Term
| Where is the fuel mixture controlled in the DA20-C1? |
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Definition
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Term
| Which V-speed represents maximum flap extended speed? |
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Definition
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Term
| Flight through rain in a DA20-C1 |
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Definition
| reduces aircraft performance |
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Term
| Excessively high engine temperatures, either in the air or on the ground, will |
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Definition
| cause loss of power, excessive oil consumption, and possible permanent internal engine damage |
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Term
What is one procedure to aid in cooling an engine that is overheating? |
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Definition
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Term
What is the maximum structural cruising speed? (picture of airspeed gauge included) |
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Definition
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Term
| Which would most likely cause the cylinder head temperature and engine oil temperature gauges to exceed their normal operating ranges? |
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Definition
| Using fuel that has a lower-than-specified fuel rating |
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Term
| If the engine oil temperature and cylinder head temperature gauges have exceeded their normal operating range, the pilot may have been operating with |
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Definition
| Too much power and with the mixture set too lean |
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Term
| What action can a pilot take to aid in cooling an engine that is overheating during a climb? |
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Definition
| Reduce rate of climb and increase airspeed |
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Term
| A circuit breaker may be reset how many times? |
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Definition
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Term
| How should a pilot determine the direction of bank from an attitude indicator? (picture of attitude indicator included) |
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Definition
By the relationship of the miniature airplane (C) to the deflected horizon (B) |
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Term
| Excessively high engine temperatures will |
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Definition
| cause loss of power, excessive oil consumption, and possible permanent internal engine damage |
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Term
| What power source spins the gyro in the Turn Coordinator? |
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Definition
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Term
| Which of the following instruments utilize a gyro? |
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Definition
Attitude Indicator, Heading Indicator, and Turn Coordinator |
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Term
| Which items are connected to the static port on the pilot-static probe? |
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Definition
| Airspeed Indicator, Altimeter, Vertical Speed Indicator, and Transponder Mode C |
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Term
| The fuel pressure normal operating range in the DA20-C1 is |
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Definition
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Term
What should be the first action after starting an aircraft engine? |
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Definition
| Adjust for proper RPM and check for desired indications on the engine gauges |
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Term
| One purpose of the dual ignition system on an aircraft engine is to provide for |
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Definition
| improved engine performance |
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Term
| Which color identifies the power-off stalling speed in a specified configuration? (picture of airspeed gauge included |
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Definition
| Lower limit of the green arc |
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Term
| What is the caution range of the airplane? (picture of airspeed gauge included) |
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Definition
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Term
| Which color identifies the never-exceed speed? (picture of airspeed gauge included) |
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Definition
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Term
| Which fuel system statement is true? |
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Definition
| The Mixture Control is part of the engine driven fuel pump |
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Term
| The proper adjustment to make on the attitude indicator during level flight is to align the (picture or attitude indicator included) |
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Definition
| miniature airplane (C) to the horizon bar |
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Term
| This altimeter indicates (picture of altimeter included) |
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Definition
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Term
What color identifies the normal flap operating range? (picture of airspeed gauge included) |
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Definition
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Term
| What does the red line on the airspeed indicator represent? |
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Definition
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Term
| To receive accurate indications during flight from a heading indicator, the instrument must be (picture of gauge included) |
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Definition
periodically realigned with the magnetic compass as the gyro precesses |
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Term
| If the ignition switch ground wire becomes disconnected, the magneto |
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Definition
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Term
| For internal cooling, air cooled engines are especially dependent on |
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Definition
| the circulation of lubricating oil |
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Term
| This altimeter indicates (picture of gauge included) |
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Definition
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Term
| Filling the fuel tanks after the last flight of the day is considered a good operating procedure because this will |
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Definition
| prevent moisture condensation by eliminating airspace in the tanks |
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Term
On aircraft equipped with fuel pumps, when is the auxiliary electric driven pump used? |
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Definition
| In the event engine-driven fuel pump fails |
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Term
What is the full flap operating range of the airplane? (picture of airspeed gauge included) |
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Definition
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Term
What power source spins the gyro in the heading indicator? |
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Definition
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Term
| Which color identifies the power-off stalling speed with wing flaps and landing gear in the landing configuration? (picture of airspeed indicator included |
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Definition
| Lower limit of the white arc |
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Term
An abnormally high engine oil temperature indication may be caused by |
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Definition
the oil level being too low |
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Term
The pitot system provides impact pressure for which instruments? |
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Definition
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Term
| This altimeter indicates (picture of gauge included) |
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Definition
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Term
Which items are connected to the pilot-static system? |
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Definition
| Airspeed indicator, Altimeter, Vertical Speed Indicator, and Transponder Mode C |
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Term
| A turn coordinator provides an indication of the (picture of turn coordinator included) |
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Definition
| movement of the aircraft about the yaw and roll axes |
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Term
| Which items are connected to the vacuum system? |
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Definition
| Attitude Indicator and Heading Indicator |
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Term
| What is the maximum flaps extended speed? (picture of airspeed indicator included) |
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Definition
| 100 (upper limit of white arc) |
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Term
| Which DA20-C1 vacuum system statement is true? |
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Definition
| Air enters the system through the air filter behind the left side of the instrument panel |
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Term
| The maximum allowable weight in the baggage compartment of the DA20-C1 is _____ pounds (not multiple choice) |
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Definition
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Term
| If a pilot changes the altimeter setting from 30.11 to 29.96, what is the approximate change in indication? |
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Definition
| Altimeter will indicate 150 feet lower |
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Term
| The cylinder head temperature (CHT) normal operating range is: |
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Definition
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Term
| To properly purge water from the fuel system of an aircraft equipped with fuel tank sumps and a fuel strainer quick drain, it is necessary to drain fuel from the |
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Definition
| fuel strainer drain and the fuel tank sumps |
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Term
| The maximum speed at which the airplane can be operated in smooth air is (picture of airspeed indicator included) |
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Definition
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Term
What power source spins the gyro in the attitude indicator? |
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Definition
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Term
| When the flaps are in the LDG position in the DA20-C1, they are extended ____ degrees (not multiple choice) |
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Definition
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Term
| An electrical system failure (battery and alternator) occurs during flight. In this situation, you would |
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Definition
| experience avionics equipment failure |
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Term
| What type of fuel does the DA20-C1 use? |
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Definition
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Term
If it is necessary to set the altimeter from 29.15 to 29.85, what change occurs? |
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Definition
| 700 foot increase in indicated altitude |
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