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1
Q

1(1). Once a “KNOCK IT OFF” is called, all participating aircraft will:
Ref: AFMAN 11-214 Chap: 3 Para: 3.4.2
A. Acknowledge with call sign in roll call fashion
B. Cease tactical maneuvering and end the scenario
C. Deconflict flight paths
D. All of the above

A

D. All of the above

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2
Q

3(3). Pilots will declare emergency fuel to the controlling agency as soon as it becomes apparent that an aircraft will enter initial or start an instrument final approach at the base of intended landing, or alternate if required, with ___ pounds of fuel (measured from the header tank) or less.
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.11.3
A. 200
B. 250
C. 300
D. 350

A

C. 300

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3
Q

2(2). Normal recovery fuel is the fuel on initial or at the FAF at the base of intended landing or alternate. Establish fuel quantity locally or ___ pounds (___ pounds for aircraft carrying 1 or more ER tank), whichever is higher.
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.11.1
A. 300; 400
B. 350; 450
C. 400; 500
D. 450; 550

A

C. 400; 500

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4
Q

4(4). Pilots will declare minimum fuel to the controlling agency as soon as it becomes apparent that an aircraft will enter initial or start an instrument approach at the base of intended landing, or alternate if required, with ___ pounds of fuel or less
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.11.2
A. 250
B. 300
C. 350
D. 500

A

C. 350

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5
Q

5(5). Once airborne if revised forecast steady state winds at ETA (±1 hour) exceed flight manual limits, the PIC will, if fuel state and/or mission parameters allow, adjust ETA to either _____ or ________.
Ref: AFMAN 11-2MQ9v3 Chap: 4 Para: 4.2.3.2.1
A. Overfly the forecast winds out of limits by at least one hour
B. Return with sufficient fuel to fly low approaches for a minimum of one hour (or as directed by local operating procedures)
C. terminate the mission to arrive at airfield of intended landing one hour before that forecast period
D. A or B
E. A and C

A

E. A and C

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6
Q

6(6). 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: AFMAN 11-2MQ9v3 Chap: 4 Para: 4.3.1
A. True
B. False

A

A. True

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7
Q

7(7). For air-to-air operations, a coordination brief between all involved players shall include the following:
Ref: AFMAN 11-2MQ9v3 Chap: 5 Para: 5.2
A. AFI 11-214 Air-to-Air Training Rules, operating area deconfliction, and FAA Special Request Approval
B. Emergency mission/lost link explanation, FAA special request approval, and operating area deconfliction.
C. Operating area deconfliction, emergency mission explanation and deconfliction, and AFI 11-214 Air-to-Air Training Rules.
D. None of the above

A

C. Operating area deconfliction, emergency mission explanation and deconfliction, and AFI 11-214 Air-to-Air Training Rules.

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8
Q

8(8). Aircrews will not takeoff if __________ turbulence is reported or forecast along the planned route of flight for clear air turbulence type III aircraft:
Ref: AFMAN 11-2MQ9v3 Chap: 4 Para: 4.2.2
A. light
B. severe
C. moderate
D. none of the above

A

B. severe

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9
Q

9(9). Abort the mission, regardless of apparent damage or subsequent normal operation, if any of the following occur:
Ref: AFMAN 11-2MQ9v3 Chap: 7 Para: 7.3.1
A. bird strike
B. over-G
C. flight control system anomalies (including uncommanded flight control inputs)
D. engine failure
E. All of the above

A

E. All of the above

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10
Q

10(10). The PIC is the final authority on the number of people allowed in the GCS (to include visitors) during operations.
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.1.1
A. True
B. False

A

A. True

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11
Q

11(11). Aircrew will perform operations check at least _____. These checks will include fuel level, oil level, electrical, datalink, engine parameters and emergency mission status at a minimum.
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.9.1.1
A. once every 30 minutes
B. once per hour
C. once every two hours
D. once per shift

A

B. once per hour

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12
Q

12(12). Change out one aircrew position at a time to ensure continuous monitoring of the aircraft. The ___ is the final authority in determining if circumstances are safe to replace aircrew positions.
Ref: AFMAN 11-2MQ9v3 Chap: 2 Para: 2.2.4.3
A. incoming PIC
B. outgoing PIC
C. both A and B
D. None of the above

A

A. incoming PIC

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13
Q

13(13). Aircrew will not place items (checklists, charts, etc.) behind the ___ at any time.
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.1.3
A. flap lever, condition lever, throttle, or speed lever
B. control stick
C. KVM switch
D. PSO

A

A. flap lever, condition lever, throttle, or speed lever

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14
Q

14(14). The fuel heater will automatically shed when aircraft voltage drops below ___ V.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.23.4
A. 23
B. 24
C. 25
D. 26

A

D. 26

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15
Q

15(15). If DEEC fails, the backup mode torque schedule limits engine power as a function of OAT and density altitude, and will not allow a command greater than ___% torque.
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.17
A. 28
B. 70
C. 78
D. 84
E. 96

A

B. 70

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16
Q

16(16). Use TERMINATE procedures when safety of flight is not a factor, and in the following cases:
Ref: AFMAN 11-214 Chap: 3 Para: 3.4.3.1
A. Below minimum altitude or minimum range, but when safety is not compromised
B. DLOs are met or are unattainable
C. Training Rules/other limits met
D. Exceeding area boundaries
E. All of the above

A

E. All of the above

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17
Q

17(17). Decreasing oil level may be an indication of an oil leak (external or internal), excessive oil consumption, or oil foaming. What are some important points to remember?
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.21 Warning & Caution
A. Minimize aircraft maneuvering and avoid excessive throttle movements.
B. Fluctuating oil pressure combined with fluctuating oil level may be an indication of a clogged oil vent line
C. Oil leaking inside the engine compartment can ignite and burn out of control resulting in the loss of the aircraft.
D. All of the above

A

D. All of the above

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18
Q

18(18). The Aircraft Component Currents Requirements chart shows typical continuous amperage for each device. However, momentary in-rush current can be up to ___ times as much when a unit is first turned on.
Ref: TO 1Q-9(M)A-1 Chap: 3
A. 1 or 2
B. 1 or 3
C. 2 or 3
D. 2 or 4

A

C. 2 or 3

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19
Q

19(19). During a forced landing (and operating on battery power), once the landing gear is lowered, battery life may preclude another full landing gear cycle prior to a successful touchdown.
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.52.8 Caution
A. True
B. False

A

A. True

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20
Q

20(20). Which of the following aircraft components draws the highest maximum amps?
Ref: TO 1Q-9(M)A-1 Chap: 3
A. MTS
B. Lynx SAR
C. Pitot heat
D. Ku-band datalink
E. Fuel heater

A

A. MTS

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21
Q

21(21). What is the maximum allowable EGT in flight?
Ref: TO 1Q-9(M)A-1 Chap: 5
A. 660 °C
B. 675 °C
C. 695 °C
D. 776 °C

A

B. 675 °C

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22
Q

22(22). Briefings and debriefings should take place in the following order of priority: Face to face, Telephonic/electronic, Airborne.
Ref: AFMAN 11-214 Chap: 3 Para: 3.3.1
A. True
B. False

A

A. True

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23
Q

23(23). ____ or lower should be used when penetrating areas of turbulence.
Ref: TO 1Q-9(M)A-1 Chap: 7 Para: 7.2.1
A. VA (maneuvering airspeed)
B. VT (threshold speed)
C. VNE (never exceed speed)
D. VS (stall speed)

A

A. VA (maneuvering airspeed)

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24
Q

24(24). Which item has the greatest drag index?
Ref: TO 1Q-9(M)A-1 Chap: 3
A. TAMLG landing gear extended
B. Propeller unfeathered (not rotating, worst case)
C. Empty M-299 half rack (2 rails)
D. GBU-12
E. GBU-38

A

B. Propeller unfeathered (not rotating, worst case)

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25
Q

25(25). In altitude preference mode, changes to the power setting affect aircraft airspeed, while aircraft pitch responds to achieve a command altitude. If the aircraft is unable to maintain the set speed and altitude, it will achieve the fastest possible airspeed, while
maintaining commanded altitude.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.11.2.
A. True
B. False

A

A. True

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26
Q

26(26). In speed preference mode, the aircraft adjusts pitch in an attempt to achieve the commanded airspeed and power settings are commanded to achieve the set altitude. If the aircraft is unable to maintain the set speed and altitude, it will depart from the set altitude in order to maintain speed.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.11.1
A. True
B. False

A

A. True

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27
Q

27(27). A _____ indicates operating procedures, techniques, etc., which could result in injury to personnel and/or loss of life if not carefully followed.
Ref: TO 1Q-9(M)A-1 Chap: Foreword Para: Warnings, Cautions, Notes
A. Warning
B. Caution
C. Advisory

A

A. Warning

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28
Q

28(28). ____ expresses a provision that is binding.
Ref: TO 1Q-9(M)A-1 Chap: Foreword Para: Shall, Will, Should, May
A. Shall
B. Should and May
C. Will

A

A. Shall

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29
Q

29(29). The EPO switch disconnects ____ from the GCS.
Ref: TO 1Q-9(M)A-1 Chap: 8 Para: 8.1.4.1.2
A. all AC power
B. all AC power and UPS output
C. UPS output
D. None of the above

A

A. all AC power

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30
Q

30(30). What does setting GCS Ignition to “Hot” do?
Ref: TO 1Q-9(M)A-1 Chap: 9 Para: 9.6.117
A. Enables the Engine Start Module (ESM)
B. Activates the EFIU
C. Activates the electric fuel pumps
D. A & C
E. All of the above

A

D. A & C

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31
Q

31(31). The EFIU monitors engine RPM received from the tach generator. If RPM drops below ____%, it automatically performs an in-flight restart.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.10.16
A. 28
B. 60
C. 78
D. 89.5
E. 92.5

A

C. 78

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32
Q

32(32). RPA crew will notify the controlling agency that they are “LOST LINK.”
Ref: AFMAN 11-214 Chap: 3 Para: 3.9.2.3
A. True
B. False

A

A. True

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33
Q

33(33). If both electric fuel pumps fail, _____.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.11.9 Warning
A. the engine will only continue to run until the fuel in the header tank is depleted
B. it is not possible to jettison fuel
C. the engine will immediately stop
D. A and B
E. All of the above

A

D. A and B

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34
Q

34(34). [Block 1] Batteries cannot be charged in flight. [Block 5] Supplied by either engine power or ground power, the aircraft electrical system has an on-board charging system for five batteries.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.12.1.5
A. True
B. False

A

A. True

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35
Q

35(35). The flaps are set automatically when airspeed exceeds ____KIAS or landing gear is up and ______.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.14.2.2
A. 134; airspeed hold is on
B. 110; cruise mode is on
C. 121; altitude hold is on
D. 100; the speed lever is full forward

A

A. 134; airspeed hold is on

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36
Q

36(36). Pilots must be alert to the possible consequences of deactivating SAS during flight. When SAS is deactivated, all ____ safety limitations are immediately turned off.
Ref: TO 1Q-9(M)A-1 Chap: 6 Para: 6.7.2 Caution
A. stall protect
B. cruise mode
C. autopilot
D. engine over speed protection

A

C. autopilot

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37
Q

37(37). With Cruise Mode ON, control sensitivity is reduced. Roll, pitch, and yaw gains are scaled with airspeed. Scaling limits roll to ____ up to ____ depending on airspeed.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.4
A. ±5°; ±40°
B. ±10°; ±40°
C. ±10°; ±60°
D. ±15°; ±60°

A

B. ±10°; ±40°

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38
Q

38(38). Cruise mode is on when any hold mode is engaged, when stall protect is enabled, or anytime airspeed is over ____.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.4
A. .7 coefficient of lift
B. .8 coefficient of lift
C. 100 KIAS
D. 110 KIAS
E. 120 KIAS

A

D. 110 KIAS

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39
Q

39(39). Do not zero trims or pitch trims in flight. Doing so will result in a 125-knot airspeed hold command if airspeed hold is engaged.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.8 Warning
A. True
B. False

A

A. True

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40
Q

40(40). The ____ feature is the first level of stall protection provided by the autopilot. It automatically decambers the ailerons when AOA increases above +5º to prevent wing tips from stalling.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.12
A. airspeed limit override
B. aileron tip stall override
C. stall protect
D. cruise mode

A

B. aileron tip stall override

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41
Q

41(41). Upon lost link while jettisoning fuel, both jettison valves will remain open.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.11.8.4
A. True
B. False

A

B. False

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42
Q

42(42). [2410] Stall protect is turned on and off by the pilot, but only takes effect at speeds below ____.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.13
A. .7 coefficient of lift
B. .8 coefficient of lift
C. 100 KIAS
D. 110 KIAS
E. 134 KIAS

A

E. 134 KIAS

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43
Q

43(43). [2410] While in the Inactive state, if AoA increases above 7 degrees it will enter the pushover state. In the pushover state, the aircraft reduces the pitch command until the
AoA decreases below 3 degrees and airspeed increases above Vmin at which point it will transition to the recovery state.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.13
A. True
B. False

A

A. True

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44
Q

44(44). Mission programming defaults to “fly-to” logic. For each mission leg during autonomous flight, the aircraft will use the programmed settings for the upcoming waypoint. Once the waypoint is passed, the settings for the next waypoint go into effect.
Ref: TO 1Q-9(M)A-1 Chap: 9 Para: 9.8.2 Note
A. True
B. False

A

A. True

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45
Q

45(45). Lost link programming and the emergency mission will not activate if “Lost Link - OK” is set ON during an operational mission.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.21 Caution
A. True
B. False

A

A. True

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46
Q

46(46). During a loss of command link, how much time passes until the RCM sends a reset command to the airborne modem?
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1-107
A. Arming time + 180 seconds
B. Arming time + 100 seconds
C. Arming time + 60 seconds
D. Arming time + 30 seconds
E. Arming time + 10 seconds

A

A. Arming time + 180 seconds

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47
Q

47(47). If EGI or FCA ____ fails, the Ku SATCOM will not be able to aim properly, which may cause the aircraft to lose Ku-band link and go lost link.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.17.1.3
A. 1
B. 2
C. 3
D. 4

A

A. 1

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48
Q

48(48). The transmission of the C-Band LOS datalink is referred to as the _____ and _____, while the Ku-Band SATCOM transmissions are called _____ and _____.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.19.1
A. uplink; downlink; command link; return link
B. command link; return link; uplink; downlink
C. transmit; receive; command link; return link
D. command link; return link; transmit; receive

A

A. uplink; downlink; command link; return link

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49
Q

49(49). The IR nose camera has its own heater and fan to prevent fogging.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.27.2
A. True
B. False

A

A. True

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50
Q

50(50). The ice detector signal stays on for _____ seconds after the ice has cleared.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.30
A. 30
B. 60
C. 45
D. 90

A

B. 60

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51
Q

51(51). The ____ mode (of the ARC-210) provides continuous scanning of four preset channels.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.32.3.1.8
A. manual
B. scan
C. preset
D. anti-jam

A

B. scan

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52
Q

52(52). A ____ background (on a VIT data element) indicates an abnormal condition. This generally indicates that the value is out of the normal operating parameters and should be monitored.
Ref: TO 1Q-9(M)A-1 Chap: 9 Para: 9.3.1
A. white
B. red
C. yellow
D. green

A

C. yellow

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53
Q

53(53). A ____ background (on the VIT data element) indicates a warning condition. This generally indicates the value is in a critical condition and will require corrective action.
Ref: TO 1Q-9(M)A-1 Chap: 9 Para: 9.3.1
A. green
B. yellow
C. red
D. both B and C

A

C. red

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54
Q

54(54). The deice system’s automatic mode is intended to be used when the aircraft is operating autonomously. If outside air temperature is less than ____, pitot heat is automatically turned on.
Ref: TO 1Q-9(M)A-1 Chap: 9 Para: 9.6.83
A. 0 °C
B. 15 °C
C. 10 °C
D. 21 °C

A

C. 10 °C

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55
Q

55(55). For an operational or emergency mission, when LOS TX #1 Inhibit is selected On, TX1 will be prevented from operating during that mission leg. What else is true about LOS TX Inhibit On?
Ref: TO 1Q-9(M)A-1 Chap: 9 Para: 9.162
A. This inhibit overrides any other programming and positively prevents the transmitter from operating under any circumstances
B. Transmitters will power up whenever triggered by later autonomous programming
C. Transmitters will power up whenever triggered by later autonomous programming inside of lights-on range
D. Transmitter frequencies will change to en route cruise settings

A

A. This inhibit overrides any other programming and positively prevents the transmitter from operating under any circumstances

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56
Q

56(56). In cruise mode, avoid flying the aircraft at AOA greater than ____ degrees. A high AOA can result in divergent roll oscillations.
Ref: TO 1Q-9(M)A-1 Chap: 2 Para: 2.31 Warning
A. +2.5
B. +5
C. +7.5
D. None of the above

A

B. +5

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57
Q

57(57). The engine may exceed maximum allowable EGT when disengaging Altitude Hold with the throttle in the ____ position with DEEC in Backup Mode.
Ref: TO 1Q-9(M)A-1 Chap: 2 Para: 2.31 Step 6 Caution
A. Full aft
B. Midrange
C. Full forward
D. Full reverse

A

C. Full forward

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58
Q

58(58). During an MCE gaining handover, the SATCOM command link is established when:
Ref: TO 1Q-9(M)A-1 Chap: 2 Para: 2.35 Step 24
A. I say it is
B. The “Ku SATCOM Command Link - lost” warning message disappears
C. System amps increase by approximately 10 amps
D. Uplink signal strength increases

A

B. The “Ku SATCOM Command Link - lost” warning message disappears

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59
Q

59(59). When flying without a lateral hold mode engaged, what is the maximum bank angle?
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.17
A. 30°
B. 5°
C. 0°
D. 40°

A

D. 40°

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60
Q

60(60). If executing a non-Push Button handover, it is necessary to update the datalink preset values found in Section 9; otherwise, the aircraft will retain the preset values for the losing GCS. Changing any of the preset
values in the HDD will result in all presets values being resent to the aircraft; however, entering an identical value in the HDD for a preset will not update any values.
Ref: TO 1Q-9(M)A-1 Chap: 2 Para: 2.35 Step 31 Caution
A. True
B. False

A

A. True

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61
Q

61(61). When executing a Push Button Handover, verify the ____ button is selected after handover data is verified.
Ref: TO 1Q-9(M)A-1 Chap: 2 Para: 2.35 Step 21
A. Apply
B. RL TX Enable
C. ARC-210 transmit
D. DVR Record

A

A. Apply

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62
Q

62(62). It is possible for the actual nose camera lens inside the fuselage to fog during descent. Fogging of the actual nose camera lens cannot be prevented with the use of nose lens heat. The Nose IR lens heater may be used to clear the nose EO camera.
Ref: TO 1Q-9(M)A-1 Chap: 2 Para: 2.42 Step 4 Caution
A. True
B. False

A

A. True

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63
Q

63(63). The UPS batteries will still be providing power if they were not turned off prior to evacuation.
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.63 Step 9 Note
A. True
B. False

A

A. True

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64
Q

64(64). With a left PSO rack (Pilot Station) failure or rack lock-up, the pilot has the option of sending the aircraft lost link prior to executing the PSO-1 Rack Lock-Up checklist.
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.66
A. True
B. False

A

A. True

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65
Q

65(65). Loss of control may be indicated by complete failure of the aircraft to respond to pilot control command. This may be caused by ____.
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.30
A. airspeed or pitot-static failure
B. catastrophic AOA failure below 134 KIAS with stall protect on, SAS failure
C. autopilot sensor failure, structural failure, or airframe icing
D. All of the above

A

D. All of the above

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66
Q

66(66). A stall condition may be indicated by _____.
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.37
A. warnings on the pilot HUD
B. excessively high AOA
C. unexpected loss of altitude
D. All of the above

A

D. All of the above

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67
Q

67(67). Pitot heat does not guarantee absence of ice from the pitot-static system. Moisture can freeze in the unheated areas of the system. This malfunction may be indicated by an FCA PPT sensor warning message, abnormal attitude, abnormal airspeed indications, or a combination of any of these. These conditions may result in ______.
Ref: TO 1Q-9(M)A-1 Chap: 7 Para: 7.3.5.1
A. aircraft pitch down or oscillation
B. loss of datalink
C. loss of aircraft control
D. All of the above

A

D. All of the above

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68
Q

68(68). Roll shaping limits the roll rate for pilot roll command inputs to reduce the possibility of lost link when rapid roll movements are used.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.15
A. True
B. False

A

A. True

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69
Q

69(69). Attempting to lower the gear with less than ____volts may cause a complete loss of battery power, leading to a possible loss of aircraft.
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.11 Step 6 Warning
A. 21
B. 24
C. 22
D. 28

A

C. 22

70
Q

70(70). Do not allow the engine to windmill between ___ and ___percent RPM. Operation within this range may cause engine damage.
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.11 Step 7 Caution
A. 18; 28
B. 10; 28
C. 60; 65
D. 50; 68

A

A. 18; 28

71
Q

71(71). The air start airspeed envelope is between ____ KIAS.
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.12
A. 100 and 160
B. 100 and 180
C. 150 and 200
D. None of the above

A

B. 100 and 180

72
Q

72(72). ___ of the external fuel tank fuel is unusable.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.11.8.1
A. 1%
B. 2%
C. 3%
D. 4%

A

C. 3%

73
Q

73(73). Maximum bank angle for autopilot controlled turns in emergency missions is limited to ____.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.17 Note
A. 20°
B. 14°
C. 30°
D. 15°

A

A. 20°

74
Q

74(74). The ATLC mission consists of ___ waypoints that define the runway and flight pattern around the airfield.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.18.2
A. 10
B. 7
C. 5
D. 15

A

A. 10

75
Q

75(75). The location of ___ is based off of a ___ glide slope and the height input for the waypoint.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1-132
A. WP5; 5°
B. WP3; 5°
C. WP4; 3°
D. WP6; 3°

A

C. WP4; 3°

76
Q

76(76). After takeoff with Auto Landing Gear selected, the landing gear is commanded up when aircraft is above ___ and VSI greater than ___ for 3 seconds.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.18.5
A. 800 ft AGL; 1200 ft/min
B. 400 ft AGL; 200 ft/min
C. 500 ft AGL; 300 ft/min
D. 600 ft AGL; 800 ft/min

A

B. 400 ft AGL; 200 ft/min

77
Q

77(77). Which two files are required for ATLC operation?
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.18.9
A. Profile file
B. Data file
C. Runway File
D. A and C

A

D. A and C

78
Q

78(78). Once the aircraft’s groundspeed is less than or equal to ___, ATLC logic will ramp the brakes to 100% over [2403] 2 seconds or [2410] 1 second.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.18.11
A. 20 knots
B. 50 knots
C. 85 knots
D. 75 knots

A

A. 20 knots

79
Q

79(79). Transition to ABORT state is not allowed once the aircraft exceeds rotation speed or the commit point, whichever comes first.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.18.12.5 Note
A. True
B. False

A

A. True

80
Q

80(80). If a takeoff abort has been triggered, ATLC will transition to this automated state and perform the following stopping procedure which includes the following commands:
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.18.12.9
A. Maintain flaps at takeoff flap setting of 15 degrees
B. Reverse thrust is used to assist in the stopping of the aircraft while ground speed is between 20 and 85 kts
C. Once the aircraft’s ground speed is less than or equal to 20 kts, ramp the brakes to 100% over 2 seconds
D. All of the above

A

D. All of the above

81
Q

81(81). Which condition is NOT required for ATLC to initialize the arming state?
Ref: TO 1Q-9(M)A-1 Chap: 1
A. Altitude=>300 ft above touchdown altitude
B. Crosswinds= within parameters
C. Airspeed=>50 KIAS
D. Baro-GPS Altitude difference=<300 ft

A

B. Crosswinds= within parameters

82
Q

82(82). To perform a PILOT ABORT - TAKEOFF prior to the aircraft’s rotation speed, what action does the Pilot need to take?
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.18.14.2.1
A. Reverse throttle
B. Command landing configuration on the control stick
C. Apply both brake pedals (>10%)
D. Press middle throttle button and pull control stick trigger

A

C. Apply both brake pedals (>10%)

83
Q

83(83). To perform a PILOT ABORT - LANDING, what action does the Pilot need to take?
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.18.4.2.2
A. Apply Brakes
B. HDD-ATLC Disable
C. Throttle forward
D. Pull back on control stick

A

D. Pull back on control stick

84
Q

84(84). The ____ is the point at which the stopping distance is greater than the distance to the rollout waypoint.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.18.15.1
A. Commit point
B. Abort point
C. Takeoff point
D. Landing point

A

A. Commit point

85
Q

85(85). For the ATLC lost link logic, the RCM will wait ____ to establish if it is a temporary or permanent dropout. If after ___, the link is still severed, the RCM will declare lost link.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.18.17
A. 5 seconds; 5 seconds
B. 3 seconds; 3 seconds
C. 2 seconds; 2 seconds
D. 4 seconds; 4 seconds

A

C. 2 seconds; 2 seconds

86
Q

86(86). The “LRD LP DES” MTS HUD indication will be displayed when the system measures the LRD energy output at approximately ___%, or less of normal operating power. It ____ recommended to use the LRD to designate for a laser-guided munition while under an LP condition.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1-277
A. 50; is
B. 60; is
C. 80; is not
D. 65; is not

A

D. 65; is not

87
Q

87(87). If a weapon being laser guided is in flight when the LRD LP DES occurs, do not stop lasing. The LRD may still be lasing at very low power. Any chance of guidance will help prevent collateral damage resulting from an unguided weapon. Continue normal lasing procedures until weapon impact.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1-277 Warning
A. True
B. False

A

A. True

88
Q

88(88). The LRD is PRF adjustable throughout the entire range of available PRF codes (____-____).
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.28.25.18
A. 0000; 1999
B. 1111; 1888
C. 1111; 1999
D. 0000; 1888

A

B. 1111; 1888

89
Q

89(89). What brevity would be used if flying in clouds or an area of reduced visibility?
Ref: AFTTP(I) 3-2.5, Brevity Pg: 32 Chap: Table 2
A. POPEYE
B. BLIND
C. NO JOY
D. SHREW

A

A. POPEYE

90
Q

90(90). Which launch mode results in a more vertical attack trajectory?
Ref: TO 1Q-9(M)A-34-1-1 Chap: 1 Para: 1.3.3.2.3
A. LOAL-D
B. LOAL-L
C. LOAL-H
D. LOBL

A

C. LOAL-H

91
Q

91(91). Which launch mode results in a more horizontal attack trajectory?
Ref: TO 1Q-9(M)A-34-1-1 Chap: 1 Para: 1.3.3.2.3
A. LOAL-D
B. LOAL-L
C. LOAL-H
D. LOBL

A

B. LOAL-L

92
Q

92(92). A ____ weapon icon (on the bottom of the HUD) indicates the weapon is selected for release.
Ref: TO 1Q-9(M)A-34-1-1 Chap: 1 Para: 1.4.13
A. green, solid
B. yellow, solid
C. red, outlined
D. green, outlined

A

A. green, solid

93
Q

93(93). The minimum ripple interval for Hellfire launches is ___ seconds for the same wing, and ___ for opposite-wing releases.
Ref: TO 1Q-9(M)A-34-1-1 Chap: 1
A. .64; .32
B. .32; .64
C. .3; .3
D. .2; .3

A

A. .64; .32

94
Q

94(94). What factor(s) are required for a commanded bomb to be released in CCRP mode?
Ref: TO 1Q-9(M)A-34-1-1 Chap: 1 Para: 1.7.3
A. RPA must be at or past the CCRP
B. RPA must be within 3,000 feet ground range of the CCRP
C. RPA course must be within 30º of the calculated run-in course (angle between aircraft course and target)
D. A & C
E. All of the above are required

A

E. All of the above are required

95
Q

95(95). The M310 launcher should not be exposed to temperatures below ____º Celsius.
Ref: TO 1Q-9(M)A-34-1-1 Chap: 1 Para: 1.7.7
A. -40
B. -45
C. -50
D. -55

A

A. -40

96
Q

96(96). AGM-114 missiles and M310 launchers cannot be jettisoned.
Ref: TO 1Q-9(M)A-34-1-1 Chap: 1 Para: 1.7.8 Note
A. True
B. False

A

A. True

97
Q

97(97). The ____ has an increased fragmentation warhead.
Ref: TO 1Q-9(M)A-34-1-1 Chap: 1 Para: 1.12.8.1
A. AGM-114/R-2
B. AGM-114/P
C. AGM-114/R-9E
D. AGM-114/M-6

A

C. AGM-114/R-9E

98
Q

98(98). For GBU-12s, squeeze the trigger at desired release point for ____ release mode, and prior to bomb release point for ____ deliveries.
Ref: TO 1Q-9(M)A-34-1-1 Chap: 2 Para: 2.7 Release Step 9 Note
A. manual; CCRP
B. ballistic; CCRP
C. manual; optimal
D. CCRP; manual

A

A. manual; CCRP

99
Q

99(99). “PRF Code Mismatch” with a yellow indicator will be present if the PRF code set on the weapon and aircraft LRD do not match. A PRF mismatch with a yellow marker will ____.
Ref: TO 1Q-9(M)A-34-1-1 Chap: 2 Para: 2.8 Missile Launch Procedures Step 33
A. prevent release
B. not prevent release
C. result in a misfire
D. result in a ballistic release

A

B. not prevent release

100
Q

100(100). Aircraft shall not be shut down until ____ has passed after last attempt to release forward-firing ordnance.
Ref: TO 1Q-9(M)A-34-1-1 Chap: 3 Para: 3.3 Step 2 Caution
A. 30 minutes
B. one hour
C. two hours
D. four hours

A

B. one hour

101
Q

101(101). Crews must positively identify the target prior to weapons release. For training sorties, crews will achieve positive identification either ____ or by confirming ____ through valid on-board/off-board cues.
Ref: AFMAN 11-2MQ9v3 Chap: 6 Para: 6.2
A. verbally; visually
B. verbally; accurate coordinates
C. visually; target location
D. visually; verbally

A

C. visually; target location

102
Q

102(102). Crews will perform a battle damage/weapons check of weapons stations prior to or during return to base (RTB). Additionally, crews will perform this check following _____.
Ref: AFMAN 11-2MQ9v3 Chap: 6 Para: 6.5
A. every ops check
B. expenditure of live ordnance
C. any altitude change
D. All of the above

A

B. expenditure of live ordnance

103
Q

103(103). When carrying releasable ordnance, remain two switch positions away from release at all times prior to intentionally releasing live or inert ordnance. The two deselected switches will be the master arm switch and the trigger.
Ref: AFMAN 11-2MQ9v3 Chap: 6 Para: 6.8.2
A. True
B. False

A

A. True

104
Q

104(104). Aircrew will conduct dry attacks with the cocked LEMA/closed hooks selected while releasable freefall munitions are on the aircraft. Aircrew will not select the live or inert GBU until ready to release the live or inert ordnance.
Ref: AFMAN 11-2MQ9v3 Chap: 6 Para: 6.7.3
A. True
B. False

A

A. True

105
Q

105(105). Aircrew will not activate the cocked LEMA/closed book station(s) (“fire”) or other training munitions until all live or inert ordnance has been visually confirmed released with the Multi-Spectral Targeting System.
Ref: AFMAN 11-2MQ9v3 Chap: 6 Para: 6.7.2
A. True
B. False

A

A. True

106
Q

106(106). For inadvertent release, accomplish the following:
Ref: AFMAN 11-2MQ9v3 Chap: 7 Para: 7.4.1
A. If able, record switch positions at the time of inadvertent release and provide to armament and safety personnel.
B. Safe all switches.
C. Record the impact point, if known.
D. If equipment failure is suspected, do not attempt further release in any mode.
E. All of the above

A

E. All of the above

107
Q

107(107). Type 3 Control - Once satisfied the attacking aircraft are correlated on the appropriate target(s), the JTAC/FAC(A) will provide attacking aircraft “CLEARED TO ENGAGE” or “Type 3, CONTINUE DRY”. The attack aircrew will report _______ to the JTAC/FAC(A).
Ref: JP 3-09.3 Close Air Support Pg: III-45 Chap: III-45
A. “Engagement Initiated”
B. “Inbound Attack”
C. “Commencing Engagement” and “Engagement Complete”
D. “Target Engaged”

A

C. “Commencing Engagement” and “Engagement Complete”

108
Q

108(108). What does DEADEYE mean?
Ref: AFTTP(I) 3-2.5, Brevity Pg: 13 Chap: Table 2
A. Acknowledges sighting of a specified reference point (either visually or via sensor)
B. Acquisition of laser designation
C. Laser designator system inoperative
D. Sighting of a friendly aircraft or ground position; opposite of BLIND

A

C. Laser designator system inoperative

109
Q

109(109). Leaving the AGM-114 missile powered on for extended durations may do what?
Ref: TO 1Q-9(M)A-34-1-1 Chap: 2 Para: AGM-114 Pre-Launch Caution
A. decrease reliability
B. cause a fire
C. decrease the maximum range
D. prevent propellant ignition

A

A. decrease reliability

110
Q

110(110). The WEZ displayed on the tracker is only representative of simulated missile capability, not operationally constrained parameters, and should not be used to determine the firing solution.
Ref: TO 1Q-9(M)A-34-1-1 Chap: 1 Para: 1.5.1
A. True
B. False

A

A. True

111
Q

111(111). Setting ripple release intervals greater than ___ may have an adverse effect on missile accuracy due to the plume from the first missile.
Ref: TO 1Q-9(M)A-34-1-1 Chap: 1 Para: 1.3.3.1.1.1 Caution
A. 0.1 sec
B. 0.32 sec
C. 1 sec
D. 4 sec

A

B. 0.32 sec

112
Q

112(112). ____ acknowledges sighing of a specified reference point (either visually or via sensor).
Ref: AFTTP(I) 3-2.5, Brevity Pg: 11 Chap: Table 2
A. TALLY
B. EYES ON
C. VISUAL
D. CONTACT

A

D. CONTACT

113
Q

113(113). ____ means the specified surface target or object has been acquired and is being tracked with an onboard sensor.
Ref: AFTTP(I) 3-2.5, Brevity Pg: 8 Chap: Table 2
A. ON COORDS
B. CAPTURE
C. THUNDER
D. CONTACT

A

B. CAPTURE

114
Q

114(114). ____ is the sighting of a target, non-friendly aircraft, or enemy position. Opposite of ____.
Ref: AFTTP(I) 3-2.5, Brevity Pg: 46 Chap: Table 2
A. VISUAL/BLIND
B. TALLY/NO JOY
C. CONTACT/COORDS
D. CAPTURE/CONTACT

A

B. TALLY/NO JOY

115
Q

115(115). For a LoaL-H engagement the missile attempts to maximize impact angle in an attempt to achieve a hard coded impact angle of ___?
Ref: AFTTP 3.3.MQ-9 Chap: 6 Para: 6.2.2
A. 75 °
B. 84 °
C. 69 °
D. 60 °

A

B. 84 °

116
Q

116(116). What type of holding game plan should be used to keep the aircraft at a constant bearing to the target and oriented either on-axis with the run-in, or off-axis from the run-in?
Ref: AFTTP 3.3.MQ-9 Chap: 7 Para: 7.3.1.2.5.3
A. Wheel
B. Figure Eight
C. Modified Figure Eight
D. Racetrack

A

D. Racetrack

117
Q

117(117). When briefing the “Clearance” portion in WTARSEC, this includes which of the following:
Ref: AFTTP 3.3.MQ-9 Chap: 7
A. When it is expected
B. Clearance authority
C. Type of Clearance
D. All of the above

A

D. All of the above

118
Q

118(118). During a Straight-Through Egress maneuver, the pilot should use bank _____and_______ to cross-control the aircraft to fly straight over the target and slow the rate of rotation in the TGP.
Ref: AFTTP 3.3.MQ-9 Chap: 7 Para: 7.3.2.1.3.3
A. Angle; roll
B. Angle; rudder
C. Pitch; angle
D. Rudder; angle

A

B. Angle; rudder

119
Q

119(119). Maximum maneuvering category for RPAs is UNLIMITED as long as they remain within assigned altitude blocks.
Ref: AFMAN 11-214 Chap: 4 Para: 4.8.2
A. True
B. False

A

A. True

120
Q

120(120). All passed restrictions ____ be read back.
Ref: JP 3-09.3 Close Air Support Chap: V-32
A. Will
B. Shall
C. Should
D. Might

A

B. Shall

121
Q

121(121). Which of the following manners can a JTAC/FAC(A) use to provide target location during the CAS Brief (9-line)?
Ref: JP 3-09.3 Close Air Support Chap: V-25-26
A. Latitude/Longitude
B. Grid Coordinates
C. Offset from known point
D. A, B and C
E. A and B only

A

D. A, B and C

122
Q

122(122). Friendly grids should not be passed if it can be avoided. If necessary, use no more than ___ digits.
Ref: JP 3-09.3 Close Air Support Chap: v-20
A. 4
B. 6
C. 8
D. 10

A

B. 6

123
Q

123(123). Danger close, Final Attack Headings, and TOTs are all examples of what during the CAS Brief (9-line)?
Ref: JP 3-09.3 Close Air Support Chap: V-30-31
A. Remarks
B. Restrictions
C. Friendly Position
D. Gameplan

A

B. Restrictions

124
Q

124(124). Maintain safe taxi speeds at all times, not to exceed ___ knots ground speed (KGS) on a taxiway,__ KGS on a runway, and less than __ KGS in a turn greater than 30 degrees.
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.6.2.5
A. 10; 20; 6
B. 10; 15; 6
C. 20; 15; 10
D. 25; 15; 10

A

A. 10; 20; 6

125
Q

125(125). Minimum runway length for Reaper operations is feet.
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.7.1
A. 3,000
B. 5,000
C. 4,000
D. 7,000

A

B. 5,000

126
Q

126(126). Minimum runway width for MQ-9 operations is ___ ft while minimum taxiway width is ___ ft.
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.7.2 - 3.7.3
A. 50; 50
B. 50; 75
C. 75; 75
D. 75; 50

A

D. 75; 50

127
Q

127(127). Crews may takeoff prior to a raised cable provided there is at least ___ ft of runway or minimum required takeoff distance (whichever is greater) prior to the raised cables.
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.8.4
A. 3,000
B. 1,000
C. 7,000
D. 5,000

A

D. 5,000

128
Q

128(128). Pilots will establish a normal glide path by ___ feet AGL. Descent rates greater than____ feet per minute (FPM) below 200 feet AGL, greater than ___ FPM below 50 feet AGL, airspeed more than __ KIAS below calculated approach speed, or a pilot-induced oscillation (PIO)/bounce require a go-around.
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.10.2.2
A. 1,500; 1,200; 600; 4
B. 200; 1,200; 800; 5
C. 500; 600; 200; 6
D. 600; 480; 200; 5

A

B. 200; 1,200; 800; 5

129
Q

129(129). Minimum approach airspeed during an SFO traffic pattern is stall speed plus ___ KIAS.
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.12.3.1
A. 10
B. 15
C. 20
D. 25

A

B. 15

130
Q

130(130). [Manual Landings] When an alternate airfield is not an option or not available, aircrews will comply with the following ceiling and visibility requirements: the worst weather (TEMPO or prevailing) must be at or above a ceiling of ___ or ___ above the lowest compatible minima (whichever is greater), and a visibility of ____ miles or ___ mile(s) above the lowest compatible minima.
Ref: AFMAN 11-2MQ9v3 Chap: 4 Para: 4.2.1.2.1
A. 1,500; 1,000; 3; 2
B. 800; 500; 3; 2
C. 800; 500; 2; 1
D. 1,500; 1,000; 3; 1

A

C. 800; 500; 2; 1

131
Q

131(131). When actual or forecasted ceiling is below _____ feet and/or the visibility is less than ___SM, aircrew members will increase recovery fuel to allow holding for____ hours over the destination at maximum endurance, at expected holding altitude, at calculated destination gross weight, and engine speed set to minimum, then expect to penetrate and land with normal recovery fuel.
Ref: AFMAN 11-2MQ9v3 Chap: 4 Para: 4.2.1.2.3
A. 3,000; 3; 2
B. 3,000; 3; 4
C. 1,500; 3; 2
D. 1,500; 3; 4

A

A. 3,000; 3; 2

132
Q

132(132). Once airborne, if destination forecasts change and the aircrew is unable to adjust landing time (early or late) to meet requirements in paragraph 4.2.1.2.1, aircrew will increase recovery fuel to allow _____ hours of holding over the destination at maximum endurance speed, at expected holding altitude, at calculated
destination gross weight, and engine speed set to minimum, then expect to penetrate and land with normal recovery fuel.
Ref: AFMAN 11-2MQ9v3 Chap: 4 Para: 4.2.1.2.2
A. 1
B. 2
C. 4
D. 8

A

C. 4

133
Q

133(133). If revised forecast steady state winds at ETA (±1 hour) exceed flight manual limits, the PIC will, if fuel state and/or mission parameters allow, adjust ETA to either:
Ref: AFMAN 11-2MQ9v3 Chap: 4 Para: 4.2.3.2.1
A. overfly the forecast winds out of limits period by at least one hour
B. terminate the mission to arrive at airfield of intended landing one hour before that forecast period
C. with sufficient fuel to fly low approaches for a minimum of four hours (or as directed by Local Operating Procedures) unless a suitable alternate is available
D. A or B
E. A or C

A

D. A or B

134
Q

134(134). Whenever the outside air temperature is less than ___ degrees Fahrenheit, or the pilot is concerned about frost, ice, or snow, apply an ice retardant to the wings or inspect the aircraft for frost immediately prior to takeoff.
Ref: AFMAN 11-2MQ9v3 Chap: 4 Para: 4.3.1
A. 60
B. 50
C. 40
D. 30

A

C. 40

135
Q

135(135). Do not takeoff or land with an RCR less than ___.
Ref: AFMAN 11-2MQ9v3 Chap: 4 Para: 4.4.1
A. 5
B. 7
C. 10
D. 12

A

D. 12

136
Q

136(136). Handling characteristics of the MQ-9 on ice or snow are not optimum. On ice and/or snow, minimize throttle setting to that required to move (or sustain movement of) the aircraft and limit taxi speed to no more than ___ KGS.
Ref: AFMAN 11-2MQ9v3 Chap: 4 Para: 4.4.2
A. 4
B. 7
C. 9
D. 12

A

A. 4

137
Q

137(137). Pilots will not taxi with nose-wheel steering, brake system, video path, or telemetry/datalink malfunctions.
Ref: AFMAN 11-2MQ9v3 Chap: 7 Para: 7.2.1
A. True
B. False

A

A. True

138
Q

138(138). If encountering a landing gear malfunction and the gear are down, leave them down and do not make touch-and-go landings.
Ref: AFMAN 11-2MQ9v3 Chap: 7 Para: 7.3.2
A. True
B. False

A

A. True

139
Q

139(139). Unless otherwise briefed, SOs will announce altitude deviations exceeding ±____ feet at the Initial Approach Fix (IAF), Final Approach Fix (FAF), and Minimum Descent Altitude (MDA), as well as when reaching Decision Height (DH) or the Missed Approach Point (MAP).
Ref: AFMAN 11-2MQ9v3 Chap: 3 Para: 3.10.2.3
A. 1,000
B. 500
C. 200
D. 100

A

D. 100

140
Q

140(140). Ground lost link is declared when the following condition(s) is/are true at the time of lost link:
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.23.2
A. Airspeed is less than 50 KIAS
B. Landing gear is commanded down
C. Ground speed is less than 50 knots
D. All of the above

A

D. All of the above

141
Q

141(141). Selected warning messages related to the navigation system may appear when the aircraft is first powered up. They should disappear after about _____ minutes.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.17.4
A. 2
B. 3
C. 5
D. 7

A

C. 5

142
Q

142(142). During AV Preflight, many navigation health and 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. Do not move the aircraft until the appropriate codes are presented.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.17.5
A. 5 or greater; zero; 1-2
B. auto; 0000; 10+
C. F7; 20; 7-9
D. 8880; absent; 5

A

C. F7; 20; 7-9

143
Q

143(143). GDT transmitter low power _____ .
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.22.4
A. is intended for maintenance purposes
B. can be used for taxi in some circumstances
C. is not intended for flight operation
D. All of the above

A

D. All of the above

144
Q

144(144). The shape of the GDT horn antenna (wide) allows the GDT to easily acquire the aircraft at approximately____ NM.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.22.3.2
A. 5
B. 5.5
C. 6.5
D. 70

A

B. 5.5

145
Q

145(145). Extended use of nose lens heat at ___% or higher on the ground will cause the lens to crack.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.27.1.1 Caution
A. 30
B. 60
C. 80
D. 100

A

B. 60

146
Q

146(146). Before starting the C-band link test, verify signal strengths are at least __ %.
Ref: TO 1Q-9(M)A-1 Chap: 2 Para: 2.19
A. 40
B. 50
C. 70
D. 80

A

B. 50

147
Q

147(147). Ground personnel can enter the __-foot hazard boundary if there is an active RL and the SATCOM Antenna look angle is greater than __ degrees. Recommended answers.
Ref: TO 1Q-9(M)A-1 Chap: 2 Para: 2.33
A. 1; 5
B. 72; 10
C. 100; 50
D. 82; 30

A

B. 72; 10

148
Q

148(148). If light-off does not occur within ___ seconds after 10% RPM, the start should be aborted.
Ref: TO 1Q-9(M)A-1 Chap: 2 Para: 2.20
A. 10
B. 15
C. 25
D. 60

A

A. 10

149
Q

149(149). Do not operate C-band directional transmitters on high power if ground personnel are within ____ feet of the antenna.
Ref: TO 1Q-9(M)A-1 Chap: 2
A. 3
B. 10
C. 20
D. 100

A

A. 3

150
Q

150(150). Confirm aircraft magnetic heading is within __º of exact runway heading when aircraft is aligned on runway centerline.
Ref: TO 1Q-9(M)A-1 Chap: 2 Para: 2.29 Step 7 Note
A. ±1
B. ±3
C. ±5
D. ±7

A

C. ±5

151
Q

151(151). A visual check of the main wheel tires, brake assemblies, and nosewheel steering should be accomplished before landing. Also, confirm ____ indication is not present within the gear indicator on the pilot HUD.
Ref: TO 1Q-9(M)A-1 Chap: 2 Para: 2.50
A. “G”
B. “D”
C. “B”
D. “E”

A

C. “B”

152
Q

152(152). Flaps are controlled manually until airspeed exceeds ___ KIAS.
Ref: TO 1Q-9(M)A-1 Chap: 6 Para: 1.14.2.1
A. .7 coefficient of lift
B. 110 KIAS
C. 100 KIAS
D. 134 KTAS
E. 134 KIAS

A

E. 134 KIAS

153
Q

153(153). During an abort, if it becomes apparent that the aircraft will depart the prepared surface
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.6
A. Condition lever - AFT
B. SAS - OFF
C. Payload - STOW
D. GDT - OFF

A

A. Condition lever - AFT

154
Q

154(154). During a GDT switch, if GDT power is switched off before the GDT uplink Tx is turned off, it is not possible to regain link with the second GDT as the Tx on the first GDT remains on.
Ref: Chap: 3 Para: 3.58 Caution
A. True
B. False

A

A. True

155
Q

155(155). What must be considered if landing with a flat main tire?
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.48
A. Land on the side of the runway corresponding to the good main tire
B. Land with any crosswind on the side of the aircraft with the good main tire
C. A & B
D. None of the above

A

C. A & B

156
Q

156(156). Maximum gear in transit speed is ____KIAS.
Ref: TO 1Q-9(M)A-1 Chap: 5 Para: Figure 5-6
A. 135
B. 158
C. 160
D. 230

A

A. 135

157
Q

157(157). The maximum crosswind component for takeoff and landing is __ knots. With symmetric or asymmetric loads the crosswind limit is __ knots.
Ref: TO 1Q-9(M)A-1 Chap: 5 Para: 5.12
A. 5; 10
B. 10; 13
C. 20; 15
D. 13; 15

A

C. 20; 15

158
Q

158(158). When conditions of snow or ice exist, the ______ are usually more slippery than any other areas due to the melting and freezing of ice and snow at this location.
Ref: TO 1Q-9(M)A-1 Chap: 7 Para: 7.3.3
A. painted areas on the aircraft
B. approach ends of the runway
C. A & B
D. None of the above

A

B. approach ends of the runway

159
Q

159(159). In extreme hot weather conditions, above °F, malfunction or damage to avionics and electrical systems may occur due to overheating.
Ref: TO 1Q-9(M)A-1 Chap: 7 Para: 7.4
A. 100
B. 120
C. 70
D. 80

A

A. 100

160
Q

160(160). To lessen the possibility of entering a hydroplaning skid:
Ref: TO 1Q-9(M)A-1 Chap: 7 Para: 7.3.6.4
A. Use moderate touchdown speeds and a soft landing to minimize exposure time hydroplaning
B. Do not apply brakes until after wheels spin up and directional control has been firmly established
C. Land slightly off centerline to absorb the most water on contact
D. All of the above

A

B. Do not apply brakes until after wheels spin up and directional control has been firmly established

161
Q

161(161). Firefighting withdrawal distance for nonessential personnel is ____ if a burning aircraft is armed with GBU-12s or AGM114s.
Ref: TO 1Q-9(M)A-1 Chap: 3 Para: 3.10
A. 300 feet
B. 3,000 feet
C. 4,000 feet
D. 5,000 feet

A

C. 4,000 feet

162
Q

162(162). Crews will ensure takeoff weather and forecasted landing weather +/- 1 hour (excluding temporary [TEMPO] groups) must be at, or greater than 800 feet and 2 SM, or 500 feet and 1 SM greater than the lowest compatible approach minimum (whichever is greater).
Ref: AFMAN 11-2MQ9v3 Para: 4.2.1.2.1
A. True
B. False

A

A. True

163
Q

163(163). ________ are responsible for submitting divert locations to MAJCOMs for approval as alternates, per AFMAN 11-202.
Ref: AFMAN 11-2MQ9v3 Para: A.6.7.2
A. OG/CC’s
B. SQ/CC’s
C. MAJCOM/CC’s
D. WG/CC’s

A

A. OG/CC’s

164
Q

164(164). OG/CCs may authorize operations within ___NM of thunderstorms when necessary to meet operational requirements. Aircrew will maintain TO directed ___NM distance unless specifically approved otherwise.
Ref: AFMAN 11-2MQ9v3 Chap: 4 Para: 4.3.3
A. 20 NM
B. 25 NM
C. 30 NM
D. 35 NM

A

B. 25 NM

165
Q

165(165). [2410] While using the endurance airspeed function of airspeed hold may lead to high AOA conditions(greater than 7 degrees) within 4-6 seconds. High AoA results from either inadequate power.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.25.15
A. True
B. False

A

A. True

166
Q

166(166). [2410] If the aircraft is in taxi path mode, lost link logic waits ______ before shutting down the engine. However, if the aircraft is traveling faster than _____, the engine is shut down immediately.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.23.3
A. 2 seconds; 10 KGS
B. 7 seconds; 25 KGS
C. 5 seconds; 15 KGS
D. 15 seconds; 25 KGS

A

D. 15 seconds; 25 KGS

167
Q

167(167). The launch enable button on the throttle is used to switch between taxi hold modes. Pressing the launch enable button while in taxi Heading hold will command taxi path hold and pressing the launch enable button while in taxi path hold will command taxi heading hold.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.25.6
A. True
B. False

A

A. True

168
Q

168(168). [2410] Bring the aircraft to a complete stop before performing a pilot takeover. Commanding a pilot takeover disables throttle position scaling for taxi. Disabling throttle position scaling sends true throttle position information to the aircraft resulting in an unintentional increase of taxi speed if the throttle is not set to ground idle. An unintended increase of taxi speed may cause the aircraft to depart the prepared surface.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.25.7 Caution
A. True
B. False

A

A. True

169
Q

169(169). Pilots will not disengage ATLC after beginning an IMC takeoff or approach, except for safety of flight or ATC direction.
Ref: AFMAN 11-2MQ9v3 Para: A6.6.2
A. True
B. False

A

A. True

170
Q

170(170). [2410] Do not enable taxi path mode until ready to taxi aircraft. Enabling taxi path mode and remaining stationary puts stress on the nosewheel steering servo causing it to overheat. Aircrew should begin taxiing within __ minutes of enabling taxi path mode to prevent overheating the nosewheel steering servo.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.15.1 Caution
A. 2
B. 4
C. 3
D. 5

A

B. 4

171
Q

171(171). [2410] 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 2 degrees off and may not reflect the actual aircraft attitude or aimpoint.
Ref: TO 1Q-9(M)A-1 Chap: 1 Para: 1.27.2 Warning
A. True
B. False

A

A. True

CB MQF (3 decks)

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