PILOT PROFICIENCY

CARAVAN 208/208B/EX G1000 Questions

54

Ground School Cessna Grand Caravan

CARAVAN 208/208B/EX G1000 PILOT TRAINING MANUAL Questions

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1.

If the pilot PFD fails, the MFD:

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2.

If the nose gear is turned past the maximum placarded travel limit:

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3.

The power turbine is on a shaft that:

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4.

The two GDC 72 air data computers supply information to which instruments?

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5.

According to the “Engine Fire in Flight” checklist, a red ENGINE FIRE CAS annunciation and warning chime:

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6.

The ice detector light is used:

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7.

The taxi/recognition lights are:

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8.

If the fuel filter becomes blocked:

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9.

The two FUEL TANK SELECTOR knobs on the overhead panel:

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10.

The CWS button on the control yoke:

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11.

The CABIN HEAT FIREWALL SHUTOFF knob:

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12.

Pressing the ALERTS softkey for the crew alert system displays the:

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13.

Fuel rejected during engine shutdown:

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14.

The minimum Ng when operating the air conditioning on the ground is:

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15.

When the EXTERNAL POWER switch is positioned to BUS:

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16.

The inertial separator should be positioned to the bypass position:

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17.

When the anti-ice fluid control switch operates in MAX FLOW AIRFRAME, a red readout on the MFD indicates:

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18.

The rudder trim system:

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19.

While operating the GWX weather radar system on the ground, ensure that:

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20.

The BARO MIN setting on the PFD is:

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21.

Loss of any pneumatic signal to the fuel control unit causes:

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22.

The parking brake is applied by:

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23.

The standby flap system is operated:

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24.

The lead-acid battery case is vented to prevent:

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25.

The maximum endurance level with a fully serviced anti-ice fluid tank in NORMAL is:

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26.

What must be accomplished when operating the air conditioning on the ground if ITT threatens to exceed 700°C:

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27.

During the overspeed governor test, the propeller rpm should not exceed:

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28.

The flashing beacon is used for:

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29.

The minimum de-ice fluid level for dis-patch into forecast icing conditions is:

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30.

Positioning the AVIONICS BUS TIE switch to ON:

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31.

With the propeller control lever positioned to MAX:

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32.

When operating with the anti-ice fluid control switch in NORMAL, a green readout on the MFD indicates that at least:

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33.

The strobe lights are required:

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34.

Engine oil level should be:

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35.

The fire-detection test function assures:

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36.

The oxygen system controls are:

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37.

The fuel-selector-off warning system sounds when:

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38.

The torque indication indicates the power:

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39.

The voltmeter and its associated selector button are used to read:

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40.

The IGNITION switch should be positioned to ON:

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41.

Fuel is pumped from the reservoir tank primarily by the:

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42.

The fire-detection system warns of excessive temperature in the engine compartment

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43.

The standby electrical system:

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44.

When the pilot chooses a lateral or vertical mode on the mode controller, the AFCS status box indicates:

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45.

The standby electrical power system is required to be installed and functional for:

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46.

When the STARTER switch is positioned to START:

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47.

The PLAY key on the audio panel allows:

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48.

The in-flight ice protection equipment provides:

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49.

The air conditioning system is:

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50.

Use landing lights during:

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51.

A WARNING ALERT accompanied by a continuous chime indicates a condition that:

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52.

Fuel flows from the wing tanks to the reservoir tank by:

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53.

The temperature at which the fire warning initiates is:

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54.

The generator control unit (GCU) controls operation of the:

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55.

The battery is:

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56.

The rudder pedals can be used to steer the nose gear approximately:

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57.

The maximum endurance level with a fully serviced anti-ice fluid tank in MAX FLOW AIRFRAME is:

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58.

The rudder lock:

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59.

The anti-ice fluid tank has a capacity of:

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60.

During operations using the emergency power lever:

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61.

The courtesy lights are controlled by:

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62.

Air induced into the engine:

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63.

The wing spoilers:

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64.

Operation of the air conditioner can cause compass deviation of more than:

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65.

The PT6A-140 engine is defined as a:

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66.

The auxiliary fuel boost pump switch:

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67.

The ground power monitor:

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