1.
1. Once a "KNOCK IT OFF" is called, all participating aircraft will:
Ref: AFI 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. 
D. 
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 pound, whichever is higher.
Ref: AFI 11-2MQ-1&9V3 Chap: 3 Para: 3.11.1
A. 
B. 
C. 
D. 
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 or less.
Ref: AFI 11-2MQ-1&9V3 Chap: 3 Para: 3.11.3
A. 
B. 
C. 
D. 
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: AFI 11-2MQ-1&9V3 Chap: 3 Para: 3.11.2
A. 
B. 
C. 
D. 
5.
5. While airborne, if revised forecast winds for ETA (±1 hour) exceed limits specified in the flight manual, the pilot will terminate the
mission in time to return to the operating base _________ unless a suitable alternate is available.
Ref: AFI 11-2MQ-1&9V3 Chap: 4 Para: 4.2.3.2
A. 
Before the forecast time of increased winds
B. 
With sufficient fuel to fly low approaches for a minimum of one hour (or as directed by local operating procedures)
C. 
With sufficient fuel to fly low approaches for a minimum of two hours (or as directed by local operating procedures)
D. 
E. 
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. If precipitation cannot be avoided, pilots should maximize climb or descent rate to
exit potential or actual icing conditions.
Ref: AFI 11-2MQ-1&9V3 Chap: 4 Para: 4.3.2
7.
7. For Air-To-Air Operations, a coordination brief between all involved players shall include the following:
Ref: AFI 11-2MQ-1&9V3 Chap: 5 Para: 5.2
A. 
AFI 11-214 Air-To-Air Training Rules, altitude deconfliction, and FAA Special Request Approval
B. 
Emergency mission/lost link explanation, FAA special request approval, and altitude deconfliction.
C. 
Altitude deconfliction, emergency mission/lost link explanation and deconfliction, and AFI 11-214 Air-To-Air
Training Rules
D. 
8.
8. Aircrews will not takeoff if forecast or reported _________ turbulence for Light/Category I aircraft is present along the route of flight.
Ref: AFI 11-2MQ-1&9V3 Chap: 4 Para: 4.2.2.1
A. 
B. 
C. 
D. 
9.
9. Abort the mission, regardless of apparent damage or subsequent normal operation, if any of the following occur:
Ref: AFI 11-2MQ-1&9V3 Chap: 7 Para: 7.3.1
A. 
B. 
C. 
Flight control system anomalies (including uncommanded flight control inputs)
D. 
E. 
10.
10. The PIC is the final authority on the number of people allowed in the GCS (to include visitors) during operations.
Ref: AFI 11-2MQ-1&9V3 Chap: 3 Para: 3.1.1
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: AFI 11-2MQ-1&9V3 Chap: 3 Para: 3.9.2.1
A. 
B. 
C. 
D. 
12.
12. Change out one crewmember at a time to ensure continuous monitoring of the aircraft. The _ is the final authority in
determining if circumstances are safe to replace crews.
Ref: AFI 11-2MQ-1&9V3 Chap: 3 Para: 2.3.4.3
A. 
B. 
C. 
D. 
13.
13. Aircrew will not place items (checklists, charts, etc.) behind the _______ at any time.
Ref: AFI 11-2MQ-1&9V3 Chap: 3 Para: 3.1.3
A. 
Flap lever, condition lever, throttle, or speed lever
B. 
C. 
D. 
14.
14. Due to the lack of visible light, the DTV video will be degraded until approximately 1 hour after sunrise and approximately 1 hour
prior to sunset.
Ref: AFTTP 3-3.MQ-9 Chap: 6 Para: 6.2.2.1.3
15.
15. The fuel heater will automatically shed when aircraft voltage drops below ________ V.
Ref: T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.12.8.1 Note
A. 
B. 
C. 
D. 
16.
16. 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: T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.17
A. 
B. 
C. 
D. 
E. 
17.
17. If the selected tank’s solenoid on the fuel feed manifold fails closed, the header tank level and pressure will decrease.
Ref: T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.29 Note
18.
18. 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: T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.21 Caution
A. 
Minimize 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 loss of aircraft
D. 
19.
19. The Aircraft Component Currents Requirements chart shows typical amperage for each device. However, momentary in-rush
current can be up to _________ times as much when a unit is first turned on.
Ref: T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.56.2 Caution
A. 
B. 
C. 
D. 
20.
20. 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: T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.56.4 Caution
21.
21. Which of the following aircraft component draws the highest maximum amps?
Ref: T.O. 1Q-9(M)A-1 Chap: 3 Para: Figure 3-17
A. 
B. 
C. 
D. 
E. 
22.
22. A warning of “Aileron servo Left (or Right) - temp in the caution range” indicates aileron servo temperature is below -45º C or
above ________°C.
Ref: T.O. 1Q-9(M)A-1 Chap: 3 Para: Figure 3-19
A. 
B. 
C. 
D. 
23.
23. What is the maximum allowable EGT in flight?
Ref: T.O. 1Q-9(M)A-1 Chap: 5 Para: Figure 5-1
A. 
B. 
C. 
D. 
24.
24. Forward CG imbalance, even at the most extreme, should not present a flight control problem.
Ref: T.O. 1Q-9(M)A-1 Chap: 6 Para: 6.12
25.
25. _________ or lower should be used when penetrating areas of turbulence.
Ref: T.O. 1Q-9(M)A-1 Chap: 7 Para: 7.2.1
A. 
VA (maneuvering airspeed)
B. 
C. 
D.