Avionics 2a352g Volume 2
- 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
Correct Answer
B. PRIMARY BUS CONTROLLER FOR THE SERIAL DIGITAL BUSESExplanation
The most important responsibility of the Enhanced Expanded Fire Control Computer is to serve as the primary bus controller for the serial digital buses. This means that it is responsible for coordinating and managing the communication between various avionics systems on the F-16 aircraft through the serial digital buses. It plays a crucial role in integrating the entire avionics system by controlling the flow of data and ensuring that information is properly transmitted and received between different components of the aircraft.Rate this question:
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- 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
Correct Answer
C. ACIUExplanation
The ACIU (Armament Control Interface Unit) backs up the Enhanced Expanded Fire Control Computer on Block 25 in the event of a failure. The ACIU is responsible for providing inputs and outputs to the fire control system, ensuring that it continues to function properly even if there is a failure in the primary computer.Rate this question:
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- 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
Correct Answer
D. CENTRAL PROCESSING UNITExplanation
The correct answer is the Central Processing Unit (CPU). The CPU is responsible for performing all arithmetic calculations as directed by the enhanced expanded fire control computer operational flight program. It is the main component of a computer system that carries out instructions and performs calculations, making it the logical choice for performing arithmetic calculations in this scenario.Rate this question:
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- 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
Correct Answer
B. ON MUX MATRIX ASSEMBLIES, 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
Correct Answer
B. 3, COMMAND, DATA, AND STATUSExplanation
The EEFCC bus protocol uses three message words: COMMAND, DATA, and STATUS. These words are used to transmit information and instructions between devices using the EEFCC bus protocol. The COMMAND word is used to specify the desired action or operation, the DATA word is used to transmit the actual data or information, and the STATUS word is used to indicate the status or result of the operation.Rate this question:
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- 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
Correct Answer
C. ODD PARITY BITExplanation
The EEFCC determines if a transmitted word is good or bad by using the odd parity bit. The odd parity bit is added to the transmitted word to ensure that the total number of 1s in the word, including the parity bit, is always odd. If the number of 1s is even, it means that there is an error in the transmission. Therefore, the EEFCC can identify if a transmitted word is good or bad based on the odd parity bit.Rate this question:
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- 7.
WHAT TRANSMITS THE STATUS WORD?
- A.
SLAVE TERMINAL
- B.
MUX BUS TRANSFORMER
- C.
ACIU
- D.
EEFCC
Correct Answer
A. SLAVE TERMINALExplanation
A slave terminal is responsible for transmitting the status word. It is a device that receives commands from a master terminal and performs actions accordingly. In this case, the slave terminal is transmitting the status word, which could be a signal or data indicating the current state or condition of the system. The other options mentioned, such as MUX bus transformer, ACIU, and EEFCC, are not relevant in the context of transmitting the status word.Rate this question:
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- 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
Correct Answer
C. IT'S A SELF-RUNNING TEST AND WHEN COMPLETE, STARTS OVER AGAINExplanation
The correct answer is "IT'S A SELF-RUNNING TEST AND WHEN COMPLETE, STARTS OVER AGAIN". This statement suggests that the EEFCC (Enhanced Electronic Flight Control Computer) self-test is automated and continuous. It runs on its own without the need for operator command and once the test is complete, it starts over again. This implies that the self-test is ongoing and constantly checks the functionality of the EEFCC.Rate this question:
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- 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
Correct Answer
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 BATTERYExplanation
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 if the main aircraft battery fails or needs to be removed or recharged, the lithium battery in the modular mission computer (MMC) will provide power as a backup. This ensures that the MMC can continue to function properly even if the main power source is unavailable.Rate this question:
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- 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
Correct Answer
B. MMC POWER SWITCH, AVIONICS POWER PANELExplanation
The correct answer is MMC POWER SWITCH, AVIONICS POWER PANEL. This is because the MMC (Maintenance Mode Control) is turned on by the power switch located on the Avionics Power Panel.Rate this question:
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- 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
Correct Answer
B. MISSION PROCESSING SETExplanation
The correct answer is MISSION PROCESSING SET. The mission processing set provides general processing capabilities for the MMC OFP (Mission Management Computer Operational Flight Program), generates symbology, and provides the interface for the head-up display pilot's display unit. This set is responsible for processing and managing the various tasks and functions required for mission execution and display.Rate this question:
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- 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
Correct Answer
B. MISSION PROCESSING SETExplanation
The mission processing set handles the majority of discrete and analog communications with the rest of the F-16 avionics. This module set is responsible for processing mission-related data and information, such as sensor inputs, navigation data, and communication signals. It ensures that the information is properly received, processed, and distributed to the relevant avionics systems and components, allowing for effective mission execution and communication with other aircraft or ground stations.Rate this question:
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- 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
Correct Answer
A. THE PARALLEL INTERMODULE BUS/SERIAL DIGITAL TEST AND MAINTENANCE BUSExplanation
The correct answer is the Parallel Intermodule Bus/Serial Digital Test and Maintenance Bus. This bus provides communication between modules and is used for testing and maintenance purposes. It allows modules to exchange data and perform diagnostic tests. The other options provided do not accurately describe the internal MMC buses that provide communication between modules.Rate this question:
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- 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
Correct Answer
C. MMC HAS TWO ADDITIONAL BUSES: CMUX AND FMUXExplanation
The given answer states that MMC has two additional buses, CMUX and FMUX, compared to the EEFCC. This implies that the architecture of the EEFCC and MMC MUX buses is the same, except for the absence of AMUX and BMUX in both the EEFCC and MMC. The answer highlights the key difference between the two architectures by mentioning the additional buses present in the MMC.Rate this question:
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- 15.
WHAT IS THE BACKUP BUS CONTROLLER FOR THE MMC?
- A.
ACIU
- B.
ECIU
- C.
XFCC
- D.
CMFDS
Correct Answer
D. CMFDSExplanation
The backup bus controller for the MMC is CMFDS.Rate this question:
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- 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
Correct Answer
A. PDU MOISTURE INDICATOR IS PINKExplanation
The excessive moisture in the HUD pilot's display unit is indicated by the pink color on the PDU moisture indicator. This suggests that there is a high level of moisture present, which could potentially affect the functionality and visibility of the HUD.Rate this question:
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- 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
Correct Answer
D. LOW ALTITUDE NAVIGATION AND TARGETING INFRARED FOR NIGHT HUDExplanation
The Low Altitude Navigation and Targeting Infrared for Night (LANTIRN) HUD has the largest field of view display surface.Rate this question:
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- 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
Correct Answer
A. DATA ENTRYExplanation
The integrated control panel is located on the HUD PDU and it is assigned to the data entry subsystem. This means that the control panel is used for inputting and manipulating data within the system. It is responsible for allowing the user to enter and edit information, making it an essential component for data management and control.Rate this question:
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- 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
Correct Answer
C. SYMExplanation
The correct answer is SYM. This control is also an on/off switch that applies power to the HUD.Rate this question:
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- 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
Correct Answer
D. THE ENERGY MANAGEMENT SWITCHExplanation
The correct answer is the energy management switch. This switch controls the display of various scales on the HUD (Head-Up Display). The HUD is a transparent display that presents information without requiring the user to look away from their usual viewpoint. The energy management switch allows the pilot to manage and monitor the aircraft's energy, which includes factors such as speed, altitude, and fuel consumption. By controlling the display of scales on the HUD, the pilot can easily access and interpret this important information during flight.Rate this question:
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- 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
Correct Answer
C. CAS, TAS AND GND SPDExplanation
The three airspeed presentations available when the velocity switch on the HUD remote control panel is used are CAS (Calibrated Airspeed), TAS (True Airspeed), and GND SPD (Ground Speed). CAS represents the airspeed corrected for instrument and position errors, TAS represents the airspeed corrected for altitude and temperature, and GND SPD represents the speed of the aircraft relative to the ground.Rate this question:
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- 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
Correct Answer
B. INCREASESExplanation
When the automatic brightness feature is selected with the brightness switch, the HUD adjusts its brightness based on the ambient light conditions. If the ambient light increases, the HUD will increase its brightness to ensure optimal visibility for the user. Therefore, the correct answer is "INCREASES".Rate this question:
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- 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
Correct Answer
C. PRI OR STBYExplanation
On the HUD remote control panel, you can check the primary and standby reticle by placing the reticle depression switch to either PRI or STBY. This means that you can select either the primary or standby reticle to be displayed on the HUD by using the switch. The primary reticle is the main or default reticle, while the standby reticle is a backup or secondary reticle. By checking both reticles, pilots can ensure that they have a functioning backup in case the primary reticle fails.Rate this question:
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- 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
Correct Answer
C. ASTERISK IN THE UPPER LEFT SIDE OF THE HUDExplanation
The correct answer is "ASTERISK IN THE UPPER LEFT SIDE OF THE HUD". This is because the question is asking about how the HUD indicates the sensor of interest. The upper left side of the HUD is where the asterisk is located, which serves as a visual indicator for the sensor of interest.Rate this question:
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- 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
Correct Answer
A. 3 OCLOCKExplanation
The orientation of the steering cue line indicates the bearing to the steer point. In this case, when the steering cue line is at 3 o'clock, it means that the steer point is located 90 degrees to the right of the current position. This suggests that the correct answer is 3 o'clock.Rate this question:
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- 26.
HOW MANY LEVELS OF ENHANCED ENVELOPE GUN SIGHT ARE THERE?
- A.
2
- B.
3
- C.
4
- D.
5
Correct Answer
D. 5Explanation
There are five levels of enhanced envelope gun sight.Rate this question:
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- 27.
THE SIZE OF THE AIR TO AIR MISSILE ALLOWABLE STEERING ERROR CIRCLE DEPENDS ON THE A RANGE TO THE TARGET AND SELECTED FIELD OF VIEW
- A.
RANGE TO THE TARGET AND SELECTED FIELD OF VIEW
- B.
MISSILE TYPE AND SELCTED FOV
- C.
RANGE TO THE TARGET
- D.
MILLILE TYPE ONLY
Correct Answer
B. MISSILE TYPE AND SELCTED FOVExplanation
The size of the air to air missile allowable steering error circle depends on the missile type and selected field of view. This means that the specific type of missile being used and the chosen field of view for targeting will determine the size of the steering error circle. It suggests that different missile types and field of view settings may have different levels of accuracy and precision in hitting the target.Rate this question:
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- 28.
WHAT MODE OF OPERATION IS THE HUD IN IF THE TARGET DESIGNATOR BOX IS 10 MILLIRADIAN ON EACH SIDE WITH A 1 MR PIPPER?
- A.
AIR TO AIR MODE
- B.
AIR TO GROUND MODE
- C.
AIR TO AIR GUNNERY MODE
- D.
AIR TO GROUND GUNNERY MODE
Correct Answer
B. AIR TO GROUND MODEExplanation
The HUD (Head-Up Display) is in the AIR TO GROUND MODE if the target designator box is 10 milliradian on each side with a 1 MR (Milliradian) pipper. In this mode, the HUD is used for targeting and engaging ground-based targets. The 10 milliradian target designator box indicates the size of the target area being designated, while the 1 MR pipper helps with precise aiming at the target. This mode is specifically designed for air-to-ground missions and provides the necessary information and tools for effective ground attack operations.Rate this question:
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- 29.
THE HUD WON'T DISPLAY THE ROLL INDICATOR WHEN THE FOLLOWING CONDITION OCCURS?
- A.
DED OR PFLD DATA IS DISPLAYED ON THE HUD
- B.
WHEN THE FLIGHT PATH MARKERS BANK ROLL INDICATORS ARE ABSENT
- C.
IN DOGFIGHT, WITH AMMUNITION NOT LOADED IN THE GUN
- D.
WHEN INERTIAL NAVIGATION UNIT DATA IS VALID
Correct Answer
A. DED OR PFLD DATA IS DISPLAYED ON THE HUDExplanation
When DED or PFLD data is displayed on the HUD, the roll indicator won't be displayed.Rate this question:
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- 30.
THE AOA BRACKET IS USED AS AN AID DURING
- A.
AIRCRAFT LANDING
- B.
TARGET DETECTION
- C.
AIR COMBAT MODES
- D.
AIRCRAFT BOMBING MODES
Correct Answer
A. AIRCRAFT LANDINGExplanation
The AOA (Angle of Attack) bracket is used as an aid during aircraft landing. It helps pilots determine the optimal angle at which the aircraft should approach the runway for a safe landing. By providing visual cues and reference points, the AOA bracket assists pilots in maintaining the correct attitude and preventing stalling or other landing mishaps.Rate this question:
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- 31.
WHICH ONE OF THE FOLLOWING IS A BACKUP RETICLE USED FOR MANUAL WEAPONS DELIVERY IN THE EVENT OF A HUD FAILURE?
- A.
STANDBY
- B.
PRIMARY
- C.
SECONDARY
- D.
INDEPENDENT
Correct Answer
A. STANDBYExplanation
The correct answer is STANDBY. In the event of a HUD failure, the standby reticle is used as a backup for manual weapons delivery. The standby reticle provides the necessary information and guidance for the pilot to accurately deliver weapons without relying on the HUD. It ensures that the pilot can still effectively engage targets even if the HUD is not functioning properly.Rate this question:
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- 32.
HOW MANY TIMES DOES THE BAROMETRIC ALTITUDE SCALE EXPAND DURING LANDING OPERATIONS?
- A.
2
- B.
5
- C.
20
- D.
50
Correct Answer
B. 5Explanation
During landing operations, the barometric altitude scale expands five times. This expansion is necessary to accurately measure the changing altitude as the aircraft descends. It allows the pilots to have a clear understanding of their vertical position in relation to the ground and helps ensure a safe landing.Rate this question:
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- 33.
WHEN AUTOMATIC RADAR ALTITUDE IS UNAVAILABLE, THE RADAR ALTITUDE DIGITAL READOUT BLANKS, THE WINDOW FLASHES, AND THE
- A.
ALTITUDE SCALE VANISHES
- B.
SYSTEM SWITCHES TO MANUAL RADAR ALTITUDE
- C.
VERTICAL VELOCITY SCALE REPLACES THE AUTOMATIC RADAR ALTITUDE SCALE
- D.
BAROMETRIC ALTITUDE SCALE REPLACES THE AUTOMATIC RADAR ALTITUDE SCALE
Correct Answer
D. BAROMETRIC ALTITUDE SCALE REPLACES THE AUTOMATIC RADAR ALTITUDE SCALEExplanation
When the automatic radar altitude is unavailable, the radar altitude digital readout blanks, the window flashes, and the altitude scale vanishes. In this situation, the system switches to the barometric altitude scale, which replaces the automatic radar altitude scale. This means that the pilot will rely on the barometric altitude scale to determine their altitude instead of the radar altitude.Rate this question:
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- 34.
WHAT INFORMS THE OPERATOR THAT AN OPTION SELECT SWITCH HAS BEEN ACTUATED?
- A.
THE COPILOT
- B.
A TONE IN THE HEADSET
- C.
A MOMENTARY FLASH ON THE MFD
- D.
A TONE IN THE HEADSET AS WELL AS A MOMENTARY FLASH ON THE MFD
Correct Answer
C. A MOMENTARY FLASH ON THE MFDExplanation
When an option select switch is actuated, the operator is informed by a momentary flash on the MFD (Multi-Function Display). This visual cue provides immediate feedback to the operator, indicating that the switch has been activated. The flash on the MFD serves as a clear and visible indication, allowing the operator to confirm that their input has been registered.Rate this question:
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- 35.
EACH ROCKER SWITCH OPERATES AS
- A.
A DECREASE CONTROL ONLY
- B.
AN INCREASE CONTROL ONLY
- C.
AN INCREASE/DECREASE CONTROL
- D.
AN ON/OFF CONTROL FOR THE APPROPRIATE SUBSYSTEM
Correct Answer
C. AN INCREASE/DECREASE CONTROLExplanation
The correct answer is "AN INCREASE/DECREASE CONTROL". This means that each rocker switch can be used to both increase and decrease the control of a certain subsystem. It allows the user to adjust the level or intensity of the subsystem in both directions, providing flexibility and control over its operation.Rate this question:
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- 36.
WHAT PROVIDES A COMMUNICATION LINK BETWEEN THE MFDs AND THE PROGRAMMABLE DISPLAY GENERATOR?
- A.
THE D MUX
- B.
THE SYSTEM FUNCTION PROCESSOR
- C.
THE DISPLAY FUNCTION PROCESSOR
- D.
THE UNIVERSOAL ASYNCHRONOUS RECEIVER TRANSMITTER
Correct Answer
D. THE UNIVERSOAL ASYNCHRONOUS RECEIVER TRANSMITTERExplanation
The Universal Asynchronous Receiver Transmitter (UART) provides a communication link between the Multi-Function Displays (MFDs) and the Programmable Display Generator. UART is a hardware device that converts parallel data from the MFDs into serial data for transmission and converts received serial data into parallel data for the MFDs to process. It allows for asynchronous communication, meaning that data can be transmitted without the need for a clock signal. Therefore, the UART acts as a bridge between the MFDs and the Programmable Display Generator, enabling them to exchange information effectively.Rate this question:
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- 37.
AN OSS FUNCTION IS IDENTIFIED BY THE
- A.
MNEMONIC ADJACENT TO THE OSS
- B.
MNEMONIC ENGRAVED ON THE OSS FACE
- C.
NUMBER SEQUENCE ADJACENT TO THE OSS
- D.
NUMBER SEQUENCE ENGRAVED ON THE OSS FACE
Correct Answer
A. MNEMONIC ADJACENT TO THE OSSExplanation
The correct answer is that an OSS function is identified by the mnemonic adjacent to the OSS. This means that the mnemonic, which is a code or abbreviation representing the function, is located next to the OSS (Open Source Software). The OSS function can be determined by looking at the mnemonic engraved or written next to the OSS on its face. This suggests that the mnemonic provides information about the specific function or purpose of the OSS.Rate this question:
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- 38.
SINCE THERE ARE TYPICALLY 11 DISPLAY FORMATS ARE AVAILABLE TO THE USER, A TWELFTH DISPLAY FORMAT WOULD BE POSSIBLE IF
- A.
THE ACTIVE TOWED DECOY SYSTEM IS INSTALLED
- B.
AN ELECTRONIC COUNTERMEASURES POD IS LOADED ON STATION 5
- C.
AN ELECTRONIC COUNTERMEASURES POD IS LOADED ON STATIONS 3, 5, or 7
- D.
A TIME COMPLIANCE TECHNICAL ORDER WOULD HAVE TO BE ACCOMPLISHED
Correct Answer
A. THE ACTIVE TOWED DECOY SYSTEM IS INSTALLEDExplanation
If the active towed decoy system is installed, it would create a twelfth display format for the user. The presence of this system would add an additional option for the user to select from the available display formats, increasing the total number to twelve.Rate this question:
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- 39.
DEPRESSING AND RELEASING THE OPTION SELECT SWITCH OF EITHER SECONDARY FORMAT CAUSES TH EDISPLAY ON THE PARTICULAR MFD TO CHANGE
- A.
MAKING THE NEW FORMAT THE PRIMARY FORMAT
- B.
BUT THIS NEW FORMAT STILL REMAINS AS A SECONDARY FORMAT
- C.
AND PROMPTS THE MFD SET TO ENTER SELF-TEST
- D.
BUT AFTER 10 SECONDS REVERTS BACK TO THE ORIGINAL PRIMARY FORMAT
Correct Answer
A. MAKING THE NEW FORMAT THE PRIMARY FORMATExplanation
Depressing and releasing the option select switch of either secondary format causes the display on the particular MFD to change, making the new format the primary format. However, this new format still remains as a secondary format and prompts the MFD set to enter self-test. After 10 seconds, it reverts back to the original primary format.Rate this question:
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- 40.
THE DISPLAY MANAGEMET SWITCH IS USED TO CONTROL FORMAT STEPPING AND
- A.
INITIALIZES THE FORMAT DISPLAY
- B.
SENSOR OF INTEREST SELECTION
- C.
AS A BACKUP FOR AN INOPERATIVE OSS
- D.
IN CERTAIN SITUATIONS ALLOWS AN INTERCHANGE OF THE LEFT AND RIGHT MFD FORMATS
Correct Answer
B. SENSOR OF INTEREST SELECTIONExplanation
The correct answer is "SENSOR OF INTEREST SELECTION". The display management switch is used to control the selection of sensors that are of interest to the operator. It allows the operator to choose which sensors to display and monitor, based on the specific situation or task at hand. This feature is important for efficient and effective monitoring and control of the system.Rate this question:
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- 41.
THE CIRCLE AROUND THE TARGET SYMBOL INDICATES THE
- A.
VELOCITY OF THE TARGET
- B.
TARGET IS IN MISSILE RANGE
- C.
TRACKING OF A FRIENDLY AIRCRAFT
- D.
TARGET IS THE ONE NEXT TO SHOOT
Correct Answer
D. TARGET IS THE ONE NEXT TO SHOOTExplanation
The correct answer is "TARGET IS THE ONE NEXT TO SHOOT". The circle around the target symbol usually indicates the target that is selected or prioritized for shooting. It helps the shooter to identify the target that needs to be engaged or fired upon next.Rate this question:
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- 42.
WHAT AVIOINICS EQUIPMENT COMPLEMENTS THE UFC SET?
- A.
DISPLAY DATA
- B.
DATA TRANSFER
- C.
UFC
- D.
COMMUNICATION AND NAVIGATION
Correct Answer
B. DATA TRANSFERExplanation
Data transfer complements the UFC set by allowing the transfer of information between different avionics equipment. This enables the UFC to receive and send data to other systems, such as communication and navigation equipment, enhancing its functionality and effectiveness. Data transfer ensures that the UFC has access to the necessary information and can communicate with other systems efficiently, ultimately improving the overall performance and capabilities of the UFC set.Rate this question:
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- 43.
WHERE IS THE DATA ENTRY ELECTRONIC UNIT POWER SUPPLY MOUNTED?
- A.
ON TOP OF THE DEEU
- B.
UNDERNEATH THE REAR COCKPIT SEAT
- C.
BEHIND THE MAIN INSTRUMENT PANEL
- D.
UNDERNEATH THE FORWARD COCKPIT SEAT
Correct Answer
A. ON TOP OF THE DEEUExplanation
The correct answer is "ON TOP OF THE DEEU." The DEEU stands for Data Entry Electronic Unit, and the power supply for this unit is mounted on top of it. This means that the power supply is located above the DEEU, providing it with the necessary electrical power.Rate this question:
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- 44.
EACH LED ON THE DED IS CALLED A
- A.
PIXEL
- B.
LED
- C.
PIXEL FIELD
- D.
LED LIGHT BULB
Correct Answer
A. PIXELExplanation
The correct answer is "PIXEL" because each LED on the DED is referred to as a pixel.Rate this question:
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- 45.
ON F-16D AIRCRAFT, THE DATA ENTRY ELECTRONIC UNIT ACCEPTS INPUTS FROM
- A.
IKP
- B.
ICP
- C.
MFD
- D.
BOTH IKP AND ICP
Correct Answer
D. BOTH IKP AND ICPExplanation
The Data Entry Electronic Unit on the F-16D aircraft accepts inputs from both the Integrated Keyboard and Display (IKP) and the Integrated Control Panel (ICP). This means that pilots can enter and input data using either the IKP or the ICP, providing them with flexibility and convenience in accessing and manipulating information on the aircraft.Rate this question:
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- 46.
IDENTIFY THE FOUR PRIORITY OVERRIDE KEYS WHICH ARE LOCATED ACROSS THE TOP OF THE ICP AND IKP
- A.
COMM1, COMM2, INS, LIST
- B.
COM1, COM2, IFF, LIST
- C.
COM3, COM4, INS, LIST
- D.
COM3, COM4, IFF, LIST
Correct Answer
B. COM1, COM2, IFF, LISTExplanation
The correct answer is COM1, COM2, IFF, LIST. These four priority override keys are located across the top of the ICP and IKP. The COM1 and COM2 keys are used for communication purposes, allowing the user to prioritize and override certain communication channels. The IFF key is used for identifying friend or foe, an important feature in military operations. The LIST key is used to access a list of options or functions, providing additional control and customization.Rate this question:
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- 47.
IF YOU DEPRESS THE LIST PRIORITY OVERRIDE KEY THE UFC WILL DISPLAY A LIST OF SELECTABLE
- A.
INFREQUENTLY ACCESSED MFD PAGES
- B.
INFREQUENTLY ACCESSED DATA PAGES
- C.
FREQUENTLY ACCESSED MFD PAGES
- D.
FREQUENTLY ACCESSED DATA PAGES
Correct Answer
B. INFREQUENTLY ACCESSED DATA PAGESExplanation
When the list priority override key is depressed, the UFC (Up-Front Control) will display a list of selectable infrequently accessed data pages. These pages are not frequently accessed by the user and may contain less commonly used information or functions. This feature allows the user to easily access these pages when needed, without cluttering the display with less frequently used options.Rate this question:
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- 48.
WHAT PAGE IS MORE OR LESS A CONTINUATION OF THE LIST PAGE?
- A.
BINGO
- B.
STEER POINT
- C.
MISC
- D.
THE COMMUNICATION, NAVIGATION AND IDENTIFICATION (CNI)
Correct Answer
C. MISCExplanation
The page that is more or less a continuation of the list page is MISC.Rate this question:
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- 49.
UFC PRIORITY FUNCTIONS ARE MADE AVAILABLE THROUGH THE PRIORITY FUNCTION, ONLY WHEN THE
- A.
CNI PAGE IS DISPLAYED ON THE DED
- B.
MISC PAGE IS DISPLAYED ON THE MFD
- C.
MISC IS DISPLAYED ON THE DED
- D.
CNI PAGE IS DISPLAYED ON THE MFD
Correct Answer
A. CNI PAGE IS DISPLAYED ON THE DEDExplanation
When the CNI (Communication, Navigation, and Identification) page is displayed on the DED (Data Entry Display), the UFC (Up-Front Control) priority functions are made available. This means that the functions can only be accessed and used when the CNI page is shown on the DED.Rate this question:
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- 50.
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
Correct Answer
D. WHEN THE ASTERISKS ARE POSITIONED ABOUT A NUMERIC DATA FIELDExplanation
The correct answer is when the asterisks are positioned about a numeric data field. This means that the UFC (Up-Front Controller) provides the capability to enter numeric data through the ICP/IKP (Integrated Control Panel/Integrated Keyboard and Display) when asterisks (*) are displayed around a numeric data field. This indicates that the field is editable and allows the user to input numerical values.Rate this question:
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