Avionics 2a352g Volume 3

100 Questions | Total Attempts: 134

SettingsSettingsSettings
Please wait...
Avionics Quizzes & Trivia

Questions and Answers
  • 1. 
    WHAT FLIGHT ENVIRONMENTAL PRESSURE IS SENSED BY SMALL HOLES LOCATED ON THE SIDES OF THE PITOT AND AIR DATA PROBES?
    • A. 

      PITOT

    • B. 

      STATIC

    • C. 

      IMPACT

    • D. 

      DIFFERNTIAL

  • 2. 
    TRUE AOA IS THE ANGLE BETWEEN AN AIRCRAFTS WING CORD LINE AND ITS
    • A. 

      ATTITUDE

    • B. 

      ALTITUDE

    • C. 

      FLIGHT PATH

    • D. 

      GLIDE SLOPE

  • 3. 
    HOW MANY SOURCES OF Pt AND Ps ARE ROUTED BY THE PITOT STATIC PROBE PNEUMATIC SYSTEM?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      4

  • 4. 
    THE PITOT STATIC PRONE PNEUMATIC SYSTEM SUPPLIES AIR DATA TO THE CADC, AMI, ALTIMETER, AND
    • A. 

      FLCC

    • B. 

      PSA

    • C. 

      ECA

    • D. 

      DFLCC

  • 5. 
    THE CADC OUTPUTS ITS DATA USING THREE METHODS. THESE METHODS ARE SERIAL DIGITAL DATA WORDS, DISCRETES, AND
    • A. 

      ANALOG

    • B. 

      DISTINCT

    • C. 

      ISOLATED

    • D. 

      COMBINED

  • 6. 
    CADC SERIAL DIGITAL DATA WORDS ARE AVAILABLE ON THE
    • A. 

      A MUX

    • B. 

      B MUX

    • C. 

      C MUX

    • D. 

      D MUX

  • 7. 
    HOW ARE CADC ANALOG OUTPUT SIGNALS TRANSFERRED TO THEIR FINAL DESTINATION?
    • A. 

      VIA THE A MUX

    • B. 

      VIA THE D MUX

    • C. 

      VIA AIRCRAFT WING

    • D. 

      VIA FIBER OPTICS

  • 8. 
    ONE COMPLETE REVOLUTION OF THE ALTIMETERS ALTITUDE DIAL EQUALS
    • A. 

      100 FEET OF ALTITUDE

    • B. 

      1000 FEET OF ALTITUDE

    • C. 

      5000 FEET OF ALTITUDE

    • D. 

      10000 FEET OF ALTITUDE

  • 9. 
    WHATS THE DISPLAY RANGE OF THE ALTIMETERS ALTITUDE DRUM COUNTER?
    • A. 

      0 - 50000

    • B. 

      0 - 80000

    • C. 

      -1000 - 50000

    • D. 

      -1000 - 80000

  • 10. 
    WHY WOULD A PILOT ADJUST THE ALTIMETER TO DISPLAY PRESSURE ALTITUDE?
    • A. 

      TO DISPLAY ALTITUDE ABOVE TERRAIN

    • B. 

      TO DISPLAY ALTITUDE BELOW SEA LEVEL

    • C. 

      TO STANDARDIZE AIRCRAFT ALTITUDES FOR LOW ALTITUDE AIR TRAFFIC CONTROL

    • D. 

      TO STANDARDIZE AIRCRAFT ALTITUDES FOR HIGH ALTITUDE AIR TRAFFIC CONTROL

  • 11. 
    WHAT COMPONENT DEVELOPS THE VVIs VERTICAL VELOCITY SIGNAL?
    • A. 

      VVI

    • B. 

      FLCC

    • C. 

      PSA

    • D. 

      CADC

  • 12. 
    THE AOA INDICATOR IS CONSIDERED A
    • A. 

      BACK UP INDICATOR

    • B. 

      VERTICAL TAPE INDICATOR

    • C. 

      SELF CONTAINED INDICATOR

    • D. 

      HORIZONTAL TAPE INDICATOR

  • 13. 
    WHATS THE FUNCTION OF THE AOA INDEXERS LEVER CONTROL SWITCH?
    • A. 

      ON/OFF SWITCH

    • B. 

      SECTOR LIGHT INTENSITY

    • C. 

      ENABLES AOA LOGIC CIRCUITS

    • D. 

      ONLY USED DURING TAKEOFF AND LANDING CONFIGURES

  • 14. 
    HOW MANY DEDICATED SENSORS ARE UTILIZED BY THE CSFDR SYSTEM?
    • A. 

      5

    • B. 

      6

    • C. 

      7

    • D. 

      8

  • 15. 
    WHATS CSFDR TYPE 1 DATA PRIMARILY USED FOR?
    • A. 

      ENGINE ANALYSIS

    • B. 

      MISHAP INVESTIGATION

    • C. 

      INDIVIDUAL AIRCRAFT TRACKING

    • D. 

      MAINTENANCE TROUBLESHOOTING

  • 16. 
    WHAT PREDETERMINES CSFDR SPECIAL EVENT CRITERIA?
    • A. 

      TYPE 1 DATA

    • B. 

      BASELINE DATA

    • C. 

      CMSU CONFIGURATION

    • D. 

      SAU OFP

  • 17. 
    WHAT CSFDR TYPE DATA IS DUBBED AS INDIVIDUAL AIRCRAFT TRAKCING DATA?
    • A. 

      1

    • B. 

      2

    • C. 

      3

    • D. 

      4

  • 18. 
    WHAT DFLCC BRANCH COMMUNICATES WITH THE SDR?
    • A. 

      A

    • B. 

      B

    • C. 

      C

    • D. 

      D

  • 19. 
    WHEN DOES THE SDR CEASE RECORDING OPERATIONS?
    • A. 

      UPON FLCS SHUTDOWN

    • B. 

      UPON A WOW CONDITION

    • C. 

      DURING DIGITAL BACKUP OPERATIONS

    • D. 

      UPON AUTOPILOT ENGAGEMENT

  • 20. 
    DANIEL BERNOULLI DEVELOPED A THEORY ON THE RELATIONSHIP OF FLUID SPEED,
    • A. 

      AND PRESSURE

    • B. 

      AIR, AND PRESSURE

    • C. 

      TIME, AND PRESSURE

    • D. 

      AIR PRESSURE, AND VENTURI

  • 21. 
    AS FLUID PASSES THROUGH A VENTURI, PRESSURE IS
    • A. 

      EQUAL THROUGHOUT THE VENTURI

    • B. 

      LOWEST WHERE SPEED IS LOWEST

    • C. 

      LOWEST WHERE SPEED IS HIGHEST

    • D. 

      A PRODUCT OF FLUID SPEED, TIME, AND DISTANCE

  • 22. 
    AS AIR RUSHES PAST AN AIRFOIL, WHAT FORCE IS CREATED?
    • A. 

      LIFT

    • B. 

      DRAG

    • C. 

      SPEED

    • D. 

      THRUST

  • 23. 
    A MORE STREAMLINED AIRFOIL HAS
    • A. 

      LESS DRAG AND LESS LIFT

    • B. 

      MORE DRAG AND LESS LIFT

    • C. 

      LESS DRAG AND MORE LIFT

    • D. 

      MORE DRAG AND MORE LIFT

  • 24. 
    WHAT IS THE RELATIONSHIP BETWEEN LIFT AND THE AOA?
    • A. 

      LIFT EQUALS AOA

    • B. 

      LIFT INCREASES WITH AOA

    • C. 

      LIFT DECREASES WITH AOA

    • D. 

      THE TERMS ARE INTERCHANGEABLE

  • 25. 
    AT WHAT POINT DO MOST AIRFOILS ENTER A STALL CONDITION?
    • A. 

      10

    • B. 

      20

    • C. 

      30

    • D. 

      40

Back to Top Back to top