Vol 3
For 2A374
- 1.
How many internal fuel tanks does the F–16 aircraft have?
- A.
Six.
- B.
Seven.
- C.
Eight.
- D.
Twelve.
Correct Answer
B. Seven. -
- 2.
How many fuel probes are in each F–16’s external wing tank?
- A.
One.
- B.
Two.
- C.
Three.
- D.
Four.
Correct Answer
C. Three. -
- 3.
On the F–16 aircraft, two low-level sensors and two air ejector control sensors are found on the fuel probes of the
- A.
F–2 and A–1 tanks.
- B.
F–1 and aft reservoir tanks.
- C.
Forward and aft reservoirs.
- D.
A–1 and forward reservoir tanks.
Correct Answer
C. Forward and aft reservoirs. -
- 4.
What F–16 fuel level sensing component(s) provides for control and operation of the air ejector valves?
- A.
Reservoir tank units.
- B.
Fuel low-level sensors.
- C.
Fuel level control unit.
- D.
Fuel quantity control unit.
Correct Answer
C. Fuel level control unit. -
- 5.
For an F–16C, at approximately how many pounds of fuel will the FWD FUEL LOW or AFT FUEL LOW lights illuminate?
- A.
250 pounds forward; 500 pounds aft.
- B.
250 pounds forward; 400 pounds aft.
- C.
400 pounds forward; 350 pounds aft.
- D.
400 pounds forward; 250 pounds aft.
Correct Answer
D. 400 pounds forward; 250 pounds aft. -
- 6.
What F–16 flight environmental pressure is sensed by small holes located on the sides of the pitot and air data probes?
- A.
Pitot.
- B.
Static.
- C.
Impact.
- D.
Differential.
Correct Answer
B. Static. -
- 7.
What F–16 device measures impact pressure?
- A.
Differential pressure sensor.
- B.
Air data probe pneumatic system.
- C.
Pitot-static probe pneumatic system.
- D.
Angle of sideslip pneumatic system.
Correct Answer
A. Differential pressure sensor. -
- 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
- A.
Flight control computer (FLCC).
- B.
Pneumatic sensor assembly (PSA).
- C.
Electronic component assembly (ECA).
- D.
Digital flight control computer (DFLCC).
Correct Answer
B. Pneumatic sensor assembly (PSA). -
- 9.
What F–16 component(s) receive air data inputs from the air data probe pneumatic system?
- A.
Altimeter.
- B.
Airspeed mach indicator (AMI).
- C.
Pneumatic sensor assembly (PSA).
- D.
PSA and central air data computer (CADC).
Correct Answer
C. Pneumatic sensor assembly (PSA). -
- 10.
The angle of sideslip pneumatic system routed air data pressures to the
- A.
Differential pressure sensor (DPS).
- B.
Pneumatic sensor assembly (PSA).
- C.
Electronic component assembly (ECA).
- D.
Digital flight control computer (DFLCC).
Correct Answer
A. Differential pressure sensor (DPS). -
- 11.
What type(s) of inputs are required by the F–16 central air data computer (CADC) to do its job?
- A.
Pitot and static pressures.
- B.
Pneumatic and electrical.
- C.
Static pressure only.
- D.
Pneumatic only.
Correct Answer
B. Pneumatic and electrical. -
- 12.
What F–16 component supplies it with altitude data when in ELEC (electric) mode?
- A.
Electronic component assembly (ECA).
- B.
Modular mission computer (MMC).
- C.
Differential pressure sensor (DPS).
- D.
Central air data computer (CADC).
Correct Answer
D. Central air data computer (CADC). -
- 13.
What F–16 component develops the vertical velocity indicator’s (VVI) vertical velocity signal?
- A.
VVI.
- B.
Flight control computer (FLCC).
- C.
Pneumatic sensor assembly (PSA).
- D.
Central air data computer (CADC).
Correct Answer
D. Central air data computer (CADC). -
- 14.
The F–16 angle-of-attack (AOA) indicator is considered a
- A.
Back-up indicator.
- B.
Vertical tape indicator.
- C.
Self-contained indicator.
- D.
Horizontal tape indicator.
Correct Answer
B. Vertical tape indicator. -
- 15.
The F–16 digital flight control computer (DFLCC) can communicate on which avionics multiplex bus(s)?
- A.
A and B-multiplex (MUX).
- B.
D and EW MUX.
- C.
A and D MUX.
- D.
B and D MUX.
Correct Answer
C. A and D MUX. -
- 16.
What is the F–16 digital flight control system angle-of-attack (AOA) transmitter probe’s travel rotation?
- A.
50 degrees.
- B.
75 degrees.
- C.
100 degrees
- D.
125 degrees
Correct Answer
C. 100 degrees -
- 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?
- A.
1.
- B.
2.
- C.
3.
- D.
4.
Correct Answer
A. 1. -
- 18.
The selected roll autopilot mode on the F–16 will only engage when either pitch attitude hold or
- A.
Pitch altitude hold is engaged.
- B.
Pitch altitude hold is disengaged.
- C.
Terrain following radar is engaged.
- D.
Terrain following radar is disengaged.
Correct Answer
A. Pitch altitude hold is engaged. -
- 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?
- A.
Stability augmentation.
- B.
Command augmentation.
- C.
Automatic angle-of-attack (AOA) limiting.
- D.
Automatic leading edge flap (LEF) positioning.
Correct Answer
B. Command augmentation. -
- 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?
- A.
Override control.
- B.
Gain scheduling.
- C.
Automatic spin prevention.
- D.
Aileron rudder interconnect.
Correct Answer
B. Gain scheduling. -
- 21.
On F–16s, what is the range of movement for the horizontal stabilizers?
- A.
21 up or down from streamline.
- B.
23 up or down from streamline.
- C.
20 down to 23 up from streamline.
- D.
23 down to 20 up from streamline.
Correct Answer
A. 21 up or down from streamline. -
- 22.
On F–16s, what deflects simultaneously with the flaperons in response to roll command signals?
- A.
Rudder.
- B.
Speed brakes.
- C.
Horizontal tail surfaces.
- D.
Leading edge flaps (LEF).
Correct Answer
C. Horizontal tail surfaces. -
- 23.
The range of movement of the F–16 rudder is how many degrees left or right of streamline?
- A.
20 degrees
- B.
30 degrees
- C.
25 degrees
- D.
35 degrees
Correct Answer
B. 30 degrees -
- 24.
On F–16s, the speed brake panels open symmetrically to a maximum of
- A.
43 degrees each
- B.
50 degrees each
- C.
60 degrees each
- D.
To a toal of 110 degrees
Correct Answer
C. 60 degrees each -
- 25.
The F–16 speed brakes receive hydraulic pressure from which hydraulic system(s)?
- A.
A.
- B.
B.
- C.
Both A and B jointly.
- D.
Both A and B alternately.
Correct Answer
A. A. -
- 26.
On the F–16, what allows pitch and roll attitude adjustments to be made while either autopilot attitude (ATT) mode is engaged?
- A.
Heading select (HDG SEL).
- B.
Relaxed static stability.
- C.
ALT (altitude) HOLD.
- D.
Control stick steering.
Correct Answer
D. Control stick steering. -
- 27.
The range of movement for the F–16 leading edge flaps (LEF) is limited to
- A.
2 degrees up to 25 degrees down.
- B.
25 degrees up to 2 degrees down.
- C.
1–1/2 inch up to 12 inches down.
- D.
1 inch down to 12–1/2 inches up.
Correct Answer
A. 2 degrees up to 25 degrees down. -
- 28.
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?
- A.
LOCK.
- B.
AUTO.
- C.
NORM.
- D.
EXTEND.
Correct Answer
B. AUTO. -
- 29.
On the F–16, the modular mission computer (MMC) multiplex (MUX) bus architecture incorporated the addition of which MUX buses?
- A.
A MUX and F MUX.
- B.
B MUX and F MUX.
- C.
C MUX and F MUX.
- D.
D MUX and F MUX.
Correct Answer
C. C MUX and F MUX. -
- 30.
On the F–16, how many different levels of modular mission computer (MMC) degradation exist?
- A.
2.
- B.
3.
- C.
4.
- D.
5.
Correct Answer
B. 3. -
- 31.
On the F–16C/D fire control radar (FCR), what component provides high-power amplification of the transmit signal?
- A.
Modular low-power radio frequency unit (MLPRF).
- B.
Programmable signal processor (PSP).
- C.
Dual-mode transmitter (DMT).
- D.
Antenna.
Correct Answer
C. Dual-mode transmitter (DMT). -
- 32.
On the F–16C/D, the antennal elevation (ANT ELEV) control and radar CURSOR/ENABLE switches are located on the
- A.
Modular low-power radio frequency assembly (MLPRF).
- B.
Pressure regulator/relief valve.
- C.
Waveguide assembly.
- D.
Throttle grip.
Correct Answer
D. Throttle grip. -
- 33.
On the F–16C/D, what component ensures there will be no arcing within the waveguide during operational flight conditions?
- A.
Pressure regulator/relief valve.
- B.
Dual-mode transmitter (DMT) interface buffer.
- C.
Modular low-power radio frequency (MLPRF) P1 assembly.
- D.
Programmable signal processor (PSP) dual-central processing unit.
Correct Answer
A. Pressure regulator/relief valve. -
- 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
- A.
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
- B.
Cursor switch on the throttle grip and the pinky switch on the side stick controller.
- C.
FOV switch on the throttle grip and the pinky switch on the side stick controller.
- D.
Pinky switch on the side stick controller or the FOV switch on the MFD.
Correct Answer
D. Pinky switch on the side stick controller or the FOV switch on the MFD. -
- 35.
During the F–16C/D fire control radar (FCR) power down sequence, how is the antenna positioned?
- A.
30 degrees left and 30 degrees up.
- B.
30 degrees left and 60 degrees up.
- C.
60 degrees left and 30 degrees up.
- D.
60 degrees left and 60 degrees up.
Correct Answer
C. 60 degrees left and 30 degrees up. -
- 36.
What is the maximum azimuth scan limits of the F–16C/D radar antenna?
- A.
Plus or equal to 10 degrees, for a total of 20 degrees of scan.
- B.
Plus or equal 30 degrees, for a total of 60 degrees of scan.
- C.
Plus or equal 60 degrees, for a total of 120 degrees of scan.
- D.
Plus or equal 120 degrees, for a total of 240 degrees of scan.
Correct Answer
C. Plus or equal 60 degrees, for a total of 120 degrees of scan. -
- 37.
Which F–16 advanced identification friend or foe (AIFF) system transponder and interrogator mode is used for altitude reporting?
- A.
1.
- B.
2.
- C.
3.
- D.
C.
Correct Answer
D. C. -
- 38.
On the F–16 advanced identification friend or foe (AIFF) system, which switch is used to command a SCAN interrogation?
- A.
RF.
- B.
C&I.
- C.
TMS.
- D.
IFF MASTER.
Correct Answer
C. TMS. -
- 39.
Which symbology will be displayed when the F–16 advanced identification friend or foe (AIFF) system receives a friendly response?
- A.
Open circle.
- B.
Closed circle.
- C.
Open square.
- D.
Closed square.
Correct Answer
A. Open circle. -
- 40.
Which F–16 advanced identification friend or foe (AIFF) system mode enables traffic identity operation?
- A.
1.
- B.
2.
- C.
4.
- D.
3/A.
Correct Answer
D. 3/A. -
- 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?
- A.
Fixed notch filter.
- B.
Interference blanker.
- C.
Switched notch filter.
- D.
Remote power supply.
Correct Answer
A. Fixed notch filter. -
- 42.
On the F–16 multifunction information distribution system (MIDS) system, the LINK–16 participants must be
- A.
Synchronized.
- B.
On the same channel.
- C.
On different channels.
- D.
Using separate networks.
Correct Answer
A. Synchronized. -
- 43.
When the F–16 multifunction information distribution system (MIDS) achieves a fine synchronization, what is displayed?
- A.
FINE.
- B.
SYNC.
- C.
READY
- D.
LINK–16.
Correct Answer
A. FINE. -
- 44.
On the F–16 multifunction information distribution system (MIDS), which color and shape is used to identify a LINK–16 friend?
- A.
Green circle.
- B.
Red triangle.
- C.
White square.
- D.
Yellow square.
Correct Answer
A. Green circle. -
- 45.
Which F–16 digital video recorder system component controls the electrical power to the digital video recorder (DVR)?
- A.
Video SEL switch panel.
- B.
Airborne video tape recorder (AVTR) panel.
- C.
Cockpit television sensor electronics unit (CTVS E/U).
- D.
Cockpit television sensor (CTVS) video sensor head (VSH).
Correct Answer
B. Airborne video tape recorder (AVTR) panel. -
- 46.
Which U–2 component performs bus control for the U–2 aircraft 1553B NAV and 1553 C&D bus?
- A.
Avionics processor (AVP).
- B.
Up-front controller (UFC).
- C.
Multifunction display (MFD).
- D.
Bus control display unit (BCDU).
Correct Answer
A. Avionics processor (AVP). -
- 47.
In which two modes does the U–2 aircraft multifunction display (MFD) operate?
- A.
Normal and Nav.
- B.
Default and Edit.
- C.
Flight and Support.
- D.
Initiated and Periodic.
Correct Answer
B. Default and Edit. -
- 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?
- A.
Avionics processor (AVP).
- B.
Up-front controller (UFC).
- C.
Multifunction display (MFD).
- D.
Bus control display unit (BCDU).
Correct Answer
B. Up-front controller (UFC). -
- 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?
- A.
IFF Key.
- B.
FIX Key.
- C.
NAV Key.
- D.
HOM Key.
Correct Answer
A. IFF Key. -
- 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?
- A.
G Key.
- B.
BULL Key.
- C.
TIME Key.
- D.
EMER Key.
Correct Answer
B. BULL Key. -
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Mar 04, 2015Quiz Edited by
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