Aircraft systems are very delicate therefore special care should be given to them in regards to management. Do you think that you understood everything we discussed in class these past months on the systems? If you said yes, test yourself by taking up this specialized and easy quiz. All the best!
Vacuum system
Fuel pump
Mixture
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Vacuum system
Airspeed indicator
Mixture
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The white radial line
The orange radial line
The red radial line
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Prevent moisture condensation by eliminating airspace in the tanks
Enrich the mixture
Improve engine performance
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Loss of power
In the event engine-driven fuel pump fails
Excessive oil consumption
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Attitude indicator, heading indicator, and turn coordinator
Altimeter, engine-driven fuel pump, cabin heat indicator
Airspeed Indicator, vertical speed indicator, and transponder mode C
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Periodically realign the magnetic compass as the gyro processes
Adjust for proper RPM and check for desired indications on the engine gauges
Use electric-driven pump
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The maintenance drains
The pitot-static tube
Fuel strainer drain and the fuel tank sumps
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VFE
VA
VNE
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Stall
Never exceed speed
Maximum cruising speed
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By the relationship of the mini plane to the deflected horizon bar
By the relationship between the altimeter and the airspeed indicator
By the relationship of
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Periodically realigned with the magnetic compass as the gyro processes
Connected to the vaccum system
Properly aligned with the turn coordinator
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Automatic mixture control
Improved engine performance
Regulating oil pressure level
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Diesel
AVGAS 100LL or 100
AVGAS 200LL or 200
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Top of green arc
The extent of white arc
Top of red arc
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The fuel level being too low
The oil level being too high
The oil level being too low
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Not enough power and with the mixture set too rich
Too many red hots in his/her pocket
Too much power and with the mixture set too lean
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The red arc
The white arc
The yellow arc
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Increase change of excessive oil consumption
Increases risk of overheating the engine
Reduces aircraft performance
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Cause the cylinder head temperature and engine oil temperature gauges to exceed their normal operating ranges
Cause loss of power, excessive oil consumption, and possible permanent internal engine damage
Cause a false reading on the altimeter and heading
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The red arc
The white arc
The green arc
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Reduce rate of climb and increase airspeed
Abort
Reduce rate of climb and decrease airspeed
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Top of green arc
The red radial line
The extent of white arc
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The automatic mixture control is part of the electric driven fuel pump
The automatic mixture control is part of the engine driven fuel pump
The automatic mixture control is part of the oil driven fuel pump
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Oil temperature and oil pressure
Vertical speed indicator with the airspeed indicator
Mini airplane to the horizon bar
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Altimeter will indicate 150 feet lower
Altimeter will indicate 0.15 feet lower
Altimeter will indicate 150 feet higher
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The lower limit of the white arc
The top of the white arc
The top of the green arc
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700 foot decrease in indicated altitude
700 foot increase in true altitude
700 foot increase in indicated altitude
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Top of green arc
The extent of white arc
The red radial line
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Electric-driven fuel pump
Engine-drive fuel pump
Auxiliary electric-driven pump
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Pitot-static system
Vacuum system
Electrical system
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Adjust for proper RPM
Pop the hood
Enrich the mixture
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300 to 420 degree Celsius
300 to 420 degrees Fahrenheit
42 to 300 degrees Fahrenheit
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Once
Twice
Three times
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Upper limit of the white arc
The extent of the green arc
Lower limit of the white arc
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17 lbs
64 lbs
44 lbs
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Air enters the system through the air filter behind the left side of the instrument panel
Air enters the system through the air filter behind the right side of the instrument panel
Air leaves the system through the air filter behind the left side of the instrument panel
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The circulation of lubricating oil
RAM air from air intakes
Gasoline (100LL or better)
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Airspeed indicator, altimeter, vertical speed indicator and transponder mode A
Airspeed indicator, altimeter, vertical speed indicator and transponder mode C
Airspeed indicator, altimeter, vertical speed indicator and transponder mode B
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Altimeter and attitude indicator
Heading indicator and vacuum indicator
Attitude indicator and heading indicator
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Excessively low oil quantity
Extreme weather conditions
Using fuel that has a lower-than-specified fuel rating
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May continue to fire
Will fail to fire
May produce sparks
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5.3-52.3psi
3.2-35.2psi
3.5-32.5psi
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Experience avionics equipment failure
Assess the situation, take proper action
Experience total electrical failure
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Pitot-static system
Vacuum system
Electrical system
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45
90
23
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Lower limit of the white arc
Lower limit of the green arc
Upper limit of the white arc
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Quiz Review Timeline (Updated): Jul 26, 2024 +
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