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

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  • 1/100 Questions

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

    • DTD
    • DTC
    • DTCP
    • DTDU
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About This Quiz

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.

Control Systems Quizzes & Trivia

Quiz Preview

  • 2. 

    The CMFD feature that allows an interchange of the left and right CMFD format is the 

    • MFDS BIT

    • DCLT

    • RESET MENU

    • SWAP

    Correct Answer
    A. SWAP
    Explanation
    The correct answer is "SWAP" because it refers to a CMFD feature that enables the interchange of the left and right CMFD format. This feature allows the user to switch the display of information between the left and right CMFD screens, providing flexibility and convenience in accessing and viewing data.

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  • 3. 

    On what F-16 would you find a PFLD

    • F-16 A/B block 15

    • F-16 C/D block 40 only

    • F-16 C/D block 40 and up

    • F-16 C/D blocks 25 through 32

    Correct Answer
    A. F-16 C/D block 40 and up
    Explanation
    The PFLD (Proximity Fuse Laser Designator) can be found on the F-16 C/D block 40 and up. This means that the PFLD is not present on the F-16 A/B block 15 or the F-16 C/D blocks 25 through 32. The answer indicates that the PFLD is specifically available on the F-16 C/D block 40 and any subsequent blocks.

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  • 4. 

    If the more faults indicators are present on the PFLD, these additional faults are reviewed by depressing the 

    • More faults button

    • F-ACK button

    • Clear button on the MFD

    • Additional faults button for 10 seconds to allow automatic display

    Correct Answer
    A. F-ACK button
    Explanation
    When there are more fault indicators present on the PFLD, the user can review these additional faults by depressing the F-ACK button. This button allows the user to acknowledge and review the additional faults indicated on the display. It is specifically designed for this purpose and helps in managing and addressing multiple faults efficiently.

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  • 5. 

    As directed by the EEFCC OFP, all arithmetic calculations are performed by the 

    • Core memory unit

    • Serial-digital interface

    • I/O unit

    • CPU

    Correct Answer
    A. CPU
    Explanation
    The CPU, or Central Processing Unit, is responsible for performing arithmetic calculations in a computer system. It is the brain of the computer and carries out all the instructions and calculations necessary for the system to function. The other options mentioned, such as the core memory unit, serial-digital interface, and I/O unit, are not directly involved in arithmetic calculations, making the CPU the correct answer.

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  • 6. 

    Which statement best describes the self-test of the EEFCC?

    • The EEFCC only utilizes BIT

    • It's run only when commanded by the operator

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

    • It's performed only once at GAC power-up

    Correct Answer
    A. It's a self-running test and when complete, starts over again
    Explanation
    The correct answer is "It's a self-running test and when complete, starts over again." This means that the self-test of the EEFCC is automated and continuous. Once the test is finished, it will automatically restart and run again. This ensures that the EEFCC is constantly monitoring and checking its own functionality without the need for manual intervention or operator command.

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  • 7. 

    When do the UFC provide the capability to enter numeric data through the ICP/IKP?

    • After the NUMERIC key is depressed

    • Only when entering navigation coordinates

    • Anytime a DED page is displayed

    • When the asterisks are positioned about a numeric data field

    Correct Answer
    A. When the asterisks are positioned about a numeric data field
    Explanation
    The UFC provides the capability to enter numeric data through the ICP/IKP when the asterisks are positioned about a numeric data field. This means that whenever there is a numeric data field displayed on the screen and the asterisks (*) are located around it, the user can input numeric data using the UFC. This indicates that the UFC is ready to accept and process numeric inputs at that time.

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  • 8. 

    Depressing the M-DEL key, depending on the situation, can display a negative sign (-) to applicable data field entries, select a mode (option) from the controlling subsystem, or display a 

    • Zero in the data field

    • One in the data field

    • Two in the data field

    • Three in the data field

    Correct Answer
    A. Zero in the data field
    Explanation
    Depressing the M-DEL key can display a zero in the data field. This means that when the M-DEL key is pressed, it will clear any existing data in the field and replace it with a zero. This could be useful in situations where the user wants to reset or clear the data in the field to start fresh.

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  • 9. 

    If you want to apply power and adjust the brightness to the HUD, which control would you use?

    • INT control

    • CONT control

    • SYM control

    • RET DEPR control

    Correct Answer
    A. SYM control
    Explanation
    The SYM control is the appropriate control to use if you want to apply power and adjust the brightness to the HUD.

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  • 10. 

    The three HUD master modes are air-to-air, air-to-ground, and

    • Navigation

    • Air-to-air guns

    • Air-to-air missles

    • Electronic countermeasures

    Correct Answer
    A. Navigation
    Explanation
    The three HUD master modes are air-to-air, air-to-ground, and navigation. The HUD (Head-Up Display) is a transparent display that presents information without requiring users to look away from their usual viewpoints. In the context of aircraft, the navigation master mode on the HUD provides essential information related to the aircraft's position, heading, altitude, and other navigational data. This mode helps pilots in accurately navigating and following flight routes and waypoints, ensuring safe and efficient navigation during flight operations.

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  • 11. 

    Which JHMCS LRU generates a magnetic field generated inside the cockpit?

    • MEU

    • MGU

    • MTU

    • PMG

    Correct Answer
    A. MTU
    Explanation
    The MTU (Magnetic Tracking Unit) generates a magnetic field inside the cockpit. This magnetic field is used by the JHMCS (Joint Helmet Mounted Cueing System) to track the pilot's head movements and provide accurate targeting information. The MTU is responsible for detecting and measuring the pilot's magnetic field, allowing the system to accurately track their line of sight and provide real-time situational awareness.

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  • 12. 

    To accurately indicate the direction of the object reflecting the radar energy, you adjust the position of the radar 

    • Antenna

    • Receiver

    • Indicator

    • Transmitter

    Correct Answer
    A. Antenna
    Explanation
    To accurately indicate the direction of the object reflecting the radar energy, you adjust the position of the radar antenna. The antenna is responsible for transmitting and receiving radar signals. By adjusting its position, you can determine the direction from which the radar energy is being reflected. The receiver and transmitter are components of the radar system, but they do not directly determine the direction of the object. The indicator is a display device that shows the information received from the antenna.

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  • 13. 

    The output of the radar transmitter is routed to the antenna

    • Through a waveguide

    • By hardwired duplex cabling

    • Through a shielded-pair coax cable

    • By electromagnetic wave propagation

    Correct Answer
    A. Through a waveguide
    Explanation
    The output of the radar transmitter is routed to the antenna through a waveguide. A waveguide is a structure that guides electromagnetic waves, such as radio waves, from one point to another. It provides a low-loss path for the waves to travel, ensuring efficient transmission. In the case of the radar system, the waveguide is used to direct the radar signal from the transmitter to the antenna, which then broadcasts the signal into the surrounding space. This method of transmission is commonly used in radar systems due to its ability to handle high-power signals and minimize signal loss.

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  • 14. 

    The F-16C/D ANT ELEV control and radar CURSOR/ENABLE switches are located on the 

    • MLPRF assembly

    • Pressure regulator/ relief valve

    • Waveguide assembly

    • Throttle grip

    Correct Answer
    A. Throttle grip
    Explanation
    The F-16C/D ANT ELEV control and radar CURSOR/ENABLE switches are located on the throttle grip. This means that the switches can be easily accessed and operated by the pilot while controlling the throttle. Placing the switches on the throttle grip allows for efficient and convenient use, as the pilot can make adjustments to the antenna elevation and radar cursor without having to reach for separate controls.

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  • 15. 

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

    • Identity

    • Response

    • Odd Parity

    • Even Parity

    Correct Answer
    A. Odd Parity
    Explanation
    Odd Parity is the type of bit that aids the EEFCC in determining if a transmitted word is good or bad. In odd parity, the number of 1s in a word is counted, and if the count is odd, the parity bit is set to 1 to make the total number of 1s even. This allows the receiver to detect if there has been an error during transmission, as any change in the number of 1s will result in an odd number of 1s and indicate a bad word.

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  • 16. 

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

    • 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.

    • 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.

    • An alkaline 3.6 volt, C size battery; provides primary power to the MMC

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

    Correct Answer
    A. 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.
    Explanation
    The correct answer is 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. This means that the MMC (presumably a component of an aircraft) is powered by a lithium battery that serves as a backup power source. In case the main aircraft battery fails, is removed, or needs to be recharged, the lithium battery in the MMC will provide power to ensure continuous operation.

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  • 17. 

    The EEFCC and MMC MUX bus architecture is basically the same except the 

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

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

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

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

    Correct Answer
    A. MMC has two additional buses; the C-MUX and F-MUX
    Explanation
    The correct answer is MMC has two additional buses; the C-MUX and F-MUX. This is because the given statement clearly states that the MMC has two additional buses, namely the C-MUX and F-MUX. The EEFCC, on the other hand, does not have these additional buses. Therefore, the difference between the two architectures lies in the presence of these additional buses in the MMC architecture.

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  • 18. 

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

    • BNGO page

    • STPT page

    • MISC page

    • CNI page

    Correct Answer
    A. MISC page
    Explanation
    The MISC page is more or less a continuation of the LIST page on the F-16 UFC. This suggests that the MISC page contains similar or related information to the LIST page, possibly providing additional details or options that are not covered on the LIST page.

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  • 19. 

    An OSS function is identified by the 

    • Mnemonic adjacent to the OSS

    • Mnemonic engraved on the OSS face

    • Number sequence adjacent to the OSS

    • Number sequence engraved on the OSS face

    Correct Answer
    A. Mnemonic adjacent to the OSS
    Explanation
    The correct answer is "mnemonic adjacent to the OSS." This means that an OSS function is identified by the mnemonic (a short and memorable name) that is located next to the OSS (Open Source Software). The mnemonic helps to describe and label the specific function or feature of the OSS, making it easier for users to understand and navigate.

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  • 20. 

    Radar sets determine the distance (range) to a potential target by measuring the 

    • Strength of the reflected pulses

    • Amplitude of the pulses reflected back to the antenna

    • Elapsed time between pulse transmission and reception

    • PRF of the reflected energy

    Correct Answer
    A. Elapsed time between pulse transmission and reception
    Explanation
    Radar sets determine the distance to a potential target by measuring the elapsed time between pulse transmission and reception. This is because the speed of the radio waves is known, so by measuring the time it takes for the pulse to travel to the target and back, the distance can be calculated. The strength of the reflected pulses, amplitude of the pulses reflected back to the antenna, and PRF of the reflected energy are not directly related to determining the distance to a target.

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  • 21. 

    The antenna waveguide duplexer in a radar system

    • Routes high-power RF into the receiver

    • Allows the same antenna to both receive and transmit RF

    • Prevents the received RF from damaging the receiver

    • Prevents high-power RF from being transmitted

    Correct Answer
    A. Allows the same antenna to both receive and transmit RF
    Explanation
    The antenna waveguide duplexer in a radar system allows the same antenna to both receive and transmit RF. This means that the radar system can use a single antenna for both sending and receiving signals, which helps to simplify the system design and reduce the number of components needed. The duplexer ensures that the transmitted RF signals do not interfere with the received signals, allowing for efficient and accurate radar operation.

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  • 22. 

    The two major operating modes of the F-16 FCR system are

    • Search and track

    • Direction and tracking

    • Beacon and air combat

    • Air-to-air and air-to-ground

    Correct Answer
    A. Air-to-air and air-to-ground
    Explanation
    The F-16 FCR system has two major operating modes: air-to-air and air-to-ground. In the air-to-air mode, the system is used for detecting and tracking enemy aircraft, allowing the pilot to engage in air combat. In the air-to-ground mode, the system is used for detecting and tracking ground targets, enabling the pilot to engage in air-to-ground attacks. These two modes provide the F-16 with versatility and the ability to perform different missions effectively.

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  • 23. 

    The most important responsibility of the EEFCC is to integrate the entire F-16 avionics system by serving as the 

    • Backup bus controller for the serial digital buses

    • Primary bus controller for the serial digital buses

    • Backup bus controller for the parallel buses

    • Primary bus controller for the parallel digital buses

    Correct Answer
    A. Primary bus controller for the serial digital buses
    Explanation
    The EEFCC's most important responsibility is to serve as the primary bus controller for the serial digital buses. This means that it is responsible for integrating the entire F-16 avionics system by controlling the communication and data transfer between different avionics components through the serial digital buses. As the primary bus controller, the EEFCC has the main authority and control over the bus system, ensuring smooth and efficient operation of the avionics system.

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  • 24. 

    Which two scenarios will generate a MMC auto restart when the MMC fails?

    • Software failures and hardware failures

    • Software failures and slave terminal failures

    • Hardware failures and slave terminal failures

    • Hardware failures and MUX bus failures

    Correct Answer
    A. Software failures and hardware failures
    Explanation
    When the MMC (Master Control Center) fails, two scenarios that can trigger an auto restart are software failures and hardware failures. Software failures refer to any issues or malfunctions that occur within the software system of the MMC, such as crashes or errors. Hardware failures, on the other hand, involve any problems with the physical components of the MMC, such as a malfunctioning processor or memory. In both cases, the MMC is designed to automatically restart itself to attempt to resolve the issue and restore normal operation.

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  • 25. 

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

    • DTU

    • DTC

    • DTCP

    • DTS/DTC

    Correct Answer
    A. DTU
    Explanation
    The correct answer is DTU. DTU stands for Data Transfer Unit, which is a component in the F-16 ADIS system that contains a microprocessor, firmware, interface electronics, power supply, and other electronics necessary to manage data transfer.

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  • 26. 

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

    • CDEEU

    • MMC

    • MFD

    • DEEU power supply

    Correct Answer
    A. CDEEU
    Explanation
    The correct answer is CDEEU. The given question is asking for the component that is considered the heart of the UFC system and controls and interfaces with the UFC. Out of the options provided, CDEEU is the only one that fits this description. The other options, MMC, MFD, and DEEU power supply, do not serve as programmable computers that control and interface with the UFC.

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  • 27. 

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

    • HUD

    • DED

    • MFD

    • MFDS

    Correct Answer
    A. HUD
    Explanation
    If the PFLD (Primary Flight Display) fails but the UFC (Up-Front Control) set is still functioning, the PFLD data can be displayed on the HUD (Head-Up Display). The HUD is a transparent display that presents information directly in the pilot's line of sight, allowing them to view critical flight data without having to look down at instruments. This ensures that the pilot can still access important information even if the PFLD is not operational.

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  • 28. 

    Identify the four priority override keys which are located across the top of the ICP and IKP

    • COM 1, COM 2, INS, LIST

    • COM 1, COM 2, IFF, LIST

    • COM 3, COM 4, INS, LIST

    • COM 3, COM 4, IFF, LIST

    Correct Answer
    A. COM 1, COM 2, IFF, LIST
    Explanation
    The correct answer is COM 1, COM 2, IFF, LIST. This is because these four keys, located across the top of the ICP and IKP, have the priority override function. The COM 1 and COM 2 keys are used for communication functions, allowing the user to prioritize and override other tasks. The IFF key is used for identifying and tracking targets, and the LIST key is used for accessing and managing lists or databases. These keys are essential for quick and efficient control and operation of the system.

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  • 29. 

    The RSU contains the components and circuits that produce normal acceleration signals and

    • Roll, lift, and yaw angular rates

    • Roll, pitch, and lift angular rates

    • Pitch, lift, and yaw angular rates

    • Pitch, roll, and yaw angular rates

    Correct Answer
    A. Pitch, roll, and yaw angular rates
    Explanation
    The RSU (Rate Sensor Unit) contains components and circuits that generate signals for measuring the angular rates of pitch, roll, and yaw. These angular rates refer to the rotational movements of an object around its three axes. By measuring these rates, the RSU can provide information about the object's orientation and motion in three-dimensional space.

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  • 30. 

    You have selected AUTO BRT with the brightness switch. If the ambient (surrounding) light increases, the brightness of the HUD

    • Increases

    • Decreases

    • Stays the same

    • Reverts to manual operation

    Correct Answer
    A. Increases
    Explanation
    The correct answer is "increases." When the AUTO BRT mode with the brightness switch is selected, the head-up display (HUD) adjusts its brightness based on the ambient light conditions. Therefore, if the surrounding light increases, the brightness of the HUD will also increase to ensure optimal visibility for the driver.

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  • 31. 

    A flashing flight-path marker indicates

    • Weapons release

    • Central air data computer failure

    • Failure of the stores management system

    • INU alignment complete

    Correct Answer
    A. Weapons release
    Explanation
    A flashing flight-path marker indicates weapons release. This means that when the flight-path marker on an aircraft's display is flashing, it is indicating that the aircraft has released its weapons. This is an important visual cue for the pilot to confirm that the weapons have been successfully released from the aircraft.

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  • 32. 

    What will inform the operator if a CMFD OSS is actuated?

    • Copilot

    • Tone in headset

    • Momentary flash on the CMFD screen

    • Tone in the headset as well as a momentary flash on the CMFD screen

    Correct Answer
    A. Momentary flash on the CMFD screen
    Explanation
    When a CMFD OSS (On-Screen Symbol) is actuated, the operator will be informed through a momentary flash on the CMFD (Central Multi-Function Display) screen. This flash serves as a visual indication to the operator that the CMFD OSS has been activated. The other options, such as the copilot or a tone in the headset, do not directly provide information about the actuation of the CMFD OSS.

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  • 33. 

    The F-16C/D radar OFP is contained in the 

    • DMT

    • Electronic equipment rack assembly

    • PSP

    • MLPRF assembly

    Correct Answer
    A. PSP
    Explanation
    The F-16C/D radar OFP (Operational Flight Program) is contained in the PSP (Programmable Signal Processor). The PSP is responsible for processing and analyzing radar signals in the F-16C/D aircraft. It is an essential component of the radar system and is housed in a separate assembly to ensure efficient and effective operation. The DMT (Digital Multi-Track) electronic equipment rack assembly and MLPRF (Multi-Mode Long Pulse Repetition Frequency) assembly are not directly related to the radar OFP and do not contain it.

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  • 34. 

    What is the core memory size of the EEFCC

    • 256K

    • 512K

    • 256M

    • 512M

    Correct Answer
    A. 512K
    Explanation
    The core memory size of the EEFCC is 512K. This means that the EEFCC has a memory capacity of 512 kilobytes.

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  • 35. 

    The UFC BIT is selected by depressing and releasing the OSS adjacent to the 

    • DEEU mnemonic on the MFD BIT2 page

    • UFC mnemonic on the MFD BIT2 page

    • UFC mnemonic on the DED BIT2 page

    • DEEU mnemonic on the DED BIT2 page

    Correct Answer
    A. UFC mnemonic on the MFD BIT2 page
    Explanation
    The correct answer is "UFC mnemonic on the MFD BIT2 page." This means that the UFC Built-In Test (BIT) is selected by depressing and releasing the UFC mnemonic on the Multi-Function Display (MFD) BIT2 page. The MFD BIT2 page is likely a menu or interface where different tests and functions can be accessed and controlled. By selecting the UFC mnemonic, the user can initiate the BIT for the UFC system.

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  • 36. 

    On the HUD remote control panel, you can check the PRI and STBY reticle by placing the RET DEPR switch to either

    • PRI or ALT

    • SEC or PRI

    • PRI or STBY

    • STBY or SEC

    Correct Answer
    A. PRI or STBY
    Explanation
    The correct answer is PRI or STBY. On the HUD remote control panel, the RET DEPR switch can be placed in either PRI or STBY position to check the PRI and STBY reticle. This suggests that the PRI and STBY reticle can be viewed simultaneously or independently by selecting either of these positions on the switch. Placing the switch in the PRI position may display the PRI reticle, while placing it in the STBY position may display the STBY reticle.

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  • 37. 

    Before an F-16 aircraft is boresighted, the

    • Engine must be installed

    • Aircraft must be completely refueled, and all stress panels must be installed

    • Equipment forward of the intake must be installed or replaced with ballast of equal weight

    • Aircraft must be parked in direct sunlight so as to gain maximum expansion while boresighting

    Correct Answer
    A. Equipment forward of the intake must be installed or replaced with ballast of equal weight
  • 38. 

    The fault gathering and reporting center of the weapons control system is the 

    • Heads-down display

    • Heads-up display

    • Stores management system

    • Enhanced expanded fire control computer (EEFCC)

    Correct Answer
    A. Enhanced expanded fire control computer (EEFCC)
    Explanation
    The fault gathering and reporting center of the weapons control system is the enhanced expanded fire control computer (EEFCC). This computer is responsible for collecting and reporting any faults or errors that occur within the system. It is designed to monitor the performance of the weapons control system and provide real-time feedback on any issues that may arise. The EEFCC plays a crucial role in maintaining the functionality and reliability of the weapons control system by identifying and addressing any faults or malfunctions.

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  • 39. 

    The CMFD bezel assembly contains a total of 20 OSS, 

    • Two rocker switches, two ALS, and the panel illuminators

    • Four rocker switches, two ALS, and the panel illuminators

    • And two rocker switches only

    • And four rocker switches only

    Correct Answer
    A. Four rocker switches, two ALS, and the panel illuminators
    Explanation
    The CMFD bezel assembly contains four rocker switches, two ALS, and the panel illuminators. This means that there are four switches that can be rocked back and forth, two ALS (which stands for Ambient Light Sensors), and the panel illuminators that provide lighting for the assembly.

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  • 40. 

    D&R either secondary OSS causes the display on the particular CMFD to change,

    • Making this new format the primary format

    • But this new format still remains as a secondary format

    • Promoting the multifunction display set to enter self-test

    • But after 10 seconds reverts back to the original primary format

    Correct Answer
    A. Making this new format the primary format
    Explanation
    When a secondary OSS (On-Screen Symbol) is activated, it causes the display on the particular CMFD (Central Multi-Function Display) to change. This new format becomes the primary format, meaning it takes precedence over the previous format. However, even though it becomes the primary format, it still remains as a secondary format. This change in format promotes the multifunction display set to enter self-test mode. After 10 seconds, the display reverts back to the original primary format. Therefore, the correct answer is that the activation of the secondary OSS makes the new format the primary format.

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  • 41. 

    The maximum azimuth scan limits of the F-16C/D radar antenna are

    • +or-10 degrees, for a total of 20 degree of scan

    • +or-30 degrees, for a total of 60 degree of scan

    • +or-60 degrees, for a total of 120 degree of scan

    • +or-120 degrees, for a total of 240 degree of scan

    Correct Answer
    A. +or-60 degrees, for a total of 120 degree of scan
    Explanation
    The correct answer is +or-60 degrees, for a total of 120 degrees of scan. This means that the F-16C/D radar antenna is capable of scanning up to 60 degrees to the left and 60 degrees to the right, resulting in a total scan coverage of 120 degrees.

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  • 42. 

    All of the following are functions provided by the DCS except

    • Page title option access

    • SOI selection

    • Positioning the DED asterisks

    • Frequently accedded data pages

    Correct Answer
    A. SOI selection
    Explanation
    The DCS (Data Control System) provides various functions, including page title option access, positioning the DED asterisks, and frequently accessed data pages. However, the function of SOI (Service Oriented Interface) selection is not provided by the DCS.

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  • 43. 

    The FCR cable assembly routes the RF sample between the 

    • DMT and the PSPBUS

    • MLPRF and the TWT

    • VCXO and the DMT

    • MLPRF STALO and the DMT

    Correct Answer
    A. MLPRF STALO and the DMT
    Explanation
    The FCR cable assembly routes the RF sample between the MLPRF STALO and the DMT.

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  • 44. 

    Where are MUX bus transformers located and what's their purpose?

    • In the EEFCC; communicates with slave terminals

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

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

    • On MUX matrix assemblies; communicates with slave terminals

    Correct Answer
    A. On MUX matrix assemblies; provides impedance matching and short-circuit protection
    Explanation
    MUX bus transformers are located on MUX matrix assemblies and their purpose is to provide impedance matching and short-circuit protection.

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  • 45. 

    How many MFL memory locations does the MMC contain?

    • 15

    • 16

    • 17

    • 18

    Correct Answer
    A. 17
    Explanation
    The MMC (Memory Management Controller) contains 17 MFL (Memory Function Logic) memory locations. This means that the MMC has the capability to store and manage data in 17 different memory locations.

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  • 46. 

    UFC priority functions are made available through the priority function keys, only when the 

    • CNI page is displayed on the DED

    • MISC page is displayed on the MFD

    • MISC page is displayed on the DED

    • CNI page is displayed on the MFD

    Correct Answer
    A. CNI page is displayed on the DED
    Explanation
    The UFC priority functions can only be accessed when the CNI page is displayed on the DED. This means that the user must navigate to the CNI page on the DED in order to access and utilize the priority function keys. The priority functions are not available on any other page or display.

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  • 47. 

    On the F-16 CMFD symbology, the circle around the target symbol indicates the  

    • Velocity of the target

    • Target is in missle range

    • Tracking of a friendly aircraft

    • Target is next to shoot

    Correct Answer
    A. Target is next to shoot
    Explanation
    The circle around the target symbol on the F-16 CMFD symbology indicates that the target is next to shoot. This means that the F-16 aircraft is currently locked onto the target and is ready to engage it with its weapons. The circle serves as a visual cue for the pilot, indicating that the target is within range and can be engaged effectively.

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  • 48. 

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

    • MMC power switch

    • SMS standby power switch

    • MMC master switch

    • Stores station switch

    Correct Answer
    A. Stores station switch
    Explanation
    The correct answer is Stores station switch. This switch would be used to provide standby power to all SMS stores stations that have inventory loaded in memory. The other options, such as MMC power switch, SMS standby power switch, and MMC master switch, do not specifically mention the functionality of providing standby power to the stores stations. Therefore, the stores station switch is the most appropriate choice for this scenario.

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  • 49. 

    If the pilot wants to eliminate moving targets on the ground that may show up as airborne targets while the antenna is in a down-look situation, what two velocity thresholds can be selected while in A/A radar mode?

    • 120 or 240 knots

    • 200 or 400 knots

    • 1,200 or 2,400 knots

    • 2,000 or 4,000 knots

    Correct Answer
    A. 1,200 or 2,400 knots
    Explanation
    In order to eliminate moving targets on the ground that may appear as airborne targets, the pilot can select two velocity thresholds while in A/A radar mode: 1,200 knots or 2,400 knots. These thresholds allow the radar system to filter out ground targets that are moving at speeds below the selected thresholds, ensuring that only actual airborne targets are detected and displayed on the radar screen.

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Quiz Review Timeline (Updated): Mar 21, 2023 +

Our quizzes are rigorously reviewed, monitored and continuously updated by our expert board to maintain accuracy, relevance, and timeliness.

  • Current Version
  • Mar 21, 2023
    Quiz Edited by
    ProProfs Editorial Team
  • Mar 05, 2014
    Quiz Created by
    Warthog93
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