Vol 3

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

Acts as a bi-stable input source.

Prevents dust buildup in the indicator.

Prevents the altimeter needle from sticking.

So the pilot can feel the indicator to be sure it is working.

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

Green circle.

Red triangle.

White square.

Yellow square.

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

It was in prior to last shut down.

Selected by the multifunction display (MFD).

Selected by the up-front control display (UFCD).

Selected on the communications (COMM) select panel.

4. 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?

Override control.

Gain scheduling.

Automatic spin prevention.

Aileron rudder interconnect.

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

Separate heating element.

Free air temperature (FAT) sensor.

Water resistant ball to prevent moisture build-up.

Nothing, it’s a hole, holes are empty by definition.

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

Synchronized.

On the same channel.

On different channels.

Using separate networks.

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

An internal float.

A compensator.

A diode adapter.

A rebalancing potentiometer.

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

Pressure regulator/relief valve.

Dual-mode transmitter (DMT) interface buffer.

Modular low-power radio frequency (MLPRF) P1 assembly.

Programmable signal processor (PSP) dual-central processing unit.

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

Quantizers.

Multiplexers.

Gyroscopes.

Accelerometers.

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

Modular low-power radio frequency assembly (MLPRF).

Pressure regulator/relief valve.

Waveguide assembly.

Throttle grip.

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

Plus or equal to 10 degrees, for a total of 20 degrees of scan.

Plus or equal 30 degrees, for a total of 60 degrees of scan.

Plus or equal 60 degrees, for a total of 120 degrees of scan.

Plus or equal 120 degrees, for a total of 240 degrees of scan.

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

1.

2.

4.

3/A.

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

FINE.

SYNC.

READY

LINK–16.

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

Fine alignment.

Coarse alignment.

Power-on alignment.

Initialization alignment.

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

Ground support computer.

Wireless area test set.

Flight line test set.

In-flight monitor.

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

Two separate (no. 1 and no. 2).

Two separate (sys. a and sys. b).

Only one system with two input sources.

Two separate systems that use the same pitot probes as inputs.

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

F–2 and A–1 tanks.

F–1 and aft reservoir tanks.

Forward and aft reservoirs.

A–1 and forward reservoir tanks.

18. 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?

IFF Key.

FIX Key.

NAV Key.

HOM Key.

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

G Key.

BULL Key.

TIME Key.

EMER Key.

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

In hours and minutes over the range of 00.00 to 60.00.

In hours and minutes over the range of 00.00 to 99.59.

In minutes and seconds over the range of 00.00 to 60.00.

In minutes and seconds over the range of 00.00 to 99.59.

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

Pitot.

Static.

Impact.

Differential.

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

Pitot and static pressures.

Pneumatic and electrical.

Static pressure only.

Pneumatic only.

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

1.

2.

3.

C.

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

Back-up indicator.

Vertical tape indicator.

Self-contained indicator.

Horizontal tape indicator.

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

Avionics processor (AP).

Up-front control display (UFCD).

Bus control display unit (BCDU).

Global positioning system (GPS) receiver.

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

Pitch altitude hold is engaged.

Pitch altitude hold is disengaged.

Terrain following radar is engaged.

Terrain following radar is disengaged.

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

Farads.

Pounds.

Gallons.

Tank units.

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

43 degrees each

50 degrees each

60 degrees each

To a toal of 110 degrees

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

0.

10.

60.

175.

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

Acceleration.

Present position.

Destination waypoint.

Current date and time.

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

YAW AXIS CUT-OFF switch.

PUST TO TURN control knob.

NAV mode pushbutton switch.

HDG mode pushbutton switch.

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

Open circle.

Closed circle.

Open square.

Closed square.

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

Normal and Nav.

Default and Edit.

Flight and Support.

Initiated and Periodic.

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

In the top section of the E-bay.

In the bottom section of the E-bay.

On a mounting base under panel F105.

On a mounting base installed in the fixed nose.

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

None.

One.

Two.

Three.

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

Cable drive.

Torque tube.

Servoactuator.

Rudder clamp.

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

26 volts alternating current (VAC).

28 volts direct current (VDC).

110 VAC.

115 VAC.

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

Engine oil quantity in pints.

Engine oil quantity in quarts.

Airframe Mounted Accessory Drive (AMAD) oil quantity in pints.

AMAD oil quantity in quarts.

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

Modular low-power radio frequency unit (MLPRF).

Programmable signal processor (PSP).

Dual-mode transmitter (DMT).

Antenna.

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

Six.

Seven.

Eight.

Twelve.

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

2.

3.

4.

5.

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

Flight control computer (FLCC).

Pneumatic sensor assembly (PSA).

Electronic component assembly (ECA).

Digital flight control computer (DFLCC).

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

30 degrees left and 30 degrees up.

30 degrees left and 60 degrees up.

60 degrees left and 30 degrees up.

60 degrees left and 60 degrees up.

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

10 megahertz (MHz).

20 MHz.

30 MHz.

40 MHz.

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

RF.

C&I.

TMS.

IFF MASTER.

46. 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?

Avionics processor (AVP).

Up-front controller (UFC).

Multifunction display (MFD).

Bus control display unit (BCDU).

47. 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?

ADF receiver

ADF loop antenna.

ADF sense antenna.

Quadrantal error corrector.

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

2.

3.

4.

5.

49. How many fuel probes are in each F–16's external wing tank?

One.

Two.

Three.

Four.

50. 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?

Fixed notch filter.

Interference blanker.

Switched notch filter.

Remote power supply.

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

50 degrees.

75 degrees.

100 degrees

125 degrees

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

Increments of 20 gph from 0–200 gph, then in increments of 100 gph from 200–2,000 gph.

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

Increments of 20 gph from 0–600 gph, then in increments of 100 gph from 600–2,000 gph.

Increments of 25 gph from 0–800 gph, then in increments of 100 gph from 800–2,000 gph.

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

Wingtip receivers (WTR).

Low band (LB) processor.

High band (HB) processor.

High band power amplifiers (HB PA).

54. 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

Cursor switch on the throttle grip and the pinky switch on the side stick controller.

FOV switch on the throttle grip and the pinky switch on the side stick controller.

Pinky switch on the side stick controller or the FOV switch on the MFD.

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

Right switch panel.

COMM select panel.

Volume control panel.

Up front control panel.

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

A.

B.

Both A and B jointly.

Both A and B alternately.

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

860 Hz signal is produced in the audio output and the HSI bearing is driven to 30 degrees.

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

1020 Hz signal is produced in the audio output and the HSI bearing is driven to 30 degrees.

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

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

Electronic component assembly (ECA).

Modular mission computer (MMC).

Differential pressure sensor (DPS).

Central air data computer (CADC).

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

Surface deflection angle detected by the transducer.

Stick deflection as detected by the feel trim actuator.

C channel information fed to the flight control computer.

A follow-up synchro mechanically linked to the control surface.

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

2 degrees up to 25 degrees down.

25 degrees up to 2 degrees down.

1–1/2 inch up to 12 inches down.

1 inch down to 12–1/2 inches up.

61. 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?

SBIT.

IBIT.

PBIT.

BBIT.

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

A and B-multiplex (MUX).

D and EW MUX.

A and D MUX.

B and D MUX.

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

LOCK.

AUTO.

NORM.

EXTEND.

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

Show mode status.

Show the active mode.

Alert the pilot of an axis servo failure.

Inform the pilot that the CPU has taken control of the aircraft.

65. 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?

1.

2.

3.

4.

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

Stability augmentation.

Command augmentation.

Automatic angle-of-attack (AOA) limiting.

Automatic leading edge flap (LEF) positioning.

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

MACH HOLD.

PITCH HOLD.

ATTITUDE HOLD.

HEADING HOLD.

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

Heading select (HDG SEL).

Relaxed static stability.

ALT (altitude) HOLD.

Control stick steering.

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

Avionics processor (AVP).

Bus control display unit (BCDU).

Up-front control display (UFCD).

Communications (COMM) select panel.

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

Rudder.

Speed brakes.

Horizontal tail surfaces.

Leading edge flaps (LEF).

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

20 degrees

30 degrees

25 degrees

35 degrees

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

250 pounds forward; 500 pounds aft.

250 pounds forward; 400 pounds aft.

400 pounds forward; 350 pounds aft.

400 pounds forward; 250 pounds aft.

73. 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?

Wingtip receivers (WTR).

Avionics processor (AVP).

High band (HB) processor.

Wingtip receiver processor (WTRP).

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

RCV (receive).

RPT (repeat).

THRT (threat).

EMIT (emitter).

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

Avionics processor (AVP).

Up-front controller (UFC).

Multifunction display (MFD).

Bus control display unit (BCDU).

76. 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?

200 gallons.

300 gallons.

400 gallons.

500 gallons.

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

A MUX and F MUX.

B MUX and F MUX.

C MUX and F MUX.

D MUX and F MUX.

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

Reservoir tank units.

Fuel low-level sensors.

Fuel level control unit.

Fuel quantity control unit.

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

7.

8.

9.

10.

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

8.

9.

10.

11.

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

VVI.

Flight control computer (FLCC).

Pneumatic sensor assembly (PSA).

Central air data computer (CADC).

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

Video SEL switch panel.

Airborne video tape recorder (AVTR) panel.

Cockpit television sensor electronics unit (CTVS E/U).

Cockpit television sensor (CTVS) video sensor head (VSH).

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

Autopilot computer unit (ACU).

Electronic engine control (EEC).

Angle of attack (AOA) transmitter.

Electronic fan temperature control (EFTC).

84. 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?

Avionics processor (AVP).

Low band (LB) processor.

High band (HB) processor.

Wingtip receiver processor (WTRP).

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

21 up or down from streamline.

23 up or down from streamline.

20 down to 23 up from streamline.

23 down to 20 up from streamline.

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

2.

3.

4.

5.

87. 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)?

2.

3.

4.

5.

88. What F–16 device measures impact pressure?

Differential pressure sensor.

Air data probe pneumatic system.

Pitot-static probe pneumatic system.

Angle of sideslip pneumatic system.

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

Capstan.

Servomotor.

Control module.

DC tach generator.

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

Differential pressure sensor (DPS).

Pneumatic sensor assembly (PSA).

Electronic component assembly (ECA).

Digital flight control computer (DFLCC).

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

Right pitot probe.

Rate sensor unit (RSU).

Free air temperature sensor (FAT).

Micro air data transducer (MADT).

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

Altimeter.

Airspeed mach indicator (AMI).

Pneumatic sensor assembly (PSA).

PSA and central air data computer (CADC).

93. 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?

No. 1.

No. 2.

No. 3.

No. 4.

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

Avionics processor (AP).

Flap position control unit.

Modular mission computer (MMC).

Digital flight control computer (DFLCC).

Vol 3

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

2.

What first name or nickname would you like us to use?

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

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

4. 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?

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

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

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

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

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

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

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

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

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

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

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

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

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

18. 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?

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

46. 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?

47. 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?

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

49. How many fuel probes are in each F–16's external wing tank?

50. 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?

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

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

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

54. 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

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

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

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

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

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

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

61. 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?

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

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

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

65. 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?

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

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

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

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

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

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

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

73. 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?

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

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

76. 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?

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