MQF Test 1 1-50

1.

2 points

Flying between 78 and 85 KIAS with flaps commanded down will constantly run the flap servos.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.26 Note

True

False

2.

2 points

The EPO switch disconnects _________.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.65.1 Caution

Incoming AC power only

Incoming AC power and UPS output

UPS output

None of the above

3.

2 points

In-flight, ______ mode(s) should be turned off in emergencies only.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.30.2.1 Caution

hold

VPP

cruise

SAS

4.

2 points

The conduct of operations and oil level checks will not interfere with tactical or safety-of-flight operations. If required, these checks may be postponed until such time as they may be accomplished without mission degradation.
Ref: AFI 11-2MQ-1&9V3 Chap: 3 Para: 3.9.2.3

True

False

5.

2 points

A manual wastegate setting can be commanded by the pilot, overriding ___________ control. However, this function is intended for emergency use only.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.10.8.1

VPP

Power Mode

AutoPilot

Both A and C

6.

2 points

If the aircraft is at or above lost link altitude when it goes lost link, it will immediately execute the emergency mission and fly a course to the emergency mission entry waypoint using that point's programmed airspeed and altitude.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: Figure 1-22

True

False

7.

2 points

The emergency mission feature can only be deactivated if "Lost Link OK" is selected in the preprogrammed mode.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.30.3 Note

True

False

8.

2 points

When SAS is engaged in flight, stick commands will not match actual aircraft pitch and roll angles for 0.5 seconds. During this time, GCS stick commands will be interpreted as control surface commands and may contribute to loss of aircraft.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.30.2.1 Warning

True

False

9.

2 points

When Auto Fuel Transfer is on, fuel is drawn from the aft fuel tank until _________ of fuel have been burned, then the system switches to the forward tank. Fuel is drawn from the forward tank until __________ of fuel have been burned.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.15.1

8 gallons, 12 gallons

12 pounds, 8 pounds

8 pounds, 12 pounds

12 gallons, 8 gallons

10.

2 points

The Stall Protect feature provides protection for both positive and negative AOA.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.30.2.6

True

False

11.

2 points

The battery charging cycle may stop for any of the following reasons:
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.17.5

Automatic or Manual Shutoff

Alternator Failure

Battery Heat

All of the above

12.

2 points

After loss of GPS, navigation accuracy degrades at a rate of ___ meters per hour.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.40.1.2

360

45

90

180

13.

2 points

A _____ indicates operating procedures, techniques, etc., which could result in personal injury and/or loss of life if not carefully followed.
Ref: T.O. 1Q-1(M)B-1 Chap: Foreword Para: Warnings, Cautions, and Notes

Warning

Note

Advisory

Caution

14.

2 points

The transmission of the C-Band LOS datalink is referred to as the _____ and _____, while the Ku-Band SATCOM transmissions are called _____ and _____.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.54.1

Transmit, Receive, Command Link, Return Link

Command Link, Return Link, Uplink, Downlink

Uplink, Downlink, Command Link, Return Link

None of the above

15.

2 points

Do not conduct flight into forecast _____ or worse icing and minimize conduct of flight into known icing conditions to the maximum extent possible..
Ref: AFI 11-2MQ-1&9V3 Chap: 4 Para: 4.3.3

moderate

light rime

light

severe

16.

2 points

When Auto Fuel Transfer is set to On, the fuel control software will attempt to balance the aircraft using the previous record of manual fuel use; i.e., it will return the calculated balance to a ____ front-to-back ratio by drawing fuel from the appropriate tank.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.15.1

2:1

2:2

4:1

3:2

17.

2 points

The attitude data system senses aircraft pitch, roll, yaw, acceleration, and heading. It consists of two redundant sensors:
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.33.1

alpha probe, AOA sensor

alpha probe, beta sensor

INS/GPS unit, Flight sensor unit/ magnetometer

Yaw Rate Sensor, Vertical Accelerometer

18.

2 points

The worst takeoff weather (TEMPO or prevailing) must be at or above a ceiling of ____ or _____ above the lowest compatible minima, and a visibility of ____ miles or _____ mile(s) above the lowest compatible minima (assuming no alternate is available).
Ref: AFI 11-2MQ-1&9V3 Chap: 4 Para: 4.2.1.2.1

800, 500, 2, 1

800, 500, 3, 2

1500, 1000, 3, 2

1500, 1000, 4, 3

19.

2 points

The effective slant range of the ROVER system is about ____ nautical miles using an aircraft omni antenna, and over ____ nautical miles using an aircraft directional antenna.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.61.3

20, 70

20, 100

10, 50

10, 70

20.

2 points

The ________feature is the first level of stall protection provided by the autopilot.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.30.2.5

cruise mode

aileron tip stall override

airspeed limit override

stall protect

21.

2 points

The return fuel tray is located in the left main landing gear bay. It returns fuel not used by the fuel injection system to __________.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.14.2

both tanks metering for proper distribution

fuel tank not in use

the wing tanks

the proper fuel tank

22.

2 points

The GPS figure of merit gives an indication of the ___________ of the GPS-only navigation position.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.40.4.3.1

actual accuracy

expected accuracy

attenuation

quality and accuracy

23.

2 points

The ice detector signal stays on for _____ seconds after the ice detector has cleared.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.51.3.2

60

15

45

30

24.

2 points

If the aircraft goes lost link it will maintain the current IFF code during the 51-second heading hold phase.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.48.1

True

False

25.

2 points

Declare minimum fuel as soon as it becomes apparent that an aircraft will commence the initial approach or reach the FAF at the base of intended landing or alternate (if required) with less than _____ lbs.
Ref: AFI 11-2MQ-1&9V3 Chap: 3 Para: 3.11.2

40

25

35

50

26.

2 points

Pilots will abort the mission, regardless of apparent damage or subsequent normaloperation, for any of the following:
Ref: AFI 11-2MQ-1&9V3 Chap: 7 Para: 7.3.1

Bird-strike

Over-G

Uncommanded Flight Control Inputs

Engine Failure

All of the above

27.

2 points

"Normal Recovery Fuel" is defined as the fuel amount at the commencement of the initial approach or at the FAF at the base of intended landing or alternate (if required). This fuel amount will be _____ lbs or higher.
Ref: AFI 11-2MQ-1&9V3 Chap: 3 Para: 3.11.1

75

50

60

40

28.

2 points

The _____ acts as the central control and processing point for aircraft Ku-Band equipment.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.62.2.3

SPMA

SLMA

LMA

PCM

29.

2 points

Which of the following statements is correct regarding the Fuel Pump Rest Cycle?
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.15.2

Both fuel pumps are activated whenever the landing gear is down or the airspeed is less than 40 KIAS

After the landing gear is retracted for 10 minutes and airspeed is above 40 KIAS, one of the fuel pumps is shut off

After one fuel pump has been shut off for 30 minutes, that pump is turned back on and 5seconds later, the other pump is shut off

All the above

30.

2 points

What does DEADEYE mean?
Ref: AFTTP(I) 3-2.5, Brevity Para: N/A

Acquisition of laser designation

Weapons impact

Laser designator system inoperative

Sighting of a friendly aircraft or ground position. Opposite of BLIND

Acknowledges sighting of a specified reference point (either visually or via sensor)

31.

2 points

If the engine is windmilling above _____ RPM, the Engine Start command will have no effect.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.8

1000

1800

1600

2200

32.

2 points

Frequencies set on channels _______ are used for scan mode.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.44.6

20-25

21-25

23-25

22-25

33.

2 points

Brakes are electrically activated. Once the pedal is at its stop pressing harder will not increase braking action.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.23 Note

True

False

34.

2 points

CLEARED TO ENGAGE - JTAC Type 3 control clearance. Attack aircraft flight leaders may initiate attacks within the parameters imposed by the JTAC. Attack platforms will provide ________ .
Ref: AFTTP(I) 3-2.6, JFIRE Chap: IV Para: Fig 4

"Target Engaged"

"Commencing Engagement and Engagement Complete"

"Inbound Attack"

"Engagement Initiated"

35.

2 points

When NAV2 is selected the system uses GPS data from what?
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.40.4.2

The integral GPS unit

FCA1

The LN100G INS/GPS unit

UARB

36.

2 points

Declare emergency fuel as soon as it becomes apparent that an aircraft will commence the initial approach or reach the FAF at the base of intended landing or alternate (if required) with less than _____ lbs of fuel.
Ref: AFI 11-2MQ-1&9V3 Chap: 3 Para: 3.11.3

40

50

45

25

37.

2 points

When operating in VPP Mode the propeller control lever commands propeller pitch. Setting the propeller pitch controls engine and propeller RPM. Moving the lever full forward sets the propeller to its ___________. Moving the lever full aft sets the propeller to its ___________.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.74.3

flight RPM position; ground RPM position

minimum RPM position; maximum RPM position

maximum RPM position; minimum RPM position

ground RPM position; flight RPM position

38.

2 points

The fuel system continues activating the fuel pumps in a 30 minute alternating sequence until one of the following occurs.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.15.2

The landing gear is raised

The fuel pressure drops below minimum or rises above maximum threshold

The airspeed drops below 50 KIAS

None of the above

39.

2 points

If datalink is lost when the aircraft is in flight, the autopilot procedure to set TX 1 and TX 2 Digital Downlink to Off (turns off ROVER operation) will happen during what time frame?
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: Figure 1-25

Arming time + 5 seconds

30 Minutes or Lost Link Altitude Reached

2 to 51 Seconds

52 Seconds to 30 Minutes

40.

2 points

Which statement is false about arming times and aircraft lost link procedures?
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: Figure 1-24

If operating in DLOS mode, the aircraft will not return to standard LOS mode

At two seconds of any lost uplink, the PCM transmits a warning message in the downlink that is presented on the status display in the GCS. This message indicates a lost link condition and the type of link lost

If the aircraft was switched to the C-band uplink from the Ku-band command link the arming time is 60 seconds. This allows time for the C-band datalink to be established

Once an uplink is reestablished, both LOS receivers are placed on the same frequency

41.

2 points

Precipitation adversely affects aircraft performance and reduces visibility. If conditions permit, pilots should minimize exposure to all types of precipitation during all phases of flight.
Ref: AFI 11-2MQ-1&9V3 Chap: 4 Para: 4.2.1.2.1

True

False

42.

2 points

The _________ is/are the primary interface between the PSO workstation processor and the equipment in the Ku-band SATCOM terminal vehicles.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.62.4.1.2

PPSL

J1/J2 Cables

PCM

LMA

43.

2 points

Pilots must be alert to the possible consequences of deactivating SAS during flight. When SAS is deactivated, all __________ safety features are immediately turned off.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.30.2.1 Caution

stall protect

engine over speed protection

autopilot

cruise mode

44.

2 points

Once a "KNOCK IT OFF" is called, all participating aircraft will:
Ref: AFI 11 -214 Chap: 3 Para: 3.4.2

Acknowledge with callsign

Cease tactical maneuvering and the scenario

Deconflict flight paths

All of the above

45.

2 points

"Danger Close" for the AGM-114 is _____ m.
Ref: AFTTP(I) 3-2.6, JFIRE Chap: Appendix F Para: Table 39

100

110

130

120

46.

2 points

Flight sensor unit autopilot data is displayed for pilot reference on VIT 8 as ____ data.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.33.3

FSU

AP1

LN100

AP2

47.

2 points

_____ expresses a provision that is binding.
Ref: T.O. 1Q-1(M)B-1 Chap: Foreword Para: Shall, Will, Should, and May

Shall

If

Will

Should and May

48.

2 points

Cruise mode limits rudder authority to prevent excessive yaw rates and sideslip angles. Yaw commands are limited to ________ in either direction when cruise mode is _______.
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.30.2.3

4°, Off

7°, On

7°, Off

4°, On

49.

2 points

Required equipment for takeoff includes:
Ref: AFI 11-2MQ-1&9V3 Chap: 3 Para: 3.2

Two separate cameras

Operational INS and GPS

IR Sensor for night takeoff

An operable radio suitable for mission accomplishment

All of the above

50.

2 points

When OAT is less than 10 C, the pilot can turn Pitot Heat Off in which De-Icing system mode?
Ref: T.O. 1Q-1(M)B-1 Chap: 1 Para: 1.51.5.1.1 and 1.51.5.1.2

Manual

Automatic

Both

None