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!
Loss of power
In the event engine-driven fuel pump fails
Excessive oil consumption
Movement of the aircraft about the yaw and roll axes
Electrical system
Cylinder head temperature
Diesel
AVGAS 100LL or 100
AVGAS 200LL or 200
Upper limit of the white arc
The extent of the green arc
Lower limit of the white arc
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
Top of green arc
The extent of white arc
Top of red arc
The fuel level being too low
The oil level being too high
The oil level being too low
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
Top of green arc
The red radial line
The extent of white arc
Top of green arc
The extent of white arc
The red radial line
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
17 lbs
64 lbs
44 lbs
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
The red arc
The white arc
The green arc
Altimeter will indicate 150 feet lower
Altimeter will indicate 0.15 feet lower
Altimeter will indicate 150 feet higher
Altimeter and attitude indicator
Heading indicator and vacuum indicator
Attitude indicator and heading indicator
Periodically realigned with the magnetic compass as the gyro processes
Connected to the vaccum system
Properly aligned with the turn coordinator
Automatic mixture control
Improved engine performance
Regulating oil pressure level
Adjust for proper RPM
Pop the hood
Enrich the mixture
Vacuum system
Fuel pump
Mixture
Vacuum system
Airspeed indicator
Mixture
5.3-52.3psi
3.2-35.2psi
3.5-32.5psi
45
90
23
Stall
Never exceed speed
Maximum cruising speed
The white radial line
The orange radial line
The red radial line
Wait!
Here's an interesting quiz for you.