Airplane Test Part 1

95 Questions

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Airplane Quizzes & Trivia

Self test questions for 2A553B Vol 5. This is part 1. Ask me for the link for part 2.


Questions and Answers
  • 1. 
    What are the flight spoilers designed to do?
    • A. 

      Provides lateral and longitudinal movement.

    • B. 

      Augment the ailerons, improving roll control.

    • C. 

      Decrease airspeed on landing.

    • D. 

      Augment the horizontal stabilizers, improving roll control.

  • 2. 
    What's the maximum spoiler travel from the 3 degree up-rigged position
    • A. 

      57 degrees up and 2 degrees down

    • B. 

      53 degrees up and 3 degrees down

    • C. 

      58 degrees up and 3 degrees down

    • D. 

      Spoilers can't move from the 3 degree up-rigged position

  • 3. 
    How much force is required to shear the shear pin in the interconnect rod?
    • A. 

      40 pounds

    • B. 

      38 pounds

    • C. 

      41 pounds

    • D. 

      45 pounds

  • 4. 
    What component provides positive system centering with no force applied to the controlwheel?
    • A. 

      A centering spring

    • B. 

      A combination centering and control spring

    • C. 

      Two centering springs

    • D. 

      A combination centering and artificial feel spring

  • 5. 
    What system assists the pilot in moving the cable system?
    • A. 

      JSAF

    • B. 

      The PAC

    • C. 

      PACS

    • D. 

      FCS

  • 6. 
    How can the pilot override PACS?
    • A. 

      By momentarily depressing the PACS switch.

    • B. 

      By applying at least 20 pounds force to the control wheel

    • C. 

      By applying 40 pounds force to the control wheel

    • D. 

      By allowing the control wheel to shear the shear pin

  • 7. 
    Control column travel of 5" forward and 9" aft corresponds to how much elevator movement?
    • A. 

      15 degrees down and 26 degrees up respectively.

    • B. 

      26 degrees down and 16 degrees up respectively

    • C. 

      26 degrees down and 15 degrees up respectively

    • D. 

      16 degrees down and 26 degrees up respectively

  • 8. 
    The pilot's input system is connected to which elevators?
    • A. 

      Inboard

    • B. 

      Outboard

    • C. 

      Left positioned elevators

    • D. 

      Right positioned elevators

  • 9. 
    The co-pilots input system is connected to which elevators?
    • A. 

      Left positioned elevators

    • B. 

      Inboard

    • C. 

      Outboard

    • D. 

      Right positioned elevators

  • 10. 
    How much force is required to shear the pin in the forward interconnect rod?
    • A. 

      40 pounds

    • B. 

      180 pounds

    • C. 

      120 pounds

    • D. 

      45 pounds

  • 11. 
    How much force is required to shear the pin in the aft rod?
    • A. 

      50 pounds

    • B. 

      180 pounds

    • C. 

      40 pounds

    • D. 

      120 pounds

  • 12. 
    Artificial feel proportional to elevator surface position is provided by what springs?
    • A. 

      Centering actuator attached to co-pilots aft quadrant, and centering springs built into the power assembly

    • B. 

      Centering assembly attached to the pilots aft quadrant, and centering bungees built into the power packages

    • C. 

      Centering spring attached to the pilots aft quadrant, and centering bungees built into the power packages.

    • D. 

      Centering spring attached to the pilots aft quadrant, and centering springs built into the power packages

  • 13. 
    Whats the purpose of the bob weight?
    • A. 

      Provides the pilot with feel forces as a function of normal acceleration

    • B. 

      Provides the pilot with feel forces as a function of Qc

    • C. 

      Provides the pilot with feel forces as a function of normal airspeed

    • D. 

      Provides the pilot with feel forces as a function of abnormal acceleration

  • 14. 
    Whats the purpose of the variable feel unit?
    • A. 

      Provides the pilot with feel forces as a function of abnormal acceleration

    • B. 

      Provides the pilot with feel forces as a function of normal airspeed

    • C. 

      Provides the pilot with feel forces as a function of normal acceleration

    • D. 

      Provides the pilot with feel forces as a function of Qc

  • 15. 
    Rudder pedal travel of 3" provides how much rudder surface travel?
    • A. 

      35 degrees right of neutral

    • B. 

      35 degrees left or right of neutral

    • C. 

      32 degrees left or right of neutral

    • D. 

      30 degrees right of neutral

  • 16. 
    How can you adjust the rudder pedals?
    • A. 

      By an automatic crank for each set of pedals, located on the main instrument panel.

    • B. 

      By turning an adjustment bolt on the pedals

    • C. 

      By a manual crank for each set of pedals, located on the main instrument panel.

    • D. 

      By using the 2240 pedal adjuster

  • 17. 
    What provides positive system centering with no force applied to the rudder pedals?
    • A. 

      A preloaded bungee that applies a force of approximately 8 pounds

    • B. 

      A centering spring

    • C. 

      A preloaded bungee that applies no force

    • D. 

      A preloaded bungee that applies a force of approximately 10 pounds

  • 18. 
    What controls operation of the trim actuator?
    • A. 

      A rudder trim control switch, located on the flight deck

    • B. 

      Two rudder trim control switches, located on the center console

    • C. 

      Two roll trim control switches, located on the center console

    • D. 

      A roll trim control knob, located on the center console

  • 19. 
    How far can the rudder be trimmed?
    • A. 

      11 (+- 2.5 degrees , - 1.5 degrees) left or right of center

    • B. 

      11 (+- 1.0 degree, - 0.5 degrees) left or right of center

    • C. 

      11 (+- 1.5 degrees , - 0.5 degrees) left or right of center

    • D. 

      12 (+- 1.7 degrees, - 0.5 degrees) left or right of center

  • 20. 
    Describe the tailing edge flaps.
    • A. 

      Fowler-Type and consist of 4 panels on each wing

    • B. 

      Slotted fowler-type and consist of 6 panels on each wing

    • C. 

      Slotted fowler-type and consist of 8 panels on each wing

    • D. 

      Fowler-Type and consist of 8 panels on each wing

  • 21. 
    What constrains the input drive from each hydraulic motor to the gearbox?
    • A. 

      A spring applied single disc brake

    • B. 

      A bungee

    • C. 

      A spring applied multi disc brake

    • D. 

      Two springs

  • 22. 
    What controls hydraulic pressure for power package operation.
    • A. 

      Two actuator operated pressure valves located within a hydraulic manifold attached to the gearbox

    • B. 

      Two manually operated pressure valves located within a hydraulic manifold attached to the power package

    • C. 

      Two actuator operated shutoff valves located within a hydraulic manifold attached to the gearbox

    • D. 

      Two solenoid-operated shut-off valves located within a hydraulic manifold attached to the power package

  • 23. 
    What tells the pilot the slat system is decoupled from the flap system?
    • A. 

      Illumination of the LE SLAT BRAKE ON LIGHT on the annunciator panel.

    • B. 

      Aural warning SLAT DECOUPLED

    • C. 

      Illumination of the SLAT BRAKE LIGHT on the main console

    • D. 

      Illumination of the RE SLAT BRAKE ON LIGHT on the annunciator panel.

  • 24. 
    What indicates "in transit" on the slat position indicator?
    • A. 

      The words RETRACT

    • B. 

      The words RETRACT and EXTEND and a Barber pole

    • C. 

      The words RETRACT or EXTEND and a Barber pole

    • D. 

      The words RETRACT or EXTEND

  • 25. 
    When does the pilot deploy the ground spoilers and flight spoilers?
    • A. 

      After touchdown but after spin-up has been established

    • B. 

      Upon landing

    • C. 

      After touchdown or after main gear wheel spin-up has been established

    • D. 

      After pilot has depressed the spoiler up switch

  • 26. 
    What tells the pilot the spoiler handle is in the locked or unlocked position
    • A. 

      A switch is electromagnetically released by the locking mechanism

    • B. 

      A lever on the center console, which is connected to the locking mechanism

    • C. 

      A lever on the main console, which is connected to the spoiler handle actuator

    • D. 

      A switch on the center console, which is connected to the locking mechanism

  • 27. 
    What are the two methods of moving the horizontal stabilizer?
    • A. 

      Rotating the screw within the nut by utilizing the screw drive or rotating the nut by using the nut drive.

    • B. 

      There is no way to move the horizontal stabilizers

  • 28. 
    What are the three direct means of controlling the horizontal stabilizer pitch trim actuator?
    • A. 

      Wheel switches, Pitch trim switches, console switches

    • B. 

      Wheel switches, manual lever, pitch trim switches

    • C. 

      Wheel switches, manual lever, console switches

    • D. 

      Wheel switches, clown flip-back switch, clown stomp lever

  • 29. 
    Whats the reason for increasing the nut drive rate when the flaps are down?
    • A. 

      To provide a slower response from pitch trim during slow speed flight.

    • B. 

      To provide a more rapid response from pitch trim during slow speed flight.

    • C. 

      To avoid under-driving the flaps which have the tendency to break at high torque low speed

    • D. 

      To provide for a normal response to match flight conditions for flap movement

  • 30. 
    Describe the electric trim switches mounted on the control wheel.
    • A. 

      Finger-controlled, double throw switches spring loaded to the center off position

    • B. 

      Single pull, single throw switches, spring loaded to norm position

    • C. 

      Finger-controlled, single throw switches.

    • D. 

      Finger-controlled, double throw switches spring loaded to the center neutral position

  • 31. 
    The manual trim levers on each side of the center console operate which drive motor?
    • A. 

      The screw drive

    • B. 

      The actuator drive

    • C. 

      The winding drive

    • D. 

      The nut drive

  • 32. 
    Console switches provide the pilot or copilot a means of operating which drive motor?
    • A. 

      The actuator nut drive

    • B. 

      The servo screw drive

    • C. 

      The actuator screw drive

    • D. 

      The servo nut drive

  • 33. 
    How is pitch trim position displayed
    • A. 

      By a scale type indicator, incorporating a vernier scale graduated in degrees from -6 to +14 located on the center main instrument panel

    • B. 

      By a dial type indicator, incorporating a scale graduated in degrees from -6 to +14 located on the center main instrument panel

    • C. 

      By a dial type indicator, incorporating a scale graduated in degrees from -5 to +17 located on the center main instrument panel

    • D. 

      By a scale type indicator, incorporating a vernier scale graduated in degrees from -5 to +17 located on the center main instrument panel

  • 34. 
    What enables the nut drive to drive at two different rates?
    • A. 

      A seperate nut drive assembly

    • B. 

      A duplicate screw drive

    • C. 

      A bungee

    • D. 

      A second flow control valve

  • 35. 
    What component drives the screw drive at a predetermined rate?
    • A. 

      A constant rate drive valve

    • B. 

      A constant rate nut drive valve

    • C. 

      A flow control valve

    • D. 

      Two flow control valves

  • 36. 
    What causes the autolube mechanism to provide one stroke of grease to the autolubricator for lubrication of the jackscrew?
    • A. 

      De-pressurizing the number 2 hydraulic system

    • B. 

      Pressurizing the number 1 hydraulic system

    • C. 

      Pressurizing the number 2 hydraulic system

    • D. 

      De-pressurizing the number 1 hydraulic system

  • 37. 
    What system provides for wing sweep positioning?
    • A. 

      The secondary flight control system

    • B. 

      The primary flight control system

    • C. 

      The pilots flight control system

    • D. 

      The primary and secondary flight control system

  • 38. 
    Which control stick uses electrical signals for positioning of the horizontal stabilizers?
    • A. 

      Pilot

    • B. 

      Navigator

    • C. 

      Co-pilot

    • D. 

      Backshop wannabe flight line pansies

  • 39. 
    If the mechanical pitch control linkage is jammed, how is the pitch of the aircraft controlled?
    • A. 

      The pilot electrical positioning signals to the pitch scas controls the pitch of the aircraft

    • B. 

      The copilot electrical positioning signals to the PACS controls the pitch of the aircraft

    • C. 

      The copilot electrical positioning signals to the pitch trim actuator controls the pitch of the aircraft

    • D. 

      The copilot electrical positioning signals to the pitch scas controls the pitch of the aircraft

  • 40. 
    Are the upper and lower rudders interconnected?
    • A. 

      Yes; they're mechanically dependent

    • B. 

      No; they're mechanically independent

    • C. 

      Yes; they're electrically and mechanically depedent

    • D. 

      No; because I said so

  • 41. 
    What subsystem provides electrical control of the roll, pitch, and yaw of the aircraft?
    • A. 

      Augmented flight control

    • B. 

      Non-Augmentable flight controls

    • C. 

      FCS

    • D. 

      SCAS

  • 42. 
    If the aircraft is flying with the wings swept to 50 degrees, what's the condition of the fairings?
    • A. 

      Held in the UP position

    • B. 

      Locked in the LEVEL position

    • C. 

      Held in the DOWN position

    • D. 

      Locked in the UP position

  • 43. 
    Whats the purpose of the lift augmentation subsystem?
    • A. 

      Negates the effects of turbulence

    • B. 

      Provides for optimum lift by varying wing-sweep,wing flaps, and wing slats position.

    • C. 

      Provides for an increase in lift by varying slat position.

    • D. 

      Provides for optimum lift by varying wing flaps, and wing slats positioning

  • 44. 
    Whats the range of wing sweep that's adjustable by the pilot?
    • A. 

      Between 14 degrees and 65 degrees

    • B. 

      Between 16 degrees and 67.5 degrees

    • C. 

      Between 15 degrees and 67.5 degrees

    • D. 

      Between 14 degrees and 63.5 degrees

  • 45. 
    How is the roll control subsystem powered?
    • A. 

      Mechanically

    • B. 

      Hydraulically

    • C. 

      Electrically

    • D. 

      Manually

  • 46. 
    Which controls stick(s) can be isolated in the event of a failure?
    • A. 

      Pilot

    • B. 

      Copilot

    • C. 

      Navigators

    • D. 

      Pilot and Copilot

  • 47. 
    What are the functions of the roll forward feel bungee?
    • A. 

      Provides control stick longitudinal artificial feel and control stick longitudinal centering.

    • B. 

      Provides control stick lateral artificial feel and control stick lateral centering.

    • C. 

      Provides control stick longitudinal artificial feel and control stick lateral centering.

    • D. 

      Provides tension on the forward roll cables

  • 48. 
    What is the purpose of the roll aft feel bungee?
    • A. 

      Places and additional "feel" tension to the roll control cables

    • B. 

      Provides the other half of the total free force of the roll control system

    • C. 

      Provides for centering of the pilot control stick

    • D. 

      All of the above

  • 49. 
    Whats the purpose of the roll master servo cylinder?
    • A. 

      Amplifies the mechanical inputs hydraulicly to overcome the friction induced into the mechanical linkage at the output of the cylinder

    • B. 

      Isolates the mechanical input linkage (from the control sticks) from the roll trim and speedbrake commands(from the speedbrake/spoiler roll trim actuator).

    • C. 

      A and C

    • D. 

      None of the above

  • 50. 
    What's the purpose of the "dead band" gap in the spoiler linkage?
    • A. 

      Causes pilot over-control by requiring a 0.5" movement of the control stick before the spoiler linkage moves.

    • B. 

      Prevents pilot over-control by requiring a 0.7" movement of the control stick before the spoiler actuaor moves.

    • C. 

      Prevents pilot over-control by requiring a 0.5" movement of the control stick before the spoiler actuaor moves.

    • D. 

      Prevents pilot over-control by requiring a 0.7" movement of the control stick before the spoiler linkage moves.

  • 51. 
    What component of the roll control subsystem prevents overstressing of the control surfaces?
    • A. 

      Left and Right override/overload bungees

    • B. 

      Right override/overload bungees

    • C. 

      Left override/overload bungees

    • D. 

      Left and Right override/overload springs

  • 52. 
    What is the purpose of the left and right ganged blocking valve assemblies?
    • A. 

      The ganged blocking valve prevents the outboard servo cylinders from extending while the hydraulic systems are deactivated.

    • B. 

      The ganged blocking valve prevents the outboard servo cylinders from retracting while the hydraulic systems are deactivated.

    • C. 

      The ganged blocking valve prevents the inboard servo cylinders from extending while the hydraulic systems are deactivated.

    • D. 

      The ganged blocking valve prevents the inboard servo cylinders from extending while the hydraulic actuators are activated.

  • 53. 
    How are the outboard spoilers controlled and actuated?
    • A. 

      Electrically controlled, mechanically actuated

    • B. 

      Mechanically controlled, hydraulicly actuated

    • C. 

      Mechanically controlled, electrically actuated

    • D. 

      Electrically controlled, hydro-mechanically actuated

  • 54. 
    How many roll control transducers are contained at the base of the copilot control stick?
    • A. 

      One

    • B. 

      Four

    • C. 

      Two

    • D. 

      Three

  • 55. 
    What signals are required to be present for the spoiler controller to operate?
    • A. 

      Spoiler SW-OFF and HYD PRESS AVAILABLE

    • B. 

      Spoiler SW-ON and HYD PRESS AVAILABLE

    • C. 

      Spoiler SW-OFF and HYD PRESS ON

    • D. 

      Spoiler SW-ON and HYD PRESS ON

  • 56. 
    What's the operating voltage of the servo actuator?
    • A. 

      115 VAC

    • B. 

      400 VAC

    • C. 

      230 VAC

    • D. 

      115 VDC

  • 57. 
    What signal prevents the speedbrakes from extending the outboard spoilers?
    • A. 

      Spoiler ON

    • B. 

      Spoiler OFF and WOW

    • C. 

      Spoiler ON and WOW

    • D. 

      WOW

  • 58. 
    At what aircraft speeds are the outboard spoilers functional?
    • A. 

      Between 1 and 1.5 MACH

    • B. 

      Between 0 and 1 MACH

    • C. 

      Between 0 and 1.5 MACH

    • D. 

      Between 0 and 2 MACH

  • 59. 
    What is the function of the outboard spoiler override bungees?
    • A. 

      Prevents overloading of the control linkage actuators if more spoiler movement then is available is "requested" by the pilot or if an aerodynamic hinger movement limit occurs

    • B. 

      Prevents overloading of the control linkage actuators if more spoiler movement then is available is "supplied" by the pilot or if an aerodynamic hinger movement limit occurs

    • C. 

      Prevents overloading of the control linkages if more spoiler movement then is available is "supplied" by the pilot or if an aerodynamic hinger movement limit occurs

    • D. 

      Prevents overloading of the control linkages if more spoiler movement then is available is "requested" by the pilot or if an aerodynamic hinger movement limit occurs

  • 60. 
    What indication informs the pilot the outboard spoilers are non longer operational?
    • A. 

      SPOILER OFF lamps on the main caution panel illuminates

    • B. 

      SPOILER UNAVAILABLE lamps on the main caution panel illuminates

    • C. 

      SPOILER OFF lamps on the auxilliary caution panel illuminates

    • D. 

      SPOILER ON lamps on the main caution panel illuminates

  • 61. 
    What's the primary function of the roll trim system?
    • A. 

      Uses the outboard spoilers to provide slight adjustments to the roll flight controls to correct for situations where the aircraft tends to roll with no input from the control stick.

    • B. 

      Uses the inboard spoilers to provide slight adjustments to the roll flight controls to correct for situations where the aircraft tends to roll with no input from the control stick.

    • C. 

      Uses the inboard spoilers positioning signal to provide slight adjustments to the roll flight controls to correct for situations where the aircraft tends to roll with no input from the control stick.

    • D. 

      Uses the inboard and outboard spoiler position signals to provide slight adjustments to the roll flight controls to correct for situations where the aircraft tends to roll with no input from the control stick.

  • 62. 
    What are the available modes of roll trim?
    • A. 

      NORM

    • B. 

      NORM, ALTER and MACH

    • C. 

      ALTER and MACH

    • D. 

      NORM, ALTER, and OFF

  • 63. 
    Which control surfaces provide roll trim during aircraft speeds above 0.99 Mach?
    • A. 

      Ailerons

    • B. 

      Horizontal Stabilizers

    • C. 

      Vertical Stabilizers

    • D. 

      Spoilers and Horizontal Stabilizers

  • 64. 
    Explain the purpose of the electromagnetic brakes on the three speedbrake/spoiler roll trim actuator motors.
    • A. 

      Halts the mechanical linkage operation in the speedbrake/spoiler system

    • B. 

      Prevents motor from being overdriven and system slippage caused by vibrations induced into the speedbrake/spoiler mechanical linkages.

    • C. 

      Prevents motor drift and slippage caused by vibrations induced into the speedbrake/spoiler mechanical linkages.

    • D. 

      None of the above

  • 65. 
    What are the limits of spoiler movement at subsonic speeds?
    • A. 

      53 degrees 53 minutes

    • B. 

      57 degrees 53 minutes

    • C. 

      55 degrees 53 minutes

    • D. 

      57 degrees 57 minutes

  • 66. 
    Which spoiler is extended if the pilot commands LWD?
    • A. 

      Right inboard spoiler

    • B. 

      Left inboard spoiler

    • C. 

      Right and Left inboard spoiler

    • D. 

      Right and Left outboard spoiler

  • 67. 
    What occurs when the TTO switch is engaged?
    • A. 

      One roll trim actuator is centered

    • B. 

      Both roll trim actuators are centered

    • C. 

      Both roll trim bungees are centered

    • D. 

      One roll trim bungee is centered

  • 68. 
    Which set of rudder pedals provides nose steering input commands?
    • A. 

      One

    • B. 

      None, the nose steering input commands originate from the SCAS

    • C. 

      Both

    • D. 

      None, the nose steering input commands originate from the FSC

  • 69. 
    What type of adjustment is available for the rudder pedals?
    • A. 

      Fore and Aft positioning

    • B. 

      Fore positioning

    • C. 

      Aft positioning

    • D. 

      No adjustment, trick question

  • 70. 
    How does the overload bungee affect yaw control during normal operation?
    • A. 

      Acts like a bell crank

    • B. 

      Acts like a centering spring

    • C. 

      Acts like a push-pull rod

    • D. 

      Acts like a centering bungee

  • 71. 
    Which hydraulic systems "feed" the aft PDU?
    • A. 

      1 and 2

    • B. 

      1 and 3

    • C. 

      2 and 4

    • D. 

      1 and 4

  • 72. 
    Which actuator provides mechanical limiting of the upper rudders?
    • A. 

      Intermediate rudder actuator number 2

    • B. 

      Intermediate rudder actuator number 3

    • C. 

      Intermediate rudder actuator number 1

    • D. 

      Intermediate rudder actuator number 4

  • 73. 
    What's the purpose of the yaw limiter system?
    • A. 

      Limits the movement of the upper rudder mechanical yaw control during certain modes of aircraft operation

    • B. 

      Limits the movement of the upper and lower rudder mechanical yaw control during certain modes of aircraft operation

    • C. 

      Limits the movement of the lower rudder mechanical yaw control during certain modes of aircraft operation

    • D. 

      Illuminates the yaw limiter light

  • 74. 
    What two signals must be present for the yaw limiter to be placed into the limited mode of operation?
    • A. 

      SLAT POSITION IN

    • B. 

      SLAT POSITION OUT and L/R Main GEAR UPLOCKED

    • C. 

      SLAT POSITION IN and L/R MAIN GEAR UPLOCKED

    • D. 

      SLAT POSITION OUT and L/R MAIN GEAR DOWNLOCKED

  • 75. 
    What indication informs the pilot the rudder may not be in the limited position?
    • A. 

      YAW LIMITER annunciator lamp on the auxilliary panel illuminates

    • B. 

      Audible "RUDDER LIMIT" sounds

    • C. 

      YAW LIMITER lever on the main console moves out of detent

    • D. 

      YAW LIMITER annunciator lamp on the main caution panel illuminates

  • 76. 
    What are the rudder limits during limited mode?
    • A. 

      +- 15 degrees

    • B. 

      +- 10 degrees

    • C. 

      +- 17 degrees

    • D. 

      +- 5 degrees

  • 77. 
    Which component of the actuator motor assembly performs the actual limiting of mechanical yaw control? (QUESTIONABLE ANSWER)
    • A. 

      CAM

    • B. 

      BRAKE

    • C. 

      SPRING

    • D. 

      BUNGEE

  • 78. 
    What's the primary purpose of the yaw trim system?
    • A. 

      Provides slight adjustment to yaw flight controls to keep the nose of the aircraft pointed straight ahead without constant pressure on the rudder pedals.

    • B. 

      Trims the aircraft about the yaw axis

    • C. 

      Trims the aircraft about the roll axis

    • D. 

      Deactives the rudder control main system

  • 79. 
    What operational modes of yaw trim are available to the copilot?
    • A. 

      NORM, ALTER, and OFF

    • B. 

      NORM, ALTER, and NORM

    • C. 

      NORM and ALTER

    • D. 

      NORM, ALTER, and ON

  • 80. 
    What component is the source of yaw trim commands during the NORM mode of operation?
    • A. 

      Flight control trim panel or flight control auxilliary panel

    • B. 

      Flight control main panel or flight control secondary panel

    • C. 

      FCS

    • D. 

      SCAS

  • 81. 
    From where do the yaw trim acuator motors recieve there power?
    • A. 

      Main Transformer

    • B. 

      PCA 2453A06

    • C. 

      YAW Trim batter

    • D. 

      SCAS PCA 2453A05

  • 82. 
    What limits are imposed on the deflection of the rudders when yaw trim is activated?
    • A. 

      +- 15 degrees

    • B. 

      +- 17 degrees

    • C. 

      +- 10 degrees

    • D. 

      +- 5 degrees

  • 83. 
    Which control stick provides electrical pitch control only?
    • A. 

      Copilot

    • B. 

      Pilot

    • C. 

      Navigators

    • D. 

      Pilot and Copilot

  • 84. 
    What's the purpose of the pitch forward feel bungee?
    • A. 

      Provides control stick fore/aft (longitudinal) artifical feel and control stick longitudinal centering

    • B. 

      Provides control stick fore/aft (longitudinal) artifical feel as a function of Qc

    • C. 

      Provides control stick fore/aft (longitudinal) artifical feel as a function of Vc

    • D. 

      Provides control stick fore/aft (longitudinal) artifical feel as a function of aircraft speed

  • 85. 
    What signals are summed by the pitch SCAS and master cylinder summing mechanism?
    • A. 

      Pitch SCAS

    • B. 

      Pitch shakers

    • C. 

      Pitch commands

    • D. 

      Linkage shakers

    • E. 

      SCAS acuator signals

  • 86. 
    When does the mechanical pitch control linkage recieve the shaker oscillations?
    • A. 

      When the aircraft is on the ground prior to rotation

    • B. 

      When the aircraft is in flight

    • C. 

      When the pitch control subystem produces a ground signal

    • D. 

      When the FCS power is applied

  • 87. 
    How are the small-amplitude oscillations produced?
    • A. 

      Rotating bob weights

    • B. 

      Rotating tension weights

    • C. 

      Rotating eccentric weights

    • D. 

      Stationary eccentric weights

  • 88. 
    What's the purpose of the pitch trim system?
    • A. 

      Provides coarse adjustments to the pitch angle of the aircraft to compensate for changes in the aircraft pitch up or down attitude.

    • B. 

      Provides slight adjustments to maintain a specific degree of roll

    • C. 

      Provides a stick so as to beat your elderly next door neighbor

    • D. 

      Provides slight adjustments to the pitch angle of the aircraft to compensate for changes in the aircraft pitch up or down attitude

  • 89. 
    Which control stick contains the pitch trim switch?
    • A. 

      Both pilot and copilot

    • B. 

      Pilots

    • C. 

      Navigators

    • D. 

      Copilots

  • 90. 
    List the modes of pitch trim.
    • A. 

      NORM

    • B. 

      ALT

    • C. 

      MACH

    • D. 

      STBY

    • E. 

      GLIDESLOPE

  • 91. 
    What's the primary source of pitch trim commands during normal operation?
    • A. 

      AFCS Trim Controller

    • B. 

      AFCS Trim Commander

    • C. 

      FCS Trim Controller

    • D. 

      FCS Trim Actuator

  • 92. 
    What's the primary source of pitch trim commands during alternate mode?
    • A. 

      Pitch Trim switches on the main panel

    • B. 

      Trim switches on the AFCS controller

    • C. 

      Pitch Trim switches on the control sticks

    • D. 

      Trim switches on the FCS controller

  • 93. 
    What's the source of copilot pitch trim commands during standby mode of operation?
    • A. 

      Alternate throttle/flight control main panel standby pitch trim switch

    • B. 

      Alternate throttle/flight control auxilliary panel standby pitch trim switch

    • C. 

      Main throttle/flight control main panel standby pitch trim switch

    • D. 

      ALLTV

  • 94. 
    What modes of operation bypass the AFCS trim controller?
    • A. 

      ALTER and STBY

    • B. 

      ALTER and NORM

    • C. 

      NORM and ALTER

    • D. 

      STBY and NORM

  • 95. 
    When is the TTO annunciator not illuminated?
    • A. 

      Anytime the TTO functions are complete

    • B. 

      Anytime the TTO functions aren't complete

    • C. 

      When power is lost to the AFCS controller

    • D. 

      When the TTO annunciator has an open