MQF

A few predator crewmemebers are authorized a copy of AFI 11-2MQ-1 V3
True False

Smoking is prohibited wihtin ___ ft of the GCS

___ fuel is defined as pre-briefed fuel amount needed to terminate an event and proceed with the remainder of the mission

A ___ indicates operation procedures, techniques, etc., which could result in personal injury and/or loss of life if not carefully followed

Comments, corrections, and questions regarding the TO 1Q-1 (M)B-1 Change 11, TO 1Q-1(M)B-34-1-1, or any phase of the fligh manual program, should be forwarded on AF Form___.

The GDT recieves the___, processes the data, and routes it to the GCS for display on the PSO workstations, while the Ku-band system recieves the ___ and routes it to the GCS for processing and display.

The ___ aircraft has ___ ARC-210 antenna(s) and is secure voice (ARC-210) capable.

the engine killswitch is disabled above ___ knots of airspeed

On___aircraft there are two MAP sensors, the second being a redundant sensor.

when auto fule transer is on, fuel is drawn from the aft fuel tank until ___of fuel has ben burned, then the system will swith to the forward tank. Fuel is drawn from teh forward tank until ___ of fuel has been burned.

Which auto iris setting automatically optimizes the dynamic range of the system to show maximum range of shades in a scene

The ___ is the primary visual interface for monitering the aircraft geographic position.

The active Operational Mission is displayed in what color on teh tracker display (when not highlighted for editing)?

Ku-band telemetry is recorded by the___.

The normal operating temperature for the GCS is ___?

The___ is/are the primary interface between the PSO workstation and the equipment in the Ku-band SATCOM terminal vehicles.

When NAV 1 is selected the system uses GPS data from?

If any servo temp reaches the red range (over ___), that servo is no longer considered reliable and must be replaced.

In which of the following VITs can you find the Prop Svo Temp?

Reference HDDwarnings: ET Low (Yellow) is at or below?

In which VIT can you find MAP 3?

When ___ mode is selected, moving the focus lever full forward or full aft activates the focus motor. Returning the lever back to the center position stops the focusing operation.

The AN/AAS-52 conducts a gain based optimization based on two temperatures when a ___ is commanded.

___ takes longer than ___ because the Thermo-Electric Cooler (TEC) must be stabilized at two preset temperatures and two alignments are performed.

Target elevation is automaticaly determined by the manual input or ___.

Failure to seperate each Emergency Mission waypoint by ___ NM will negate the recovery orbit and may result in loss of the aircraft should lost link occur.

GCS software will automatically delete any mission during upload if it has less than ___ waypoints.

If the flight sensor unit failes, the sstem will automatically selec teh ___. If this occurs, ___ to ensure the INS is providing a good attitude reference.

The MCE will mute command link as soon as C-band up signal strengths are greater than 0% for more than ___ seconds.

To enhance the probability fo a successful handover, a reapplication of the ___ is recommended.

If the RPM drops below ___ while in ___ Mode, that mode is terminated and ___ Mode is automatically enabled to allow the pilot to control the propeller pitch during engine failure.

Wha will Auto-Mux TX 1,2,VQ, and Enerdyne video source.

Recomended descent profile is gear down, ___KIAS, and power as required to maintain engine temperatures

Touching down in excess of ___ feet per minuet rate of descent may result in aircraft damage.

When adjusting the boresight, all use ___ numbers for up and right, and ___ numbers for down and left.

In teh case of a GCS LOSS OF LINE POWER emergency, the UPS and bateries will power the PSO racks for approximately ____ without line power.

If primary and secondary airspeeds exceed a ___KIAS differential, ensure that the Airspeed or Pilot/Static Failure checklist is exectued prior to switching airspeed source.

Servos have a high probability of failure after ___ at ___.

When battery voltage drops below ___ volts, all electrical poer may be lost. Gear must be extended before system drops below ___ volts.

A loss of coolant could be indicated by a large difference (greater than 50 degrees) between CHT and ___.

Turbocharger failure is inidicated by excessive or inadiquate ___, or warning messages on teh HDD.

When turned on both the LRD and Heater draw ___ amps

The "Battery-leaking current" message appers when: Net battery current is greater than ___ amps. Crews should run the applicable ___ checklist.

CHT- tem high warning is recieved when CHT is above 230 F. If this message appears, cross-check CHT and coolant Temp and go to the ___checklist.

In MQ-1B Block 10 aircraft, Engine MAP 1 (or 2) pressure high message appears when MAP 1 (or 2) is above ___ in Hg. Reduce power and if warning does not clear within 30 seconds, go to ___ checklist.

In MQ-1B Block 10 aircraft, Engine MAP 1 (or 2) pressure low message appears when MAP 1 (or 2) is below ___ in Hg. Increase Throttle and if warning does not clear within 30 seconds, go to ___ checklist.

Deadband automatically turns on when __ mode is selected, and __ when another mode is selected.

DTV ___ and ___ FOV have no focus control.

Software in the aircraft prefents arming fo the lasers if less than ___ knots of airspeed indicated.

all target data distance use the following units:

In the AN/AAS-52, the deadband modifier can be set from __ to __.

___Should be selected prior to initiating an AN/AAS-52 reset to prevent rapid gimbal movement when teh AN/AAS-52 is reset.

The AAS-52 equipped with Boresight Enhancement (BE) capability can be calibrated at any temperature and altitude. Which of the following codes indicates that the MTS is BE compliant?

If notn-LEP equipped personell are int eh area to be designated and unable to ensure teh absense of personell using image magnifying devices in the area to be designated. MTS minimum slant range or altitude will be ___?

Laser Firing Indicator will display ___ (Low Power) for conditions where energy output is approx. 80%

The effective slant range of the ROVER system is about ___ NM using an aircraft omni antenna, and over ___ NM using the aircraft directional antenna.

Maximum wind for all aircraft operations is ___ and the maximum gust factor permitted is ___

The AGM-114 requires an acceleration of ___Gs for ___ seconds to arm.

All personel must remain clear of the RPA with hung ordinance for one hour after ___.