Avionics 2a352g Volume 2

100 Questions | Total Attempts: 75

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Avionics Quizzes & Trivia

Questions and Answers
  • 1. 
    THE MOST IMPORTANT RESPONSIBILITY OF THE ENHANCED EXPANDED FIRE CONTROL COMPUTER IS TO INTEGRATE THE ENTIRE F-16 AVIONICS SYSTEM BY SERVING AS THE
    • A. 

      BACKUP BUS CONTROLLER FOR THE SERIAL DIGITAL BUSES

    • B. 

      PRIMARY BUS CONTROLLER FOR THE SERIAL DIGITAL BUSES

    • C. 

      BACKUP BUS CONTROLLER FOR THE PARALLEL DIGITAL BUSES

    • D. 

      PRIMARY BUS CONTROLLER FOR THE PARALLEL DIGITAL BUSES

  • 2. 
    IN THE EVENT OF A FAILURE, WHAT COMPONENT BACKS UP THE ENHANCED EXPANDED FIRE CONTROL COMPUTER ON BLOCK 25?
    • A. 

      FCC

    • B. 

      ECIU

    • C. 

      ACIU

    • D. 

      HUD EU

  • 3. 
    AS DIRECTED BY THE ENHANCED EXPANDED FIRE CONTROL COMPUTER OPERATIONAL FLIGHT PROGRAM, ALL ARITHMETIC CALCULATIONS ARE PERFORMED BY THE
    • A. 

      CORE MEMORY UNIT

    • B. 

      SERIAL DIGITAL INTERFACE

    • C. 

      INPUT/OUTPUT UNIT

    • D. 

      CENTRAL PROCESSING UNIT

  • 4. 
    WHERE ARE MUX BUS TRANSFORMERS LOCATED AND WHAT'S THEIR PURPOSE?`
    • A. 

      ON MUX MATRIX ASSEMBLIES, COMMUNICATES WITH SLAVE TERMINALS

    • B. 

      ON MUX MATRIX ASSEMBLIES, PROVIDES IMPEDANCE MATCHING AND SHORT-CIRCUIT PROTECTION

    • C. 

      IN THE EEFCC, COMMUNICATES WITH SLAVE TERMINALS

    • D. 

      IN THE EEFCC, PROVIDES IMPEDANCE MATCHING AND SHORT-CIRCUIT PROTECTION

  • 5. 
    HOW MANY MESSAGE WORDS ARE USED FOR EEFCC BUS PROTOCOL AND WHAT ARE THE WORDS?
    • A. 

      3, COMMAND, DATA, AND SYNC

    • B. 

      3, COMMAND, DATA, AND STATUS

    • C. 

      4, COMMAND, DATA, STATUS AND SYNC

    • D. 

      4, COMMAND, DATA, STATUS AND RESPONSE

  • 6. 
    WHAT HELPS THE EEFCC DETERMINE IF A TRANSMITTED WORD IS GOOD OR BAD?
    • A. 

      IDENTITY BIT

    • B. 

      RESPONSE BIT

    • C. 

      ODD PARITY BIT

    • D. 

      EVEN PARITY BIT

  • 7. 
    WHAT TRANSMITS THE STATUS WORD?
    • A. 

      SLAVE TERMINAL

    • B. 

      MUX BUS TRANSFORMER

    • C. 

      ACIU

    • D. 

      EEFCC

  • 8. 
    WHAT STATEMENT BEST DESCRIBES THE EEFCC SELF-TEST?
    • A. 

      THE EEFCC ONLY UTILIZES BIT

    • B. 

      ITS RUN ONLY WHEN COMMANDED BY THE OPERATOR

    • C. 

      IT'S A SELF-RUNNING TEST AND WHEN COMPLETE, STARTS OVER AGAIN

    • D. 

      IT'S A PERFORMED ONLY ONCE AT GENERAL AVIONICS COMPUTER POWER-UP

  • 9. 
    WHAT TYPE BATTERY DOES THE MODULAR MISSION COMPUTER CONTAIN, AND WHAT IS ITS PURPOSE?
    • A. 

      AN ALKALINE 3.6 VOLT, C SIZE BATTERY, IT PROVIDES PRIMARY POWER TO THE MMC

    • B. 

      A LITHIUM 3.6 VOLT, D SIZE BATTERY, IT PROVIDES A BACK-UP CAPABILITY IN THE EVENT OF FAILURE, REMOVAL, OR RECHARGING OF THE AIRCRAFT BATTERY

    • C. 

      AN ALKALINE 3.6 VOLT BATTERY, C SIZE BATTERY, IT PROVIDES A BACK-UP CAPABILITY IN THE EVENT OF FAILURE, REMOVAL, OR RECHARGING OF THE AIRCRAFT BATTERY

    • D. 

      A LITHIUM 3.6 VOLT, D SIZE BATTERY, IT PROVIDES PRIMARY POWER TO THE MMC

  • 10. 
    WHAT SWITCH TURNS ON THE MMC AND WHERE IS IT LOCATED?
    • A. 

      MMC MASTER SWITCH, ICP

    • B. 

      MMC POWER SWITCH, AVIONICS POWER PANEL

    • C. 

      MMC MASTER SWITCH, AVIONICS POWER PANEL

    • D. 

      MMC POWER SWITCH, ICP

  • 11. 
    WHICH MMC MODULE SET PROVIDES FOR GENERAL PROCESSING CAPABILITIES OF THE MMC OFP, GENERATES SYMBOLOGY, AND PROVIDES THE INTERFACE FOR THE HEAD-UP DISPLAY PILOTS DISPLAY UNIT?
    • A. 

      POWER SUPPLY SET

    • B. 

      MISSION PROCESSING SET

    • C. 

      AIRCRAFT INPUT/OUTPUT SET

    • D. 

      SYMBOLOGY GENERATOR SET

  • 12. 
    WHICH MODULE SET HANDLES THE MAJORITY OF DISCRETE AND ANALOG COMMUNICATIONS WITH THE REST OF THE F-16 AVIONICS?
    • A. 

      POWER SUPPLY SET

    • B. 

      MISSION PROCESSING SET

    • C. 

      AIRCRAFT INPUT/OUTPUT SET

    • D. 

      SYMBOLOGY GENERATOR SET

  • 13. 
    WHAT ARE THE TWO INTERNAL MMC BUSES THAT PROVIDE COMMUNICATION BETWEEN MODULES?
    • A. 

      THE PARALLEL INTERMODULE BUS/SERIAL DIGITAL TEST AND MAINTENANCE BUS

    • B. 

      THE PARALLEL INTERMODULE BUS/SERIAL DIGITAL TEST AND EVALUATIONS BUS

    • C. 

      THE DISCRETE DIGITAL DATA BUS/PARALLEL TEST AND MAINTENANCE BUS

    • D. 

      THE DICRETE DIGITAL DATA BUS/PARALLEL TEST AND EVALUATIONS BUS

  • 14. 
    THE EEFCC AND MMC MUX BUS ARCHITECTURE IS BASICALLY THE SAME EXCEPT THE
    • A. 

      MMC DOESN'T USE THE AMUX OR BMUX

    • B. 

      EEFCC DOESN'T USE THE AMUX OR BMUX

    • C. 

      MMC HAS TWO ADDITIONAL BUSES: CMUX AND FMUX

    • D. 

      EEFCC HAS TWO ADDITIONAL BUSES: THE CMUX AND FMUX

  • 15. 
    WHAT IS THE BACKUP BUS CONTROLLER FOR THE MMC?
    • A. 

      ACIU

    • B. 

      ECIU

    • C. 

      XFCC

    • D. 

      CMFDS

  • 16. 
    THERE IS EXCESSIVE MOISTURE IN THE HUD PILOTS DISPLAY UNIT WHEN THE
    • A. 

      PDU MOISTURE INDICATOR IS PINK

    • B. 

      PDU MOISTURE INDICATOR IS BLUE

    • C. 

      HUD DESICCATOR IS PINK

    • D. 

      HUD DESICCATOR IS BLUE

  • 17. 
    WHAT HUD PDU HAS THE LARGEST FIELD OF VIEW DISPLAY SURFACE?
    • A. 

      CONVENTIONAL HUD

    • B. 

      WIDE ANGLE RASTER HUD

    • C. 

      WIDE ANGLE CONVENTIONAL HUD

    • D. 

      LOW ALTITUDE NAVIGATION AND TARGETING INFRARED FOR NIGHT HUD

  • 18. 
    THE INTEGRATED CONTROL PANEL IS LOCATED ON THE HUD PDU, HOWEVER ITS ASSIGNED TO WHAT SUBSYSTEM?
    • A. 

      DATA ENTRY

    • B. 

      FIRE CONTROL

    • C. 

      DATA TRANSFER

    • D. 

      STORES MANAGEMENT

  • 19. 
    WHICH ONE OF THE FOLLOW CONTROLS IS ALSO AN ON/AFF SWITCH THAT APPLIES POWER TO THE HUD?
    • A. 

      INT

    • B. 

      CONT

    • C. 

      SYM

    • D. 

      RET DEPR

  • 20. 
    WHAT THREE POSITION SWITCH CONTROLS DISPLAY OF VARIOUS SCALES ON THE HUD?
    • A. 

      ALT

    • B. 

      TEST SWITCHES

    • C. 

      DED

    • D. 

      THE ENERGY MANAGEMENT SWITCH

  • 21. 
    WHAT ARE THE THREE AIRSPEED PRESENTATIONS AVAILABLE WHEN THE VELOCITY SWITCH ON THE HUD REMOTE CONTROL PANEL IS USED?
    • A. 

      CAS, TAS AND MGT

    • B. 

      TAS, GND SPD, AND MH

    • C. 

      CAS, TAS AND GND SPD

    • D. 

      GND SPD, CAS AND MH

  • 22. 
    YOU HAVE SELECTED AUTOMATIC BRIGHTNESS WITH THE BRIGHTNESS SWITCH. IF THE AMBIENT LIGHT INCREASES, THE BRIGHTNESS OF THE HUD
    • A. 

      DECREASES

    • B. 

      INCREASES

    • C. 

      STAYS THE SAME

    • D. 

      REVERTS TO MANUAL OPERATION

  • 23. 
    ON THE HUD REMOTE CONTROL PANEL, YOU CAN CHECK THE PRIMARY AND STANDBY RETICLE BY PLACING THE RETICLE DEPRESSION SWITCH TO EITHER
    • A. 

      PRI OR ALT

    • B. 

      PRI OR SEC

    • C. 

      PRI OR STBY

    • D. 

      STBY OR SEC

  • 24. 
    THE HUD INDICATES THE SENSOR OF INTEREST BY THE
    • A. 

      LINE AROUND THE HUD DISPLAY

    • B. 

      ASTERISK IN THE LOWER LEFT SIDE OF THE HUD

    • C. 

      ASTERISK IN THE UPPER LEFT SIDE OF THE HUD

    • D. 

      ASTERISK IN THE UPPER RIGHT SIDE OF THE HUD

  • 25. 
    THE ORIENTATION OF THE STEERING CUE LINE INDICATES BEARING TO THE STEER POINT, WHICH IS 90 DEGREES WHEN THE STEERING CUE LINE IS AT
    • A. 

      3 OCLOCK

    • B. 

      6 OCLOCK

    • C. 

      9 OCLOCK

    • D. 

      12 OCLOCK

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