2A375 (F-16/u-2)

Front 1

How many internal fuel tanks does the F–16 aircraft have?

Back 1

Seven

Front 2

How many fuel probes are in each F–16’s external wing tank?

Back 2

Three.

Front 3

On the F–16 aircraft, two low-level sensors and two air ejector control sensors are found on the fuel probes of the

Back 3

forward and aft reservoirs

Front 4

What F–16 fuel level sensing component(s) provides for control and operation of the air ejector valves?

Back 4

Fuel level control unit

Front 5

For an F–16C, at approximately how many pounds of fuel will the FWD FUEL LOW or AFT FUEL LOW lights illuminate?

Back 5

400 pounds forward; 250 pounds aft

Front 6

What F–16 flight environmental pressure is sensed by small holes located on the sides of the pitot and air data probes?

Back 6

Static.

Front 7

What F–16 device measures impact pressure?

Back 7

Differential pressure sensor.

Front 8

The F–16 pitot-static probe pneumatic system supplies air data to the central air data computer (CADC), airspeed Mach indicator (AMI), altimeter, and

Back 8

pneumatic sensor assembly (PSA)

Front 9

What F–16 component(s) receive air data inputs from the air data probe pneumatic system?

Back 9

Pneumatic sensor assembly (PSA)

Front 10

The angle of sideslip pneumatic system routed air data pressures to the

Back 10

differential pressure sensor (DPS).

Front 11

What type(s) of inputs are required by the F–16 central air data computer (CADC) to do its job?

Back 11

Pneumatic and electrical

Front 12

What F–16 component supplies it with altitude data when in ELEC (electric) mode?

Back 12

Central air data computer (CADC)

Front 13

What F–16 component develops the vertical velocity indicator’s (VVI) vertical velocity signal?

Back 13

Central air data computer (CADC)

Front 14

The F–16 angle-of-attack (AOA) indicator is considered a

Back 14

vertical tape indicator

Front 15

The F–16 digital flight control computer (DFLCC) can communicate on which avionics multiplex bus(s)?

Back 15

A and D MUX.

Front 16

What is the F–16 digital flight control system angle-of-attack (AOA) transmitter probe’s travel rotation?

Back 16

100*

Front 17

On the F–16, how many rotary variable differential tranducers (RVDT) does an F–16 digital flight control system (DFLCS) angle-of-attack (AOA) transmitter probe contain?

Back 17

1

Front 18

The selected roll autopilot mode on the F–16 will only engage when either pitch attitude hold or

Back 18

pitch altitude hold is engaged

Front 19

What F–16 flight control system (FLCS) feature smoothes flight control surface movements by modifying pilot commands as a function of air data scheduling?

Back 19

Command augmentation

Front 20

On the F–16, what is the amount of control surface movement in relation to the amount of pressure applied to the side-stick or rudder pedals called?

Back 20

Gain scheduling.

Front 21

On F–16s, what is the range of movement for the horizontal stabilizers?

Back 21

21* up or down from streamline

Front 22

On F–16s, what deflects simultaneously with the flaperons in response to roll command signals?

Back 22

Horizontal tail surfaces

Front 23

The range of movement of the F–16 rudder is how many degrees left or right of streamline?

Back 23

30*

Front 24

On F–16s, the speed brake panels open symmetrically to a maximum of

Back 24

60* each

Front 25

The F–16 speed brakes receive hydraulic pressure from which hydraulic system(s)?

Back 25

A

Front 26

On the F–16, what allows pitch and roll attitude adjustments to be made while either autopilot attitude (ATT) mode is engaged?

Back 26

Control stick steering

Front 27

The range of movement for the F–16 leading edge flaps (LEF) is limited to

Back 27

2* up to 25* down

Front 28

On the F–16, flap position will vary between 2 degrees (1 inch) up and 25 degrees (12–1/2inches) down with the leading edge flaps switch in which position?

Back 28

AUTO.

Front 29

On the F–16, the modular mission computer (MMC) multiplex (MUX) bus architecture incorporated the addition of which MUX buses?

Back 29

C MUX and F MUX

Front 30

On the F–16, how many different levels of modular mission computer (MMC) degradation exist?

Back 30

3

Front 31

On the F–16C/D fire control radar (FCR), what component provides high-power amplification of the transmit signal?

Back 31

Dual-mode transmitter (DMT)

Front 32

On the F–16C/D, the antennal elevation (ANT ELEV) control and radar CURSOR/ENABLE switches are located on the

Back 32

throttle grip

Front 33

On the F–16C/D, what component ensures there will be no arcing within the waveguide during operational flight conditions?

Back 33

Pressure regulator/relief valve

Front 34

On the F–16 fire control radar (FCR), the field of view (FOV) display may be expanded while in ground-map (GM) mode by using the

Back 34

pinky switch on the side stick controller or the FOV switch on the MFD

Front 35

During the F–16C/D fire control radar (FCR) power down sequence, how is the antenna positioned?

Back 35

60* left and 30* up

Front 36

What is the maximum azimuth scan limits of the F–16C/D radar antenna?

Back 36

+/-60* , for a total of 120* of scan

Front 37

Which F–16 advanced identification friend or foe (AIFF) system transponder and interrogator mode is used for altitude reporting?

Back 37

Mode C

Front 38

On the F–16 advanced identification friend or foe (AIFF) system, which switch is used to command a SCAN interrogation?

Back 38

TMS.

Front 39

Which symbology will be displayed when the F–16 advanced identification friend or foe (AIFF) system receives a friendly response?

Back 39

Open circle

Front 40

Which F–16 advanced identification friend or foe (AIFF) system mode enables traffic identity operation?

Back 40

3/A

Front 41

Which F–16 multifunction information distribution system (MIDS) component is installed in the upper antenna path and blocks tactical air navigation (TACAN) transmissions in the identify friend or foe (IFF) transmit frequencies?

Back 41

Fixed notch filter

Front 42

On the F–16 multifunction information distribution system (MIDS) system, the LINK–16participants must be

Back 42

synchronized.

Front 43

When the F–16 multifunction information distribution system (MIDS) achieves a fine synchronization, what is displayed?

Back 43

FINE.

Front 44

On the F–16 multifunction information distribution system (MIDS), which color and shape is used to identify a LINK–16 friend?

Back 44

Green circle

Front 45

Which F–16 digital video recorder system component controls the electrical power to the digital video recorder (DVR)?

Back 45

Airborne video tape recorder (AVTR) panel

Front 46

Which U–2 component performs bus control for the U–2 aircraft 1553B NAV and 1553C&D bus?

Back 46

Avionics processor (AVP)

Front 47

In which two modes does the U–2 aircraft multifunction display (MFD) operate?

Back 47

Default and Edit

Front 48

Which U–2 aircraft component provides a heads-forward capability to monitor and control critical and frequently used communication navigation aids and identification (CNI) systems?

Back 48

Up-front controller (UFC)

Front 49

Which U–2 aircraft up-front control display (UFCD) core key provides the capability to modify modes and codes, zeroize the system, and transmit an emergency message?

Back 49

IFF Key

Front 50

Which U–2 aircraft up-front control display (UFCD) core function key provides radial and range information from a reference point to aircraft position?

Back 50

BULL Key

Front 51

Which U–2 inertial navigation component can also act as an emergency backup, supplying position, velocity, and time data to the position solution?

Back 51

Global positioning system (GPS) receiver

Front 52

What U–2 PIIG inertial navigation unit internal component provides a reference for the measurement of aircraft attitude and keeps the platform level?

Back 52

Gyroscopes.

Front 53

What does the U–2 PIIG inertial navigation system require for the inertial navigation system (INS) alignment to begin?

Back 53

Present position

Front 54

The gyroscopic drift is measured to improve the gyro biases during which U–2 PIIG inertial navigation system (INS) alignment?

Back 54

Fine alignment

Front 55

On the U–2 aircraft, what is the sump quantity indicator measured in for the fuel sump tank quantity system?

Back 55

Gallons.

Front 56

On the U–2, how many sump tanks are in the fuselage that feed fuel to the engines during engine operation?

Back 56

4

Front 57

On the U–2 aircraft, the fuel sump tank quantity indicating system utilizes a reluctance-type probe containing

Back 57

an internal float

Front 58

On the U–2 aircraft, what is the fuel flow scale of the fuel totalizer indicator?

Back 58

Increments of 25 gph from 0–400 gph, then in increments of 100 gph from 400–2,000 gph

Front 59

On the U–2 aircraft, how is flight time remaining displayed on the fuel totalizer indicator?

Back 59

In hours and minutes over the range of 00.00 to 99.59

Front 60

What will the U–2 fuel totalizer indicator fuel remaining quantity automatically default to when the STEP/INC and SET/SHIFT pushbuttons are pushed at the same time?

Back 60

500 gallons

Front 61

What does the U–2 dual oil quantity (analog) indicator left analog liquid crystal diode (LCD) indicate?

Back 61

Engine oil quantity in quarts

Front 62

What U–2 component receives the electrical flap position signal from the wing flap position transmitter?

Back 62

Avionics processor (AP)

Front 63

On the U–2 standby flight display, the NAV button allows selection of how many instrument landing system (ILS) functions?

Back 63

3

Front 64

How many separate pitot static systems are on the U–2 aircraft?

Back 64

Two separate (no. 1 and no. 2)

Front 65

What is the purpose of the vibrator installed on the rear of the U–2 standby altimeter?

Back 65

Prevents the altimeter needle from sticking.

Front 66

On the U–2, what feature is unique to the right pitot tube compared to the left pitot tube?

Back 66

Free air temperature (FAT) sensor

Front 67

On the U–2 aircraft, what is connected to a pushrod that moves the rudder surface in the autopilot air data system (APADS)?

Back 67

Torque tube

Front 68

Which component inside the U–2 autopilot actuator commands the clutch to engage?

Back 68

Control module

Front 69

Which U–2 autopilot control panel (APCP) switch provides a way to manually change the heading of the aircraft when the autopilot is engaged?

Back 69

PUST TO TURN control knob

Front 70

The U–2 air data sensor unit (ADSU) uses total pressure and static pressure inputs from which pitot-static system to generate electronic air data outputs?

Back 70

No. 2

Front 71

On a U–2, why do the four mode select servo switches (lights) on the autopilot control panel (APCP) come on?

Back 71

Show the active mode

Front 72

On a U–2, control surface (elevator) feedback comes from

Back 72

a follow-up synchro mechanically linked to the control surface

Front 73

What other U–2 autopilot mode will be disengaged when ALTITUDE HOLD mode is engaged?

Back 73

MACH HOLD

Front 74

How many command modes does the yaw axis have in the U–2 autopilot?

Back 74

None.

Front 75

What is the air data sensor unit’s (ADSU) primary sensor on a U–2?

Back 75

Micro Air Data Transducer (MADT)

Front 76

What test set replaced the portable data transfer system (PDTS) when reconnaissance avionics maintainability program (RAMP) modified U–2 aircraft hit the flight line?

Back 76

Ground support computer

Front 77

On a U–2, where does the air data engine interface unit send its signal?

Back 77

Electronic fan temperature control (EFTC)

Front 78

Which component provides ON/OFF function for the U–2 ARC–217 high frequency (HF) radio system?

Back 78

Volume control panel

Front 79

On the U–2 aircraft, which component initiates initiated built-in-test (IBIT) and polls the ARC–217 high frequency (HF) system for results?

Back 79

Avionics processor (AVP)

Front 80

On the U–2 ARC–217 high frequency (HF) radio system, how many basic modes of operation are selectable from the up-front control display (UFCD)/multifunction display (MFD)?

Back 80

3

Front 81

When the U–2 ARC–217 high frequency (HF) radio system is powered on, the HF radio be in the mode

Back 81

it was in prior to last shut down

Front 82

What is the U–2 ARC–217 high frequency (HF) radio’s amplitude output in watts when MEDIUM is selected?

Back 82

60

Front 83

Where is the U–2 automatic direction finding (ADF) receiver located?

Back 83

In the top section of the E-bay

Front 84

Which U–2 automatic direction finding (ADF) system component compensates for the deflection of arriving radio signals caused by the wings and fuselage of the aircraft?

Back 84

Quadrantal error corrector

Front 85

When the U–2 automatic direction finding (ADF) control panel MODE CONTROL switch is held in the TEST position, a

Back 85

1020 Hz signal is produced in the audio output and the HSI bearing is driven to 45 degrees

Front 86

Which U–2 ALQ–221 electronic warfare suite (EWS) system component sends the incoming emitter signals to the wingtip receiver processor (WTRP)?

Back 86

Wingtip receivers (WTR)

Front 87

On the U–2 ALQ–221 electronic warfare suite (EWS) system, which component does the low band (LB) processor interface with for threat identification for detected threats?

Back 87

High band (HB) processor

Front 88

On the U–2 ALQ–221 electronic warfare suite (EWS) system, what is the total number of transmit antennas?

Back 88

8

Front 89

On the U–2 ALQ–221 electronic warfare suite (EWS) system, what is the total number of receive antennas?

Back 89

9

Front 90

On the U–2 ALQ–221 electronic warfare suite (EWS) system, what light illuminates when the high band (HB) processor detects an emitter?

Back 90

RCV (receive)

Front 91

Which U–2 ALQ–221 electronic warfare suite (EWS) system component calculates the range, location, and lethality information for both low and high band threats?

Back 91

High band (HB) processor

Front 92

On the U–2 ALQ–221 electronic warfare suite (EWS) system, which built-in-test (BIT) runs every 5 seconds on a non-intrusive basis and does not affect system performance?

Back 92

BBIT.

Front 93

What is the frequency reference generated by the internal rubidium oscillator of the U–2disciplined rubidium oscillator (DRO)?

Back 93

10 megahertz (MHz)

Front 94

What is the operating voltage of the U–2 disciplined rubidium oscillator (DRO)?

Back 94

28 volts direct current (VDC)