Short recharge time

    • E. 

      All of the above

  • 10. 
    What advantages does a Nicad Battery have over a Lead Acid Battery?
    • A. 

      Good starting capability

    • B. 

      Cheaper

    • C. 

      Higher service life

    • D. 

      Short recharge time

    • E. 

      All of the above

  • 11. 
    Above How many Ng does the GCU provide automatic cut-off?
    • A. 

      48%

    • B. 

      52%

    • C. 

      46%

  • 12. 
    The GCU controls the starter-Generator and serves what functions?
    • A. 

      Overspeed protection

    • B. 

      Speed sensor

    • C. 

      Starter cut out

    • D. 

      Voltage regulation and protection from high voltage + reverse current

    • E. 

      All of the above

  • 13. 
    14.) When will the Generator be disconnected from the Buses?
    • A. 

      In the vent of a high voltage situation only

    • B. 

      In the event of a high voltage or reverse current situation

    • C. 

      In the event of a reverse current situation only

  • 14. 
    How is the starter/generator cooled?
    • A. 

      By an integral fan

    • B. 

      Blast tube above the oil cooler, in the air inlet on the right forward cowling.

    • C. 

      Fuel heat exchanger

    • D. 

      A and B

    • E. 

      A, B and C

  • 15. 
    If the gound plug receptacle is plugged in(with power ON) and Battery is ON aswell, will the ground plug receptacle overpower the electrical system and cause a short?
    • A. 

      Yes

    • B. 

      No

  • 16. 
    What is the purpose of the Ground  power monitor? Page 2-6 Flight safety
    • A. 

      Senses the voltage level applied to the external power receptacle

    • B. 

      Senses the airplane bus voltage and illuminates the “voltage low” annunciator (below 24.5 volts system voltage)

    • C. 

      A and B

  • 17. 
    When the battery Voltage is below 20 volts (Before start). Will the Battery contactor be connected to the distribution bus, internal start contactor, Generator contactor?
    • A. 

      Yes

    • B. 

      No

  • 18. 
    With the Starter switch in the “motor” / “start” position during flight/start sequence. Will the Generator come online?
    • A. 

      Yes

    • B. 

      No

  • 19. 
    As per the POH. At how many %Ng must the starter switch be placed in the “OFF” position during the start cycle
    • A. 

      42%

    • B. 

      46%

    • C. 

      48%

    • D. 

      50%

    • E. 

      52%

  • 20. 
    • A. 

      I tconnects the 2 electrical busses together

    • B. 

      It connects the 2 avionics busses together

    • C. 

      It connects the 2 avionics busses when the Generator has gone offline and the Standby power(Alternator) is operational

  • 21. 
    With Regard to the external power switch. When the “starter” side is selected, External power is applied to the……..? Page 2-15 Flight safety
    • A. 

      Starter motor only

    • B. 

      Starter and main bus

    • C. 

      Starter, main bus and Battery

  • 22. 
    With Regard to the external power switch. When the “Bus” side is selected External power is applied to the……..? Page 2-15 Flight safety
    • A. 

      Starter motor only

    • B. 

      Main bus only

    • C. 

      Starter and main bus

    • D. 

      Starter, main bus and Battery

  • 23. 
    Is it recommended to charge The Battery with external power(By switiching on the Battery switch and switching the external power switch to “BUS”)?
    • A. 

      Yes

    • B. 

      No

  • 24. 
    If a CB pops after how many minutes will you reset that CB(at the engine/inside the cockpit)?(As per the flight safety manual page 2-15)
    • A. 

      1

    • B. 

      2

    • C. 

      3

  • 25. 
    Below what Voltage will the standby electrical system (Alternator) supply power to the system?
    • A. 

      24 volt

    • B. 

      24.5 volts

    • C. 

      27.5 volts

  • 26. 
    When the stanby power goes ON during flight(Gene goes offline). What will your initial actions be to maintain comms/avionics(After tripping and reseting the Generator)?
    • A. 

      Switch On “avionics bus tie”

    • B. 

      Switch On “avionics stanby power”

    • C. 

      Switch On “avionics stanby power” and “avionics bus tie”

  • 27. 
    How do you check the standby electrical system?(As per the POH)
    • A. 

      “Trip” the generator

    • B. 

      Selector knob “ALT” observe a 1 volt drop between “GEN” and “ALT”

    • C. 

      A and B

  • 28. 
    When should the strobe light be used(strictly speaking)? (As per the flight safety manual)
    • A. 

      At night

    • B. 

      At day and Night

    • C. 

      At day

  • 29. 
    When is it not recommended to use the strobe light?
    • A. 

      On the ground

    • B. 

      In fog

    • C. 

      In haze

    • D. 

      In precipitation

    • E. 

      All of the above

  • 30. 
    When is it not recommended to use the flashing beacon?
    • A. 

      Flying through haze

    • B. 

      Flying through Precipitation

    • C. 

      Flying through clouds/overcast conditions

    • D. 

      All of the above

    • E. 

      A and C

  • 31. 
    • A. 

      “Cabin” toggle switch on the lighting control panel

    • B. 

      Rocker switch just forward of the air stair door

    • C. 

      All of the above

  • 32. 
    How do you control the intensity of the annunciator lamps?
    • A. 

      By selecting “day/night” switch to” night”(All green annunciators will be dimmed and some Amber annunciators)

    • B. 

      By turning the “Eng inst” rheostat, the intensity can be changed.

    • C. 

      A and B

  • 33. 
    All annunciator panel lamps can be replaced by one another, except which annunciator? (which has a different bulb – Page 4-2 Flight safety manual)
    • A. 

      “Ignition ON”

    • B. 

      "Starter energized"

    • C. 

      "oil pressure low"

    • D. 

      All of the above

  • 34. 
    How many lamps does each light assembly contain?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      They don't have lights

  • 35. 
    Below what oil pressure will the “oil pressure low” annunciator come on?
    • A. 

      40 PSI

    • B. 

      38 PSI

    • C. 

      40 +/- 2 PSI

    • D. 

      35 PSI

  • 36. 
    When the “fuel Press low” light goes on. What pressure is available in the fuel manifold?
    • A. 

      4.75 PSI

    • B. 

      4.25 PSI

    • C. 

      2.75 PSI

    • D. 

      5 PSI

  • 37. 
    When the” voltage Low” annunciator comes on, electrical system bus voltage has dropped below how many volts?
    • A. 

      27.5 volts

    • B. 

      24.5 volts

    • C. 

      25 volts

    • D. 

      24 volts

  • 38. 
    When the “vacuum Low” annunciator comes on. Suction has dropped below what pressure?
    • A. 

      4.5 In HG

    • B. 

      4.0 In HG

    • C. 

      3.5 In HG

    • D. 

      3.0 In HG

    • E. 

      2.5 In HG

  • 39. 
    When the “fuel reservoir Low” light comes on. How full is the reservoir?
    • A. 

      Just below full

    • B. 

      3/4 full

    • C. 

      2/4 full

    • D. 

      1/4 full

    • E. 

      Empty

  • 40. 
    When the lef/right fuel low annunciator comes on. How much fuel is left in the Rh/LH tank?
    • A. 

      20 Gallons

    • B. 

      25 Gallons

    • C. 

      30 Gallons

    • D. 

      35 Gallons

    • E. 

      Half full or less

  • 41. 
    When the “door warning annunciator” comes on, what does that mean?
    • A. 

      Uppr aft passenger door is open

    • B. 

      Upper aft cargo door is open

    • C. 

      Upper aft cargo door or passenger door is open

    • D. 

      Lowe aft passenger door is open

    • E. 

      Lower aft cargo door is open

  • 42. 
    If the chip detector light comes on, what does it mean?
    • A. 

      Metal chips have been detected in either the reduction gearbox or accessory gearbox.

    • B. 

      Metal chips have been detected in the reduction gearbox

    • C. 

      Metal chips have been detected in the accessory gearbox

  • 43. 
    If  the “fuel selector off” annunciator comes on, what does it mean?
    • A. 

      One or Both fuel selectors are placed in the off position

    • B. 

      The” fuel selector warning” CB is not set or the” start control” CB is not set

    • C. 

      A and B

  • 44. 
    How many fuel selector warning horns does the Caravan have?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      4

    • E. 

      5

  • 45. 
    How many fuel nozzle assemblies does the C208 have?
    • A. 

      14

    • B. 

      7

    • C. 

      2

  • 46. 
    The fuel shut off valves is AKA.....
    • A. 

      Fuel selectors

    • B. 

      Fuel manifold

    • C. 

      Fuel boost pump

  • 47. 
    Where is the ejector pump + electrical auxillary boost pump situated?
    • A. 

      Just before the fuel manifold

    • B. 

      Just before the firewall shut off valve

    • C. 

      Inside the fuel reservoir tank

  • 48. 
    How does the fuel get to the reservoir manifold(to get to the engine driven boost pump)?
    • A. 

      By ejector pump

    • B. 

      Auxiliary boost pump

    • C. 

      By both ejector pump and Auxiliary boost pump

  • 49. 
    What drives the ejector pump?
    • A. 

      It is self driven

    • B. 

      It is driven by engine

    • C. 

      It is driven by Engine driven fuel pump

    • D. 

      It is driven by Auxilliary fuel fuel pump

  • 50. 
    If the ejector boost pump fails, will the auxiliary boost pump come on automatically, If fuel boost pump is in the "Normal" position?
    • A. 

      No

    • B. 

      Yes

  • 51. 
    If the fuel filter bypass flag pops out(fuel filter blocked). Will the fuel still be filtered?
    • A. 

      Yes

    • B. 

      No

  • 52. 
    What is the purpose of oil-fuel heater?
    • A. 

      To heat oil

    • B. 

      To ensure that water particles that are held in suspension in fuel do not freeze.

    • C. 

      To cool oil

    • D. 

      B and C

    • E. 

      To ensure better combustion of fuel

  • 53. 
    55.) Fuel quantity is measure by how many fuel quantity transmitters in total?
    • A. 

      8

    • B. 

      4

    • C. 

      2

    • D. 

      16

  • 54. 
    What is the purpose of the FCU?
    • A. 

      To meter the fuel

    • B. 

      Directs fuel to flow divider

    • C. 

      To pump fuel

    • D. 

      A, B and C

    • E. 

      A and B only

  • 55. 
    Fuel Venting is achieved by?
    • A. 

      Fuel Caps

    • B. 

      Check valve equipped vent lines

    • C. 

      Vent lines

  • 56. 
    When parked on a slope. When will fuel transfer from one tank to another?
    • A. 

      If the higher wing tank's selector is in the "ON" position

    • B. 

      If the lower wing tank's selector is in the "ON" position

    • C. 

      When either the low or hihg wing tnak's selector is in the "ON" position

  • 57. 
    During start if one of the fuel selectors L or R are off. Will an aural warning + fuel selector off anaunciator go off?
    • A. 

      Yes

    • B. 

      No

  • 58. 
    Is it possible to start,Taxi, Take -off with both fuel selectors off, only running off the Fuel reservoir tanks?
    • A. 

      Yes

    • B. 

      No

  • 59. 
    If the "FUEL SELECT OFF WARN" CB and the "START CONT" CB has been pulled, will the "FUEL SELECTOR OFF" annunciator come on?
    • A. 

      Yes

    • B. 

      No

  • 60. 
    Past how many Degrees of turn will you damage the Nose gear? (Max amount of degrees you can turn)
    • A. 

      52 degree

    • B. 

      54 degrees

    • C. 

      56 degrees

    • D. 

      58 degrees

    • E. 

      60 degrees

  • 61. 
    Before the 1st flight of the day and after refuelling. Which points must you strain fuel?
    • A. 

      Fuel tank sump quick drain valves(2 valves)

    • B. 

      Fuel reservoir quick drain valve

    • C. 

      Fuel filter quick drain valves

    • D. 

      All of the above

  • 62. 
    If the gear is not locked in the center position and the nose gear is not extended fully. Will you be able to use the rudder trim?
    • A. 

      Yes

    • B. 

      No

  • 63. 
    When is the stall warning activated?
    • A. 

      At the stall

    • B. 

      2kts before the stall

    • C. 

      5-10 kts before the stall

    • D. 

      4-8 kts before the stall

  • 64. 
    If the inertial seperator is in the normal position(Not bypass), If a stone passes through the system will it go into the compressor section?
    • A. 

      Yes

    • B. 

      No

  • 65. 
    What helps to cool oil during ground Ops?
    • A. 

      Primary exhaust system

    • B. 

      Secondary exhaust system

    • C. 

      Primary oil cooler

    • D. 

      Secondary oil cooler

  • 66. 
    When a Lead acid battery is fitted, is there any Battery overheat warning system?
    • A. 

      Yes

    • B. 

      No

  • 67. 
    If I overfill the C208 oil to over "MAX COLD" or "MAX COLD", what might the consequences be?
    • A. 

      Increased oil consumption

    • B. 

      Increased oil mist passing through engine oil breather

    • C. 

      Nothing will happen

    • D. 

      Decreased oil consumption

    • E. 

      A and B

  • 68. 
    What is the maximum operating altitude limitation(Ground OPS) for the C208 from sea level to 5000ft? (Degrees celsius)
    • A. 

      +47

    • B. 

      +49

    • C. 

      +51

    • D. 

      +53

    • E. 

      +55

  • 69. 
    What is the maximum OAT(Ground OPS) limit for the C208 from 5000ft and above?
    • A. 

      There is no limit

    • B. 

      ISA +27 degrees Celsius

    • C. 

      ISA +37 degrees Celsius

    • D. 

      ISA +47degrees Celsius

    • E. 

      ISA +52 degrees Celsius

  • 70. 
    What is the maximum luggage(LBS) that can be stored aft of the rearmost row of seats?
    • A. 

      275

    • B. 

      300

    • C. 

      325

    • D. 

      350

    • E. 

      375

  • 71. 
    What is the combined load carrying capacity of the Cargo pods on a C208?
    • A. 

      790

    • B. 

      890

    • C. 

      990

    • D. 

      1090

    • E. 

      1190

  • 72. 
    The Vortex generators on the C208, what are their functions?
    • A. 

      They Provide enhanced lateral stability

    • B. 

      Reduce stall speed

    • C. 

      Increases STOL

    • D. 

      Re-energizes boundary layer

    • E. 

      All of the above

  • 73. 
    How many elevator trim tabs does a C208 have?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      4

    • E. 

      None

  • 74. 
    Vso on a C208 is?
    • A. 

      45 KIAS

    • B. 

      50 KIAS

    • C. 

      55

    • D. 

      60

    • E. 

      63

  • 75. 
    What is Vs on C208
    • A. 

      45

    • B. 

      50

    • C. 

      55

    • D. 

      60

    • E. 

      63

  • 76. 
    What is the maximum speed that you are allowed to fly with 30 degrees of flap?
    • A. 

      No limit

    • B. 

      125 KIAS

    • C. 

      150 KIAS

    • D. 

      175 KIAS

    • E. 

      200 KIAS

  • 77. 
    What can be the consequences if the power lever is retarded below IDLE into Beta during flight?
    • A. 

      Engine might overspeed

    • B. 

      Loss of airplane control

    • C. 

      A and B

  • 78. 
    What is the maximum cruise power setting for the C208?
    • A. 

      685 degrees celsius

    • B. 

      740 degrees celsius

    • C. 

      765 degrees celsius

    • D. 

      805 Degrees celsius

    • E. 

      There is no limitation

  • 79. 
    When you are Tq limited for T/O(Less than 1865ft/LBS as per T/O graphs). Will you be able to get 675 SHP out of the engine during T/O?
    • A. 

      Yes

    • B. 

      No

  • 80. 
    What is the maximum allowable ITT for T/O?
    • A. 

      740 degrees celsius

    • B. 

      765 degrees celsius

    • C. 

      805 degrees celsius

    • D. 

      850 degrees celsius

    • E. 

      There is no limit

  • 81. 
    If a stall warnig goes off on the ground. What could you do to disconnect the stall warning from the circuit(getting rid of the nuisance temporarily)?
    • A. 

      Press yoke forward

    • B. 

      Pull back on control column

    • C. 

      There is nothing you can do about a situation like that

  • 82. 
    Ng is a % of how many RPM?
    • A. 

      32500 RPM

    • B. 

      35000 RPM

    • C. 

      37500 RPM

    • D. 

      40000 RPM

    • E. 

      42500 RPM

  • 83. 
    What is the maximum climb power allowed for the C208?
    • A. 

      740 degrees celsius and 101.6%

    • B. 

      765 degrees celsius and 101.6%

    • C. 

      805 degrees celsius and 101.6%

    • D. 

      850 degrees celsius and 101.6%

    • E. 

      There is no limit

  • 84. 
    What is the maximum continuous power (ITT) for the C208?
    • A. 

      740 Degrees celsius, Tq 1865ft/Lbs, 101.6%

    • B. 

      765 Degrees celsius, Tq 1865ft/Lbs, 101.6%

    • C. 

      805 Degrees celsius, Tq 1865ft/Lbs, 101.6%

    • D. 

      850 Degrees celsius, Tq 1865ft/Lbs, 101.6%

    • E. 

      There is no limit

  • 85. 
    When is Maximum continous power used?
    • A. 

      During T/O

    • B. 

      During Cruise(to achieve highest TAS possible)

    • C. 

      In extreme icing conditions

    • D. 

      Winshear downdraughts

    • E. 

      C and D

  • 86. 
    Is the 20kts Maximum demonstrated crosswind velocity in the POH a limitation on the C208?
    • A. 

      Yes

    • B. 

      No

  • 87. 
    Can the fuel selector warning horns go off simultaneously?
    • A. 

      No

    • B. 

      Yes

  • 88. 
    Can you as pilot reset the fuel filter bypass flag(after the flag has popped out)?
    • A. 

      No

    • B. 

      Yes

  • 89. 
    What can happen if the fuel can drain is not drained after Flight(6 shut downs)?
    • A. 

      Can will overflow its contents overboard automoatically

    • B. 

      Fuel can drain lines can burst by the 7th flight

    • C. 

      Nothing will happen

  • 90. 
    On a C208 with full reverse thrust selected for the landing. The ground roll will be decreased by how many %?
    • A. 

      5

    • B. 

      10

    • C. 

      15

    • D. 

      20

    • E. 

      25

  • 91. 
    With a right quartering crosswind from behind, Beta mode should not be selected for more than how many seconds in a parked position?
    • A. 

      20 secs

    • B. 

      25 secs

    • C. 

      30 secs

    • D. 

      35 secs

    • E. 

      A right quartering crosswind from behind could never damage the cargo pod

  • 92. 
    Below +4 degrees celsius with visible moisture, should the Inertial seperator be put into the BYPASS postion? (As per POH)
    • A. 

      Yes

    • B. 

      No

  • 93. 
    If No ITT rise is observed within ____ secs from the time the condition lever is moved into the Low idle position from cut off, the Condition lever should be moved to the cut off position  and engine start aborted.
    • A. 

      2 secs

    • B. 

      4 secs

    • C. 

      6 secs

    • D. 

      8 secs

    • E. 

      10 secs

  • 94. 
    Are you allowed to move the condition lever into a intermediate position between Low idle and High Idle? (As per flight safety manual)
    • A. 

      Yes

    • B. 

      No

  • 95. 
    If during start you monitor the Ng gauge, Ng shoots past 20%. Will continue the start adding in fuel?
    • A. 

      I will continue the start

    • B. 

      I will discontinue start

  • 96. 
    Below what degrees Fahrenheit is an APU start not recommended?
    • A. 

      -20

    • B. 

      0

    • C. 

      20

    • D. 

      40

    • E. 

      There is no temperature limitations on start with a APU

  • 97. 
    What is the minimum Ng for Idle
    • A. 

      46%

    • B. 

      48%

    • C. 

      50%

    • D. 

      52%

    • E. 

      There is no minimum

  • 98. 
    What is the maximum ITT at Idle power lever?
    • A. 

      685 Degrees celsius

    • B. 

      740 Degrees celsius

    • C. 

      765 Degrees celsius

    • D. 

      805 Degrees celsius

    • E. 

      There is no limit

  • 99. 
    What is the maximum Tq allowable at 1800 RPM
    • A. 

      1825

    • B. 

      1865

    • C. 

      1900

    • D. 

      1970

    • E. 

      2090

  • 100. 
    What is the maximum Tq allowable at 1900 RPM
    • A. 

      1825

    • B. 

      1865

    • C. 

      1900

    • D. 

      1970

    • E. 

      2090

  • 101. 
    What is the maximum bank angle on a C208?
    • A. 

      45

    • B. 

      60

    • C. 

      75

    • D. 

      90

    • E. 

      There is no maximum

  • 102. 
    With the "FUEL LOW" annunciator ON. What is the maximum full rudder slip time allowable?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      4

    • E. 

      There is no maximum time allowable

  • 103. 
    When using any Avgas in any way on a C208. What is the limitation on OAT for Take off?
    • A. 

      +25 degrees celsius

    • B. 

      +29 degrees celsius

    • C. 

      + 33 degrees celsius

    • D. 

      + 37 degrees celsius

    • E. 

      There is no limitation

  • 104. 
    When using any Avgas in any way on a C208. What is the limitation on operating Altitude?
    • A. 

      7000 ft

    • B. 

      8000 ft

    • C. 

      9000 ft

    • D. 

      10000 ft

    • E. 

      11000ft

  • 105. 
    When using any Avgas in any way on a C208. Should the auxilliary Boost Pump be On for all flight operations?
    • A. 

      Yes

    • B. 

      No

  • 106. 
    What is the oil capacity for a C208?
    • A. 

      9.5 Qts

    • B. 

      10.5 QTS

    • C. 

      12 Qts

    • D. 

      14 Qts

    • E. 

      16 Qss

  • 107. 
    What is the maximum glide speed of a C208 at 8750 LBS equipped with Cargo pods?
    • A. 

      104 KIAS

    • B. 

      100 KIAS

    • C. 

      95 KIAS

    • D. 

      87 KIAS

    • E. 

      79 KIAS

  • 108. 
    What is the maximum glide speed of a C208 at 7500 LBS equipped with Cargo pods?
    • A. 

      104 KIAS

    • B. 

      100 KIAS

    • C. 

      95 KIAS

    • D. 

      87 KIAS

    • E. 

      79 KIAS

  • 109. 
    What is the maximum glide speed of a C208 at 6250 LBS equipped with Cargo pods?
    • A. 

      104 KIAS

    • B. 

      100 KIAS

    • C. 

      95 KIAS

    • D. 

      87 KIAS

    • E. 

      79 KIAS

  • 110. 
    What is the manuevring speed of a C208 at 8750 LBS ?
    • A. 

      148 KIAS

    • B. 

      143 KIAS

    • C. 

      137 KIAS

    • D. 

      125 KIAS

    • E. 

      112 KIAS

  • 111. 
    What is the manuevring speed of a C208 at 7500 LBS ?
    • A. 

      148 KIAS

    • B. 

      143 KIAS

    • C. 

      137 KIAS

    • D. 

      125 KIAS

    • E. 

      112 KIAS

  • 112. 
    What is the manuevring speed of a C208 at 6250 LBS ?
    • A. 

      148 KIAS

    • B. 

      143 KIAS

    • C. 

      137 KIAS

    • D. 

      125 KIAS

    • E. 

      112 KIAS

  • 113. 
    What is the manuevring speed of a C208 at 5000 LBS ?
    • A. 

      148 KIAS

    • B. 

      143 KIAS

    • C. 

      137 KIAS

    • D. 

      125 KIAS

    • E. 

      112 KIAS

  • 114. 
    What is Vy on a C208(SL to 10000ft)?
    • A. 

      115-120 KIAS

    • B. 

      104 KIas

    • C. 

      92 KIAS

    • D. 

      72 KIAS

  • 115. 
    What is Vx on a C208? (SL to 20000ft)
    • A. 

      115 - 120 KIAS

    • B. 

      104 KIAS

    • C. 

      92 KIAS

    • D. 

      72 KIAS

  • 116. 
    What is the definition of a "Hot start"(as per POH)?
    • A. 

      A start exceeding 805 Degrees celsius ITT

    • B. 

      A start where the ITT peaks just below 1090 Degrees celsius ITT

    • C. 

      A start that reaches 1090 Degrees celsius ITT

    • D. 

      A start exceeding 1090 Degrees celsius ITT

  • 117. 
    What is the maximum window open speed on the C208?
    • A. 

      200 KIAS

    • B. 

      175 KIAS

    • C. 

      150 KIAS

    • D. 

      125 KIAs

    • E. 

      There is no limitation

  • 118. 
    What is Vmo(maximum operating speed on the C208)?
    • A. 

      200 KIAS

    • B. 

      175 KIAs

    • C. 

      150 KIAS

    • D. 

      125 KIAs

    • E. 

      250 KIAS

  • 119. 
    The maximum Transient Tq on the C208 is_____? And Limited to how many secs _____?
    • A. 

      2040, 2 secs

    • B. 

      2400, 20secs

    • C. 

      2000, 30 secs

    • D. 

      1865, 4 secs

  • 120. 
    What is the maximum Transient ITT on the C208?
    • A. 

      765

    • B. 

      805

    • C. 

      850

    • D. 

      1090

  • 121. 
    What is the maximum Ambient Ng for the C208?
    • A. 

      101.6%

    • B. 

      102.6%

    • C. 

      103.6%

    • D. 

      104.6%

  • 122. 
    What is the maximum ambiet Prop RPM for the C208?
    • A. 

      1900 RPM

    • B. 

      2000 RPM

    • C. 

      2090 RPM

    • D. 

      2200 RPM

    • E. 

      2400 RPM

  • 123. 
    With the Fuel quantity indicator indicating empty. How much unuseable fuel is lef in the tanks?
    • A. 

      0.5 Gal

    • B. 

      1.5 Gal

    • C. 

      2.5 Gal

    • D. 

      3.5 Gal

    • E. 

      4.5 Gal

  • 124. 
     The fuel tank selectors located on the overhead panel:
    • A. 

      Are BOTH normally on for flight

    • B. 

      Are BOTH Normally off during refueling

    • C. 

      Are turned off during ground OPS

    • D. 

      A and B

  • 125. 
    Fuel is primarily pumped form the Reservoir tank primarily by the:
    • A. 

      Ejector boost pump

    • B. 

      Auxiliary boost pump

    • C. 

      Engine driven fuel pump

    • D. 

      FCU

  • 126. 
    When the rudder pedals is depressed(fully without brakes), during taxiing on the ground. How many degrees will the steering bungee turn the nose wheel?
    • A. 

      10 degrees either side of centre

    • B. 

      15 degrees either side of centre

    • C. 

      20 degrees either side of centre

    • D. 

      25 degrees either side of centre

    • E. 

      30 degrees either side of centre

  • 127. 
    On the newer models of C208. To unlock the Rudder gust lock if you forgot to unlock it during the preflight(rear of the aircrft near to the Rudder). You will....
    • A. 

      Press yoke forward

    • B. 

      Pull back on yoke to the fully aft position

  • 128. 
    After the Master switch is turned OFF(After shut down), If you forget to switch of the STANDBY POWER switch. What will happen?
    • A. 

      Nothing

    • B. 

      Several of the Amber annunciator will stay ON

    • C. 

      Several of the red annunciators will stay ON

    • D. 

      All of the annunciators will stay ON

  • 129. 
    During a Balked laning. When must the first 30 degrees of flaps be retracted?
    • A. 

      Immediatly after iniating the go-around(before applying power)

    • B. 

      Immediatly after iniating the go-around(after applying go-around power)

    • C. 

      When positive rate of climb is established and power is applied

    • D. 

      100ft above iniating the go-around(well into the go-around)

    • E. 

      None of the above

  • 130. 
    How many axial compressor stages does a PT6A have?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      4

    • E. 

      5

  • 131. 
    How many Centrifugal Compressor stages does a PT6A have?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      4

    • E. 

      5

  • 132. 
    If the power lever is moved aft of the IDLE position without engine running and the props feathered. Can any damage be done?
    • A. 

      Yes

    • B. 

      No

  • 133. 
    Failure of any Pneumatic signal input will result in the Ng dropping to _____?
    • A. 

      48% Ng

    • B. 

      50% Ng

    • C. 

      52% Ng

    • D. 

      65% Ng

    • E. 

      Minimum idle Ng

  • 134. 
    Is it desireable for the front section of the engine(prop etc.) to rotate after engine has shut down?
    • A. 

      Yes

    • B. 

      No

  • 135. 
    High Idle on the fuel condition lever is how many Ng?
    • A. 

      48%

    • B. 

      50%

    • C. 

      52%

    • D. 

      62%

    • E. 

      65%

  • 136. 
    Is there any lights outside the C208, which are controlled by any switches which are not inside the cockpit (left hand side of the control column)?
    • A. 

      Yes

    • B. 

      No

  • 137. 
    Which engine instruments are not electrically operated(please choose 2)?
    • A. 

      Prop RPM

    • B. 

      ITT indicator

    • C. 

      Ng% indicator

    • D. 

      Oil pressure

    • E. 

      FF

  • 138. 
    How many igniters does a PT6A engine have?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      4

    • E. 

      5

  • 139. 
    The "ON" position of the ignition switch is used when(Choose the correct ones)?
    • A. 

      Air start without starter assist

    • B. 

      Operation on water-covered runways

    • C. 

      During flight in heavy precipitation

    • D. 

      During inadvertent icing encounters with Inertial seperator for 5 mins

    • E. 

      When a near fuel exhaustion exists ("RESERVOIR FUEL LOW")

  • 140. 
    Does the compressor air inlet filter air?
    • A. 

      Yes

    • B. 

      No

  • 141. 
    How many exhausts does a C208 have?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      4

    • E. 

      5

  • 142. 
    How many fuel filters does a C208 have?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      4

    • E. 

      5

  • 143. 
    The ITT sensing system is situated where?
    • A. 

      Just before the Turbine section

    • B. 

      Just before the Compressor section

    • C. 

      Behind the Turbine section

    • D. 

      Near the exhaust

    • E. 

      Between the Power turbine and Compressor turbine

  • 144. 
    How many overspeed Governors does the C208 have?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      4

    • E. 

      5

  • 145. 
    As per the POH. How often should the oil breather can drain be drained?
    • A. 

      After every flight

    • B. 

      After every 3 flights

    • C. 

      After every 6 flight

    • D. 

      Never

    • E. 

      After the last shut down of each day

  • 146. 
    If the engine oil pressure drops suddenly(engine fails) and you don't feather the props. Will the Props feather themselves?
    • A. 

      Yes

    • B. 

      No

  • 147. 
    Is the EPA CAN(fuel drain can) fireproof?
    • A. 

      Yes

    • B. 

      No

  • 148. 
    When should the avionics power switches be off?
    • A. 

      Prior to turning ON the battery switch

    • B. 

      Prior to starting the engine

    • C. 

      Before applying external power source

    • D. 

      All of the above

  • 149. 
    With the Cabin heat firewall knob in the OFF position and the mixing air control in the GRD position. Can a compressor stall happen at High power setttings?
    • A. 

      Yes

    • B. 

      No

  • 150. 
    With the Cabin heat firewall knob in the OFF position and the mixing air control in the GRD position. Can a compressor stall happen at Low power setttings?
    • A. 

      Yes

    • B. 

      No

  • 151. 
    What function does the static dischargers serve on the C208?
    • A. 

      To To improve radio communication through rain

    • B. 

      To improve radio communication through Dust

    • C. 

      To improve radio communication through snow

    • D. 

      To improve radio communication through ice crystals

    • E. 

      All of the above