CDC 2A354C Volume 1. F-16 Attack Control Systems

100 Questions | Total Attempts: 309

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2A354C Quizzes & Trivia

The F-16 fighting falcon is a single engine fighter jet initially developed for the American Air Force. CDC 2a354c Volume 1. F-16 Attack Control Systems is specifically designed to test your knowledge on this fighter jet. All the best and enjoy.


Questions and Answers
  • 1. 
    The most important responsibility of the EEFCC 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 buses

    • D. 

      Primary bus controller for the parallel digital buses

  • 2. 
    The fault gathering and reporting center of the weapons control system is the 
    • A. 

      Heads-down display

    • B. 

      Heads-up display

    • C. 

      Stores management system

    • D. 

      Enhanced expanded fire control computer (EEFCC)

  • 3. 
    As directed by the EEFCC OFP, all arithmetic calculations are performed by the 
    • A. 

      Core memory unit

    • B. 

      Serial-digital interface

    • C. 

      I/O unit

    • D. 

      CPU

  • 4. 
    What is the core memory size of the EEFCC
    • A. 

      256K

    • B. 

      512K

    • C. 

      256M

    • D. 

      512M

  • 5. 
    Where are MUX bus transformers located and what's their purpose?
    • A. 

      In the EEFCC; communicates with slave terminals

    • B. 

      On MUX matrix assemblies; provides impedance matching and short-circuit protection

    • C. 

      In the EEFCC; provides impedance matching and short-circuit protection

    • D. 

      On MUX matrix assemblies; communicates with slave terminals

  • 6. 
    When the EEFCC determines if a transmitted word is good or bad, what type of bit aids in this?
    • A. 

      Identity

    • B. 

      Response

    • C. 

      Odd Parity

    • D. 

      Even Parity

  • 7. 
    Which statement best describes the self-test of the EEFCC?
    • A. 

      The EEFCC only utilizes BIT

    • B. 

      It's run only when commanded by the operator

    • C. 

      It's a self-running test and when complete, starts over again

    • D. 

      It's performed only once at GAC power-up

  • 8. 
    What type of battery does the MMC contain, and what is the battery's purpose?
    • A. 

      An alkaline 3.6 volt, C size batter; it provides a back-up capability in the event of failure, removal, or recharging of the aircraft battery.

    • 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, C size battery; provides primary power to the MMC

    • D. 

      A lithium 3.6 volt, D size battery; it provides primary power to the MMC

  • 9. 
    If you want standby power to all SMS stores stations that have inventory loaded in memory, which switch would you use?
    • A. 

      MMC power switch

    • B. 

      SMS standby power switch

    • C. 

      MMC master switch

    • D. 

      Stores station switch

  • 10. 
    The two internal MMC  buses that provide communication between modules are the 
    • A. 

      Parallel intermodule/ serial digital test and maintenance bus

    • B. 

      Parallel intermodule/ serial digital test and evaluation bus

    • C. 

      Discrete digital data bus/ parallel test and maintenance bus

    • D. 

      Discrete digital data bus/ parallel test and evaluation bus

  • 11. 
    The EEFCC and MMC MUX bus architecture is basically the same except the 
    • A. 

      MMC doesn't use the A-MUX or B-MUX

    • B. 

      EEFCC doesn't use the A-MUX or B-MUX

    • C. 

      MMC has two additional buses; the C-MUX and F-MUX

    • D. 

      EEFCC has two additional buses; the C-MUX and F-MUX

  • 12. 
    Which two scenarios will generate a MMC auto restart when the MMC fails?
    • A. 

      Software failures and hardware failures

    • B. 

      Software failures and slave terminal failures

    • C. 

      Hardware failures and slave terminal failures

    • D. 

      Hardware failures and MUX bus failures

  • 13. 
    How many MFL memory locations does the MMC contain?
    • A. 

      15

    • B. 

      16

    • C. 

      17

    • D. 

      18

  • 14. 
    The MMC BIT is
    • A. 

      Interruptive, meaning the normal operation of the subsystem is maintained during the actual BIT

    • B. 

      Nointerruptive, meaning that normal operation of the subsystem is maintained during the actual BIT

    • C. 

      Interruptive, meaning that normal operation of the subsystem is not available until the BIT has been completed

    • D. 

      Noninterruptive, meaning that normal operation of the subsystem is not available until the BIT has been completed

  • 15. 
    Which F-16 ADIS component contains a microprocessor, firmware, interface electronics, power supply, and other electronics necessary to manage data transfer?
    • A. 

      DTU

    • B. 

      DTC

    • C. 

      DTCP

    • D. 

      DTS/DTC

  • 16. 
    Which F-16 ADIS component is a transportable, nonvolatile memory, which interfaces aircraft systems through the DTU
    • A. 

      DTD

    • B. 

      DTC

    • C. 

      DTCP

    • D. 

      DTDU

  • 17. 
    Considered the heart of the UFC system, this component is a programmable computer that controls and interfaces the UFC
    • A. 

      CDEEU

    • B. 

      MMC

    • C. 

      MFD

    • D. 

      DEEU power supply

  • 18. 
    On what F-16 would you find a PFLD
    • A. 

      F-16 A/B block 15

    • B. 

      F-16 C/D block 40 only

    • C. 

      F-16 C/D block 40 and up

    • D. 

      F-16 C/D blocks 25 through 32

  • 19. 
    If the PFLD fails but the UFC set is still functioning, the PFLD data can be displayed on the
    • A. 

      HUD

    • B. 

      DED

    • C. 

      MFD

    • D. 

      MFDS

  • 20. 
    Identify the four priority override keys which are located across the top of the ICP and IKP
    • A. 

      COM 1, COM 2, INS, LIST

    • B. 

      COM 1, COM 2, IFF, LIST

    • C. 

      COM 3, COM 4, INS, LIST

    • D. 

      COM 3, COM 4, IFF, LIST

  • 21. 
    All of the following are functions provided by the DCS except
    • A. 

      Page title option access

    • B. 

      SOI selection

    • C. 

      Positioning the DED asterisks

    • D. 

      Frequently accedded data pages

  • 22. 
    On the F-16 UFC, which page is more or less a continuation of the LIST page?
    • A. 

      BNGO page

    • B. 

      STPT page

    • C. 

      MISC page

    • D. 

      CNI page

  • 23. 
    UFC priority functions are made available through the priority function keys, only when the 
    • A. 

      CNI page is displayed on the DED

    • B. 

      MISC page is displayed on the MFD

    • C. 

      MISC page is displayed on the DED

    • D. 

      CNI page is displayed on the MFD

  • 24. 
    When do the UFC provide the capability to enter numeric data through the ICP/IKP?
    • A. 

      After the NUMERIC key is depressed

    • B. 

      Only when entering navigation coordinates

    • C. 

      Anytime a DED page is displayed

    • D. 

      When the asterisks are positioned about a numeric data field

  • 25. 
    When the CNI page is displayed, how many function values can be changed using the increment/decrement switch?
    • A. 

      Two

    • B. 

      Three

    • C. 

      Four

    • D. 

      Five

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