SO Closed Book Flashcards

1
Q

Change out one crewmember at a time to ensure continuous monitoring of the AC. The ___ is the final authority in determining if circumstances are safe to replace crews.

A

Incoming PIC

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2
Q

Zoom lock prevents an inadvertent change in the selected FOV when________.

A

Firing LRD, LTM, LRD/LTM with auto track engaged

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3
Q

The LRD is firing at a degraded level (LRD LP DES). The energy output is approximately ___% or less. If a weapon has been released ___________. If a weapon has not been released, it is advised to____________.

A

65; continue to lase; abort and cycle the laser

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4
Q

T/F: Both LRD and LTM provide means of obtaining slant range info.

A

False

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5
Q

In the event the AC loses command link/uplink and enters the lost link profile, the lasers are automatically set to __ and ___.

A

OFF; disarmed

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6
Q

What are the max temperature limits for the MTS during an operation and non-operation?

A

+55 and +85*C

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7
Q

The MTS sensor can be used to inspect the ___ of the wing for ice accumulation.

A

Leading edge

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8
Q

Operational techniques, procedures, etc., which could result in damage to equipment if not carefully followed.

A

Caution

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9
Q

___ express non-mandatory provisions.

A

Should and May

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10
Q

The EPO switch disconnects ____.

A

All AC power from the GCS

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11
Q

There are 3 ranges of condition lever settings. The ___ position provides for normal ops, the detent position closes the fuel shutoff valve, and ___ position mechanically feathers the propeller and closes the fuel shutoff valve.

A

Full fwd; full aft

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12
Q

Outboard wing tanks feed the inboard tanks via___.

A

Gravity

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13
Q

Below what fuel feed pressure does the RCM turn on the electric fuel pump that is not in use to supply fuel from the header tank to the engine?

A

15psi

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14
Q

If the header tank exceeds ___psi, a return solenoid failure warning is downlinked to the GCS.

A

4.2

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15
Q

The transmission of the C-band LOS datalink is referred to as the ___ and ___, while Ku-band SATCOM transmissions are called ___ and ___.

A

Uplink and Downlink;
Command link and Return link

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16
Q

___ is indicated by a complete loss of HUD video with continuous presence of telemetry.

A

Video source failure

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17
Q

T/F: The laser PRF code is a direct reflection of the actual pulse rate. The higher PRF code, the faster the laser pulses.

A

False

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18
Q

The accuracy of estimated remaining flight time is reduced when the battery capacity is at or below ___%.

A

20

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19
Q

Do not allow the engine to windmill between ___ and ___% RPM.

A

18 and 28

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20
Q

Gear must be extended before the system drops below ___ volts. Attempting to lower gear with less than ___volts may cause complete loss of battery power.

A

22; 22

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21
Q

When the LRD is ON it typically draws ___ amps (the same as the MTS turret heater).

A

15

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22
Q

If the range to the target is 10km, what is the LTM spot height and width?

A

11x18m

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23
Q

Operational altitude for the LRD and LTM is___.

A

45,000ft

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24
Q

Fast blink fires the LTM ____ times per second. Slow blink fires the LTM ___.

A

3; once every 2 seconds

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25
Q

GCS generated payload graphics are created within ___ using the RS-422 telemetry data embedded in the downlink.

A

GCS

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26
Q

The deadband modifier can adjust the SOs joystick deadband between ___.

A

0-63

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27
Q

Never intentionally point the MTS at the sun. This renders the system inoperable for up to ___.

A

1 minute

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28
Q

GIM DIS ___ code means the EU to Ethernet communication has failed.

A

100

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29
Q

There are 2 over temperature warnings that can appear on the MTS HUD: WRA 1 OVHT (turret) and WRA 2 OVHT (electronics assembly). The temp threshold for both is ___.

A

85*C

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30
Q

When a tracked target is lost due to momentarily obscured, the track enters ____mode. This mode is indicated by the track gate corners___. If the system is able to require track, the track gate corners will return to a ___ display. If the system is unable to require the track, after ___ seconds it will automatically cancel the auto track ode and revert to rate mode.

A

Coast; flashing; solid; 2

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31
Q

Do NOT fire lasers at ____, flat glass, glazed ice, or any other reflective surface.

A

Still water

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32
Q

If the ___ tank fuel pressure does NOT recover and the level continues to drop, the engine will only run until the ___ tank is depleted.

A

Header; header

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33
Q

A jet pump manifold solenoid that fails ___ would prevent fuel from being pumped in the header tank and cause a ___ header tank level. Lockout the affected tank if required.

A

Closed; Low

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34
Q

___ mode is intended to provide the operator stable control of the MTS when flying directly over a target. Effective use of ___ mode requires the AC to fly directly towards the target and then have the target pass through nadir.

A

Vertical; vertical

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35
Q

If excessive gimbal bouncing is encountered while using ___mode, attempt to minimize the length of time that the mode is activated to prevent a possible GIM DIS condition.

A

Targeting

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36
Q

The point track function is designed to keep the sensor aligned with an area of ___.

A

Significant contrast

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37
Q

T/F: During the SO FENCE check, the general flow goes bottom-to-top and right-to-left.

A

False

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38
Q

T/F: Post-impact procedures include pilot commands for “CEASE LASER, SAFE LASER” and “MASER ARM SAFE.”

A

False

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39
Q

The ATLC mission consists of ___ waypoints that define the runway and flight pattern around the airfield.

A

10

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40
Q

Which two files are required for ATLC ops?

A

(A) profile & (C) runway

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41
Q

Once the AC ground speed is less than or equal to ___, ATLC logic will ramp the brakes to 100% over 2 seconds.

A

20knots

42
Q

For ATLC LL logic, the RCM will wait ____ to establish if it is temporary or permanent dropout. If after ___, the link is still severed, the DCM will declare LL.

A

2 & 2 seconds

43
Q

Crews must positively ID all targets prior to weapons release. For training sorties, achieve pos ID either ___ or by confirming ____ via valid onboard/off board cues.

A

Visually; target location

44
Q

T/F: Stores can be jettisoned with nose gear extended.

A

False

45
Q

DEADEYE

A

Laser Designation system inoperative

46
Q

______ acknowledges sighting of a specified reference point.

A

CONTACT

47
Q

______ means the specified surface target or object has been acquired and is being tracked with an onboard sensor.

A

CAPTURED

48
Q

_____ is the sighting of a target, non-friendly AC, or enemy position. Opposite of _____.

A

TALLY; NO JOY

49
Q

LRD PRF code range:

A

1111-1888

50
Q

Do NOT power ON hellfires unnecessarily. Leaving it powered on for extended durations may___.

A

Decrease reliability

51
Q

Which launch mode results in higher impact angles?

A

LOAL-High

52
Q

Which launch mode results in a lower impact angle?

A

LOAL-Low

53
Q

The PRF code entered into the GBU12/51 PRF setting does NOT change the PRF code set____________________.

A

By the load crew into the bombs CCG code select switches.

54
Q

The hellfire gets its targeting parameters ______.

A

Directly from the MTS

55
Q

The ____ has an increased fragmentation ring warhead.

A

AGM114/R9E

56
Q

All personnel must remain clear of AC with hung-fire ordnance for ____ after last attempted launch.

A

1 hour

57
Q

Type 3 control - once satisfied the attacking AC are correlated on the appropriate targets, the JTAC will provide attacking AC “CLEARED TO ENGAGE” or “TYPE 3 CONTINUE DRY” The attack aircrew will report __________ to JTAC.

A

“Commencing engagement” and “engagement complete”

58
Q

If the JTAC required a specific attack heading for the weapon (but not the AC), that restriction ____ be stated clearly when the FAH is passed.

A

MUST

59
Q

Which of the following manners can a JTAC use to provide target location during CAS brief (9line)?

A

(A) Lat/long, (B) grid coords., & (C) offset from known point

60
Q

Friendly grids should not be passed if it can be avoided. If necessary, use no more than ___ digits.

A

6

61
Q

Danger close, final attack headings, and TOTs are all examples of what during CAS briefing (9Line)?

A

Restrictions

62
Q

________ targets are properly validated and placed in the joint target list. Deliberate targets are further broken down into 2 categories: scheduled and on-call.

A

Deliberate

63
Q

Which role is not primary JTAC responsibility?

A

Location

64
Q

UAS either FW or RW operate using similar CAS procedures to manned AC, to include airborne laser procedures. Which is NOT a unique consideration that needs to be addressed when using UAS?

A

Weapons loadout

65
Q

Danger close for GBU 12 is

A

270meters

66
Q

T/F: With wing walkers, avoid taxi obstructions by at least 15ft.

A

False

67
Q

T/F: The pilot will use the TGP to ensure AC is clear of obstructions during taxi?

A

False

68
Q

Maintain safe taxi speeds at all times, not to exceeed _____ knots ground speed (KGS) on taxiway, ____KGS on runway, and less than ____KGS in turn 30* or greater.

A

10; 20; 6

69
Q

Minimum taxi interval between MQ9 AC is : ___ft daytime, ___ft nighttime.

A

150; 300

70
Q

Minimum runway length for MQ9 operation is ___ft.

A

5000

71
Q

Minimum runway width for MQ9 is ____ft while min taxiway width is ___ft.

A

75; 50

72
Q

Pilots will establish normal glide path by ___ft AGL. Descent rates greater than___ft per minute (FPM) below 200AGL, greater than ___FPM below 50AGL, airspeed more than ___KIAS below calculated approach speed, or a PIO/bounce requires a go-around.

A

200; 1200; 800; 5

73
Q

Unless otherwise briefed, SO will announce altitude deviations exceeding +/- ___ft at the IAF, FAF, and min descent Alt, as well as when reaching descent height or missed approach point. IN OTHER WORDS ALL THE FUCKING TIME

A

100

74
Q

For landing, place the MTS in position mode and display flight graphics on both PSO racks no later than ___ft AGL.

A

500

75
Q

Minimum approach airspeed during SFO traffic pattern is stall speed plus ___ KIAS.

A

15

76
Q

Forecast weather must be at or above AFI 11-2MQ9v3 minima at the ETA +/- ____.

A

1 hour

77
Q

When actual or forecasted ceiling is below ____ft and visibility is less than ____NM, aircrew will increase recovery fuel to allow holding for ___ hours over the destination at max endurance speed,……

A

3000; 3; 2

78
Q

A momentary increase in engine RPM and ___ during the shutdown process indicates the purge system is functioning.

A

EGT

79
Q

To perform a normal engine shutdown, the pilot moves the throttle to the ___ position for a minimum of ___minutes.

A

Ground idle; 3

80
Q

T/F: When power is applied to AC, INS function goes through a self-test aligns its sensors, and outputs attitude and navigation data. Moving the AC at this time is I’ll NOT AAFFECT THE INS attitude and nav results.

A

False

81
Q

During AV preflight, many nav health status parameters are presented. The main concern for the operator is that FCA # stat is ____ and FCA # err is ___. Under normal conditions, this will take ____ minutes.

A

F7; 20; 7-9

82
Q

The GPS key code 4400 means:

A

The P-code key is unverified, that it expires in 2 hour or less, and no keys were loaded.

83
Q

During AV preflight the oil level should be ____% or above.

A

90

84
Q

When running the transfer LOS/SATCOM, link test checklist, the pilot and crew chief must ensure the ground personnel are at least ____ft from the AC and the ___ are on before enabling SATCOM RL Tx.

A

70ft; strobe lights

85
Q

If lights-off does NOT occur within ___seconds after 10% RPM, the start should be aborted.

A

10

86
Q

Speed lever must be set to ___ for takeoff. Do not attempt to takeoff with speed lever in ___ position.

A

High; low

87
Q

Nose gear temp can be monitored on VIT ___. If steering becomes jammed at full lock, apply steering _____ the direction of turn.

A

VIT 8; opposite

88
Q

What EP checklist should you initiate if you experience degraded or frozen video and telemetry when low to the ground?

A

Total downlink failure below 2,000ft AGL or on ground

89
Q

Max gear in transit speed is:

A

135

90
Q

Crews may takeoff prior to a raised cable provided there is at least ___ft of runway or minimum required takeoff distance prior to raised cables.

A

5000

91
Q

When an alternate airfield is not an option, aircrews will comply with the following ceiling/visibility requirements: the worst weather must be at or below ceiling of ___or___ above the lowest compatible minima and a visibility of ___or___miles above lowest compatible minima.

A

800; 500
2; 1

92
Q

The shape of the GDT horn antenna (wide) allows the GDT to easily acquire the AC at approximately ___NM.

A

5.5

93
Q

What must be considered if landing with a flat main tire?

A

A & B

94
Q

(GEN2IR) An error exists within the scaling of the IR nose camera, resulting in HUD overlay and flight path marker (FPM) offsets. The HUD overlay graphics and FPM may be up to ___* off and may not reflect the actual AC attitude or aimpoint, which could result in steep/shallow approaches or nose-first landings.

A

2

95
Q

Set ___ for comm. delay RMIT

A

1.25sec

96
Q

Bingo fuel

A

600lbs

97
Q

Who is responsible for checking AC forms during changeout?

A

PIC

98
Q

Crew will preface laser call with:

A

Training

99
Q

Standard load-out A is:

A

2x R9E, 2x R2, 2x GBU12

100
Q

During losing Hand Over ops, crews will set the second waypoint of the ops mission to “lost link ok” with a ____ minute loiter.

A

30

101
Q

What’s the primary question aircrew should ask themselves regarding the law of war principle of proportionality?

A

Does the military advantage outweigh the anticipated collateral cost if this target is struck?