Mq-9 Pilot Mqf 6 Sq Feb 2016

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  • 1/92 Questions

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

    • Acknowledge with call sign in roll call fashion
    • Cease tactical maneuvering and end the scenario
    • Deconflict flight paths
    • All of the above
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Mq-9 Pilot Mqf 6 Sq Feb 2016 - Quiz
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  • 2. 

    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

    • True

    • False

    Correct Answer
    A. True
    Explanation
    Precipitation, such as rain or snow, can have a negative impact on aircraft performance and visibility. Therefore, pilots should try to minimize their exposure to precipitation during all stages of the flight. If it is not possible to avoid precipitation, pilots should aim to climb or descend at the maximum rate possible in order to exit potential or actual icing conditions. This will help to maintain the safety and efficiency of the aircraft during flight.

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  • 3. 

    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

    • Light

    • Severe

    • Moderate

    • None of the above

    Correct Answer
    A. Severe
    Explanation
    Aircrews will not takeoff if forecast or reported severe turbulence for Light/Category I aircraft is present along the route of flight.

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  • 4. 

    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

    • Bird strike

    • Over-G

    • Flight control system anomalies (including uncommanded flight control inputs)

    • Engine failure

    • All of the above

    Correct Answer
    A. All of the above
    Explanation
    If any of the listed events occur during a mission, it is necessary to abort the mission. This includes a bird strike, over-G force, flight control system anomalies (such as uncommanded flight control inputs), or engine failure. Regardless of the apparent damage or subsequent normal operation, any of these events pose a significant risk and require the mission to be aborted.

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  • 5. 

    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

    • True

    • False

    Correct Answer
    A. True
    Explanation
    According to AFI 11-2MQ-1&9V3, the PIC (Pilot in Command) has the ultimate authority to determine the number of people allowed in the GCS (Ground Control Station) during operations, including visitors. Therefore, the statement is true.

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  • 6. 

    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

    • Once every 30 minutes

    • Once per hour

    • Once every two hours

    • Once per shift

    Correct Answer
    A. Once per hour
    Explanation
    Aircrew will perform operations checks at least once per hour. This includes checking the fuel level, oil level, electrical systems, datalink, engine parameters, and emergency mission status. This frequency ensures that all necessary systems are functioning properly and any potential issues can be identified and addressed in a timely manner.

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  • 7. 

    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

    • Incoming PIC

    • Outgoing PIC

    • Both A and B

    • None of the above

    Correct Answer
    A. Incoming PIC
    Explanation
    The correct answer is "incoming PIC". According to the given reference, the incoming Pilot in Command (PIC) is the final authority in determining if circumstances are safe to replace crews. This means that it is the responsibility of the incoming PIC to assess the situation and make the decision on whether it is safe to change out one crewmember at a time while ensuring continuous monitoring of the aircraft.

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  • 8. 

    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

    • True

    • False

    Correct Answer
    A. True
    Explanation
    The DTV video will be degraded during the periods of approximately 1 hour after sunrise and 1 hour prior to sunset due to the lack of visible light. This means that the video quality will be lower during these times compared to other times of the day when there is sufficient visible light. The reference provided confirms this information.

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  • 9. 

    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

    • 23

    • 24

    • 25

    • 26

    Correct Answer
    A. 26
  • 10. 

    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

    • True

    • False

    Correct Answer
    A. True
    Explanation
    If the selected tank's solenoid on the fuel feed manifold fails closed, it means that the solenoid valve is stuck in the closed position and is not allowing fuel to flow into the header tank. As a result, the fuel level and pressure in the header tank will decrease because no fuel is being supplied to it.

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  • 11. 

    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

    • Minimize maneuvering and avoid excessive throttle movements

    • Fluctuating oil pressure combined with fluctuating oil level may be an indication of a clogged oil vent line

    • Oil leaking inside the engine compartment can ignite and burn out of control resulting in loss of aircraft

    • All of the above

    Correct Answer
    A. All of the above
    Explanation
    The given correct answer is "All of the above". This means that all the points mentioned in the options are important to remember when dealing with a decreasing oil level. Minimizing maneuvering and avoiding excessive throttle movements is important to prevent further damage or loss of oil. Fluctuating oil pressure combined with fluctuating oil level may indicate a clogged oil vent line, which needs to be addressed. Additionally, oil leaking inside the engine compartment can be dangerous as it can ignite and result in the loss of the aircraft. Therefore, all the mentioned points are important considerations when faced with a decreasing oil level.

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  • 12. 

    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

    • 1-2

    • 1-3

    • 2-3

    • 2-4

    Correct Answer
    A. 2-3
    Explanation
    The Aircraft Component Currents Requirements chart provides typical amperage values for each device, but when a unit is first turned on, there can be a momentary in-rush current that is up to 2-3 times higher than the typical amperage. This means that when a device is initially powered on, it may draw a significantly higher amount of current than what is typically required for normal operation. This information is important to consider when designing electrical systems and selecting appropriate circuit protection devices to handle these momentary high currents.

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  • 13. 

    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

    • True

    • False

    Correct Answer
    A. True
    Explanation
    During a forced landing, the aircraft may be operating on battery power. Once the landing gear is lowered, it uses up battery life. If the battery life is not sufficient, there may not be enough power left for another full landing gear cycle before successfully touching down. Therefore, the statement is true.

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  • 14. 

    23. What is the maximum allowable EGT in flight? Ref: T.O. 1Q-9(M)A-1 Chap: 5 Para: Figure 5-1

    • 660° C

    • 675° C

    • 695° C

    • 776° C

    Correct Answer
    A. 675° C
    Explanation
    The maximum allowable EGT in flight is 675°C. This information can be found in T.O. 1Q-9(M)A-1, Chapter 5, Figure 5-1.

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  • 15. 

    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

    • True

    • False

    Correct Answer
    A. True
    Explanation
    According to T.O. 1Q-9(M)A-1, Chapter 6, Paragraph 6.12, even if the forward center of gravity (CG) imbalance is at its most extreme, it should not cause any flight control problems.

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  • 16. 

    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

    • VA (maneuvering airspeed)

    • VT (threshold speed)

    • VNE (never exceed speed)

    • VS (stall speed)

    Correct Answer
    A. VA (maneuvering airspeed)
    Explanation
    According to T.O. 1Q-9(M)A-1, Chapter 7, Paragraph 7.2.1, when penetrating areas of turbulence, the maneuvering airspeed (VA) or lower should be used. This is because maneuvering airspeed is the maximum speed at which abrupt control inputs can be made without exceeding the aircraft's structural limits. Using a lower airspeed helps to ensure the safety and stability of the aircraft in turbulent conditions.

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  • 17. 

    26. Which item has the greatest drag configuration index? Ref: T.O. 1Q-9(M)A-1 Chap: 3 Figure 3-16

    • TAMLG landing gear extended

    • Propeller unfeathered (not rotating, worst case)

    • Empty M-299 half rack (2 rails)

    • GBU-12

    • GBU-38

    Correct Answer
    A. Propeller unfeathered (not rotating, worst case)
    Explanation
    The drag configuration index refers to the amount of drag produced by a particular configuration. In this case, the propeller unfeathered (not rotating, worst case) would have the greatest drag configuration index because it would create the most drag compared to the other items listed.

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  • 18. 

    27. In altitude preference mode, changes to the power setting affect aircraft airspeed, while aircraft pitch responds to achieve commanded 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: T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.15.8.2

    • True

    • False

    Correct Answer
    A. True
    Explanation
    In altitude preference mode, changes to the power setting will impact the aircraft's airspeed. The aircraft pitch will then adjust in order to achieve the commanded altitude. If, for some reason, the aircraft is unable to maintain the set speed and altitude, it will prioritize maintaining the commanded altitude and achieve the fastest possible airspeed. This means that even if the aircraft cannot maintain the desired speed, it will still maintain the commanded altitude.

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  • 19. 

    29. A _________ indicates operating procedures, techniques, etc., which could result in personal injury and loss of life if not carefully followed. Ref: T.O. 1Q-9(M)A-1 Chap: Foreword Para: Warnings, Cautions, and Notes

    • Note

    • Warning

    • Caution

    • Advisory

    Correct Answer
    A. Warning
    Explanation
    A warning indicates operating procedures, techniques, etc., which could result in personal injury and loss of life if not carefully followed.

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  • 20. 

    30. _________ expresses a provision that is binding. Ref: T.O. 1Q-9(M)A-1 Chap: Foreword Para: Shall, Will, Should, and May

    • Shall

    • Should and May

    • Will

    • If

    Correct Answer
    A. Shall
    Explanation
    The term "shall" expresses a provision that is binding. In legal and contractual contexts, "shall" is often used to indicate a mandatory requirement or obligation. It implies that the action or condition described must be followed or fulfilled without exception.

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  • 21. 

    33. The EFIU monitors engine RPM received from the tach generator. If RPM drops below _____ % it automatically performs an inflight restart. Ref: T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.10.15

    • 28

    • 60

    • 78

    • 89.5

    • 92.5

    Correct Answer
    A. 78
    Explanation
    The EFIU monitors engine RPM received from the tach generator. If RPM drops below 78%, it automatically performs an inflight restart.

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  • 22. 

    34. The return manifold receives excess fuel from the ______ tank. Ref: T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.11.4

    • Aft

    • Forward

    • Center

    • Header

    Correct Answer
    A. Header
    Explanation
    The return manifold receives excess fuel from the header tank.

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  • 23. 

    35. If both electric fuel pumps fail, ________ Ref: T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.11.7 Warning

    • The engine will only continue to run until the fuel in the header tank is depleted

    • It is not possible to jettison fuel

    • The engine will immediately stop

    • A and B above

    • All of the above

    Correct Answer
    A. A and B above
    Explanation
    If both electric fuel pumps fail, the engine will only continue to run until the fuel in the header tank is depleted and it is not possible to jettison fuel. This means that once the fuel in the header tank is used up, the engine will no longer receive fuel and will stop running. Additionally, since it is not possible to jettison fuel, there is no way to remove excess weight from the aircraft to prolong the engine's operation. Therefore, both statements A and B above are correct.

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  • 24. 

    36. Batteries cannot be charged in flight.(MQ-9 Block 1 only) Ref: T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.12.5

    • True

    • False

    Correct Answer
    A. True
    Explanation
    The given answer is true because according to the reference T.O. 1Q-9(M)A-1, batteries cannot be charged in flight for the MQ-9 Block 1. This means that the batteries of the MQ-9 Block 1 cannot be recharged while the aircraft is in the air.

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  • 25. 

    39. 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: T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.15.2

    • ±5°, ± 40°

    • ± 10°, ± 40°

    • ± 10°, ± 60°

    • ± 15°, ± 60°

    Correct Answer
    A. ± 10°, ± 40°
    Explanation
    When Cruise Mode is turned on, the control sensitivity is reduced. This means that the aircraft will respond less to control inputs from the pilot. The roll, pitch, and yaw gains are scaled with airspeed, meaning that they are adjusted based on the speed of the aircraft. In this case, the scaling limits the roll to a maximum of ±10° and the yaw to a maximum of ±40°, depending on the airspeed. This means that the aircraft will only be able to roll up to 10° and yaw up to 40° when Cruise Mode is activated.

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  • 26. 

    43. Stall protect is turned on and off by the pilot, but only takes effect at speeds below ________. Ref: T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.15.10

    • .7 coefficient of lift

    • .8 coefficient of lift

    • 100 KIAS

    • 110 KIAS

    • 120 KIAS

    Correct Answer
    A. 120 KIAS
  • 27. 

    44. Stall protect prevents stall by deflecting the ruddervators down when AOA exceeds a threshold value of 7 degrees. Stall protect disengages when the AOA is less than 3 degrees. Ref: T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.15.10

    • True

    • False

    Correct Answer
    A. True
    Explanation
    Stall protect is a system that is designed to prevent an aircraft from stalling. In this case, the stall protect system activates when the angle of attack (AOA) exceeds 7 degrees. When this happens, the ruddervators (a combination of rudder and elevators) are deflected downward, which helps to maintain lift and prevent a stall. However, once the AOA drops below 3 degrees, the stall protect system disengages. Therefore, the statement that stall protect prevents stall by deflecting the ruddervators down when AOA exceeds 7 degrees and disengages when the AOA is less than 3 degrees is true.

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  • 28. 

    45. Mission programming employs "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: T.O. 1Q-9(M)A-1 Chap: 9 Para: 9.8.2 Note

    • True

    • False

    Correct Answer
    A. True
    Explanation
    Mission programming employs "fly-to" logic, which means that for each leg of the mission during autonomous flight, the aircraft will use the programmed settings for the upcoming waypoint. Once the aircraft passes the waypoint, the settings for the next waypoint will go into effect. This ensures that the aircraft follows the programmed flight path and executes the necessary actions at each waypoint.

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  • 29. 

    46. Lost link programming and the emergency mission will not activate if "Lost Link - OK" is set ON during an operational mission. Ref: T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.15.15 Caution

    • True

    • False

    Correct Answer
    A. True
    Explanation
    If "Lost Link - OK" is set ON during an operational mission, it means that the lost link programming is functioning properly. In this case, the emergency mission and the activation of the lost link programming will not take place because there is no need for it. This is stated in T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.15.15 Caution, which suggests that the statement is true.

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  • 30. 

    48. If EGI ________ 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: T.O. 1Q-9(M)A-1 Chap: 1 Para: 1.17.1.3

    • 1

    • 2

    • 3

    • 4

    Correct Answer
    A. 1
    Explanation
    If the EGI (Embedded GPS/INS) fails, the Ku SATCOM (Ku-band Satellite Communication) system will not be able to aim properly. This can result in the aircraft losing the Ku-band link and experiencing a lost link situation.

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  • 31. 

    49. 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-9(M)A-1 Chap: 1 Para: 1.18.1

    • Uplink, Downlink, Command Link, Return Link

    • Command Link, Return Link, Uplink, Downlink

    • Transmit, Receive, Command Link, Return Link

    • Command Link, Return Link, Transmit, Receive

    Correct Answer
    A. Uplink, Downlink, Command Link, Return Link
    Explanation
    The transmission of the C-Band LOS datalink is referred to as the uplink and downlink, while the Ku-Band SATCOM transmissions are called the command link and return link.

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  • 32. 

    50. The IR nose camera has its own heater and fan to prevent fogging. Ref: T.O. 1Q-9(M)A-1 Chap 1 Para 1.28.2

    • True

    • False

    Correct Answer
    A. True
    Explanation
    The IR nose camera has its own heater and fan to prevent fogging, as stated in T.O. 1Q-9(M)A-1 Chap 1 Para 1.28.2. This means that the camera is equipped with a heating element and a fan that work together to keep the lens clear of fog, ensuring that the camera can capture clear images even in conditions where fogging may occur.

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  • 33. 

    52. The _________ mode (of the ARC-210) provides continuous scanning of four preset channels. Ref: T.O. 1Q-9(M)A-1 Chap 1 Para 1.31.1.1.8

    • Manual

    • Scan

    • Preset

    • Anti-jam

    Correct Answer
    A. Scan
    Explanation
    The correct answer is "Scan". According to the given reference, the Scan mode of the ARC-210 provides continuous scanning of four preset channels.

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  • 34. 

    53. 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: T.O. 1Q-9(M)A-1 Chap: 9 Para: 9.3.1

    • White

    • Red

    • Yellow

    • Green

    Correct Answer
    A. Yellow
    Explanation
    A yellow background on a VIT data element indicates an abnormal condition. This is because a yellow background generally indicates that the value is out of the normal operating parameters and should be monitored. This information is based on T.O. 1Q-9(M)A-1 Chap: 9 Para: 9.3.1.

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  • 35. 

    57. Data from the Preset Configuration window cannot be applied/uploaded if the aircraft airspeed is above ________ KIAS. Ref: T.O. 1Q-9(M)A-1 Chap: 2 Para: 2.13 Note

    • 40

    • 50

    • 60

    • 70

    Correct Answer
    A. 50
  • 36. 

    59. The engine may exceed maximum allowable EGT when disengaging Altitude Hold with the throttle in the _______ position. Ref: T.O. 1Q-9(M)A-1 Chap: 2 Para: 2.30 Step 8 Caution

    • Full aft

    • Midrange

    • Full forward

    • Full reverse

    Correct Answer
    A. Full forward
    Explanation
    When disengaging Altitude Hold with the throttle in the Full forward position, there is a possibility that the engine may exceed the maximum allowable Exhaust Gas Temperature (EGT). This information can be found in T.O. 1Q-9(M)A-1, Chapter 2, Paragraph 2.30, Step 8 Caution.

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  • 37. 

    60. During an MCE gaining handover, the Ku command link is established when: Ref: T.O. 1Q-9(M)A-1 Chap: 2 Para: 2.27 Step 17

    • I say it is

    • The "Ku Command Link Lost" warning message disappears

    • System amps increase by approximately 10 amps

    • Uplink signal strength increases

    Correct Answer
    A. The "Ku Command Link Lost" warning message disappears
    Explanation
    During an MCE gaining handover, the Ku command link is established when the "Ku Command Link Lost" warning message disappears. This indicates that the communication link between the MCE and the Ku command has been restored and is functioning properly. The disappearance of the warning message signifies that the handover process has been completed successfully and the system is now able to transmit and receive commands via the Ku command link.

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  • 38. 

    61. Airspeed, altitude and heading hold should be set to ensure valid parameters are set in the autopilot, in the event an inadvertent uplink is established. Ref: T.O. 1Q-9(M)A-1 Chap: 2 Para: 2.38 Step 36 Caution

    • True

    • False

    Correct Answer
    A. True
    Explanation
    The explanation for the given correct answer is that setting the airspeed, altitude, and heading hold in the autopilot ensures that valid parameters are established. This is important in case there is an inadvertent uplink, meaning an unintentional communication or data transfer, that could potentially affect the autopilot settings. By having the correct parameters set, the autopilot can continue to operate effectively and maintain the desired airspeed, altitude, and heading.

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  • 39. 

    62. Upon Successful hand-off it is necessary to update the datalink preset values found in Section 1; 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 in the HDD for any of these items will not update any values. Ref: T.O. 1Q-9(M)A-1 Chap: 2 Para: 2.38 Step 51 Caution

    • True

    • False

    Correct Answer
    A. True
    Explanation
    Upon successful hand-off, updating the datalink preset values in Section 1 is necessary to ensure that the aircraft does not retain the preset values for the losing Ground Control Station (GCS). If any of the preset values are changed in the HDD (Handheld Display Device), all preset values will be resent to the aircraft. However, entering an identical value in the HDD for any of these items will not update any values. This information is referenced from T.O. 1Q-9(M)A-1, Chapter 2, Paragraph 2.38, Step 51 Caution.

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  • 40. 

    63. 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: T.O. 1Q-9(M)A-1 Chap: 2 Para: 2.41 Step 3 Caution

    • True

    • False

    Correct Answer
    A. True
    Explanation
    During descent, the actual nose camera lens inside the fuselage may become fogged. This fogging cannot be prevented by using nose lens heat. However, the Nose IR lens heater can be used to clear the nose EO camera. This information is stated in T.O. 1Q-9(M)A-1 Chap: 2 Para: 2.41 Step 3 Caution. Therefore, the statement is true.

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  • 41. 

    64. If power is shut off due to a GCS fire, the UPS batteries will still provide power if they were not turned off prior to evacuation. Ref: T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.68 Step 6

    • True

    • False

    Correct Answer
    A. True
    Explanation
    According to T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.68 Step 6, if power is shut off due to a GCS fire, the UPS batteries will still provide power if they were not turned off prior to evacuation. This means that even if the power is shut off, the UPS batteries will continue to supply power. Therefore, the statement "If power is shut off due to a GCS fire, the UPS batteries will still provide power if they were not turned off prior to evacuation" is true.

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  • 42. 

    65. 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: T.O. 1Q-9(M)A-1 Chap 3 Para 3.71

    • True

    • False

    Correct Answer
    A. True
    Explanation
    In the given statement, it is mentioned that in case of a left PSO rack failure or lock-up, the pilot can choose to send the aircraft lost link before following the PSO-1 Rack Lock-Up checklist. This means that the pilot has the option to inform about the lost link before taking further actions. The reference provided supports this statement. Therefore, the correct answer is True.

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  • 43. 

    67. Loss of control may be indicated by complete failure of the aircraft to respond to pilot control command. This may be caused by ____________. Ref: T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.34

    • Airspeed or pitot/static failure

    • Catastrophic AOA failure below 120 KIAS with stall protect on, SAS failure

    • Autopilot sensor failure, structural failure or airframe icing

    • All of the above

    Correct Answer
    A. All of the above
    Explanation
    Loss of control may be indicated by a complete failure of the aircraft to respond to pilot control commands. This can be caused by various factors, including airspeed or pitot/static failure, catastrophic angle of attack (AOA) failure below 120 KIAS with stall protect on, SAS failure, autopilot sensor failure, structural failure, or airframe icing. Therefore, all of the above options can contribute to the loss of control in an aircraft.

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  • 44. 

    68. A stall condition may be indicated by ____________ . Ref: T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.41

    • Warnings on the pilot HUD

    • Excessively high AOA

    • Unexpected loss of altitude

    • All of the above

    Correct Answer
    A. All of the above
    Explanation
    A stall condition may be indicated by warnings on the pilot HUD, excessively high AOA, and unexpected loss of altitude. These indicators can help the pilot recognize that the aircraft is approaching or has entered a stall, which is a dangerous condition where the airflow over the wings becomes disrupted and lift is greatly reduced. By recognizing these indicators, the pilot can take appropriate actions to recover from the stall and regain control of the aircraft.

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  • 45. 

    69. Pitot heat does not guarantee the absence of ice from the pitot/static system. Moisture can freeze in the unheated areas. This malfunction may be indicated by an FCA PPT sensor warning message, abnormal attitude, abnormal airspeed or a combination of any of these. These conditions may result in ____________ .

    • Aircraft pitch down or oscillations

    • Loss of datalink

    • Loss of aircraft control

    • All of the above

    Correct Answer
    A. All of the above
    Explanation
    Pitot heat does not guarantee the absence of ice from the pitot/static system. Moisture can still freeze in the unheated areas, leading to various malfunctions. These malfunctions can be indicated by an FCA PPT sensor warning message, abnormal attitude, abnormal airspeed, or a combination of any of these. These conditions can result in aircraft pitch down or oscillations, loss of datalink, or loss of aircraft control. Therefore, all of the above options can occur as a result of this malfunction.

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  • 46. 

    70. If an aileron or tail servo enters the red region, land as soon as possible. Ref: T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.38 Step 2 Caution

    • True

    • False

    Correct Answer
    A. True
    Explanation
    According to T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.38 Step 2 Caution, if an aileron or tail servo enters the red region, it is necessary to land as soon as possible.

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  • 47. 

    71. When battery voltage drops below ________ volts, all electrical power may be lost. Ref: T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.11 Step 6 Caution

    • 21

    • 24

    • 22

    • 28

    Correct Answer
    A. 22
    Explanation
    When the battery voltage drops below 22 volts, there is a risk of losing all electrical power. This information is stated in T.O. 1Q-9(M)A-1 Chapter 3, Paragraph 3.11, Step 6 Caution.

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  • 48. 

    72. Do not allow the engine to windmill between _______ and ________ percent RPM. Operation within this range may cause engine damage. Ref: T.O. 1Q-9(M)A-1 Chap: 3 Para: 3.11 Step 7 Caution

    • 18-28

    • 10-28

    • 60-65

    • 50-68

    Correct Answer
    A. 18-28
  • 49. 

    74. ER With aircraft weight greater than 10,500 lbs, maneuvering at a bank angle greater than 30º in level flight, or greater than 25º while climbing will result in the aircraft pitching up and achieving high AOA. Ref: ASI-09069 Chap: 1 Para: 1.8.3 Warning

    • True

    • False

    Correct Answer
    A. True
    Explanation
    Maneuvering an aircraft with a weight greater than 10,500 lbs, at a bank angle greater than 30° in level flight, or greater than 25° while climbing, will cause the aircraft to pitch up and achieve a high angle of attack (AOA). This information is stated in ASI-09069, Chapter 1, Paragraph 1.8.3 as a warning. Therefore, the statement is true.

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  • Jul 22, 2024
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  • Apr 23, 2019
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