CPL AGK Exam with all Correct & 100% Verified Answers |Actual
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rapid opening and closing of the throttle. ✔Correct Answer-A detuning of engine crankshaft
couterweights is a source of overstress that may be caused by:
airspeed and RPM. ✔Correct Answer-A fixed-pitch propeller is designed for best efficiency
only at a given combination of
Left around the vertical axis, and to the right around the longitudinal axis ✔Correct Answer-A
propeller rotating clockwise as seen from the rear, creates a spiralling slipstream. The spiralling
slipstream, along with torque effect, tends to rotate the airplane to the
Idle the engine and momentarily turn the ignition off ✔Correct Answer-A way to detect a
broken magneto primary grounding lead is to
The oil level being too low ✔Correct Answer-An abnormally high engine oil temperature
indication may be caused by
Enrich the fuel/air mixture ✔Correct Answer-Applying carburetor heat will
Should not normally happen. Indicates a magneto not grounding in OFF position ✔Correct
Answer-Before shutdown, while at idle, the ignition key is momentarily turned OFF. The engine
continues to run with no interruption; this
Installation and instrument error ✔Correct Answer-Calibrated airspeed is best descried as
indicated airspeed corrected for
Using a lower grade of fuel than recommended ✔Correct Answer-Detonation can be caused
by:
Detonation may occur at high-power settings when: ✔Correct Answer-the fuel mixture ignites
instantaneously instead of burning progressively and evenly
The unburned fuel/air change in the cylinders is subjected to instantaneous combustion
✔Correct Answer-Detonation occurs in a reciprocating aircraft engine when
One hundred eighty (180) degrees turn ✔Correct Answer-Errors in both pitch and bank
indicator or an attitude indicator are usually at a maximum as the aircraft rolls out of a
The circulation of lubricating oil ✔Correct Answer-For internal cooling, reciprocating aircraft
engines are especially dependent on
, Gains altitude with no mixture adjustment ✔Correct Answer-Fouling of spark plugs is more
apt to occur if the aircraft
Exhaust gases leaking into the cockpit ✔Correct Answer-Frequent inspections should be made
of aircraft exhaust manifold-type heating systems to minimize the possibility of
Weight of fuel and weight of air entering the cylinder ✔Correct Answer-Fuel/air ratio is the
ratio between the
Could accidentally start if the propeller is moved with fuel in the cylinder ✔Correct Answer-If
the ground wire between the magneto and the ignition switch becomes disconnected, the
engine
Increased, increased the RPM before increasing the manifold pressure ✔Correct Answer-In
aircraft equipped with constant-speed propellers and normally-aspirated engines, which
procedure should be used to avoid placing undue stress on the engine components? When
power is being:
Will increase the ground roll ✔Correct Answer-Leaving the carburetor heat on during takeoff
Normal operations ✔Correct Answer-Maximum structural cruising speed is the maximum
speed at which an airplane can be operated during
Provide the same area amount of lift at a slower airspeed ✔Correct Answer-One of the main
functions of flaps during the approach and landing is to:
Ratio of thrust horsepower to brake horsepower ✔Correct Answer-propeller efficiency is the:
Decrease the fuel flow to compensate for decreased air density ✔Correct Answer-The basic
purpose of adjusting the fuel/air mixture control at altitude is to:
The most power can be obtained for any given throttle setting ✔Correct Answer-The best
power mixture is the fuel/air ratio at which
Prevents the fuel/air combination from becoming too rich at higher altitudes ✔Correct
Answer-The mixture control can be adjusted, which
A broken magneto ground wire ✔Correct Answer-The most probable reason an engine
continues to run after the ignition switch has been turned off is:
Mixture control ✔Correct Answer-The pilot controls the air/fuel ratio with the:
Complete Update |Already Graded A+ (Just Released)
rapid opening and closing of the throttle. ✔Correct Answer-A detuning of engine crankshaft
couterweights is a source of overstress that may be caused by:
airspeed and RPM. ✔Correct Answer-A fixed-pitch propeller is designed for best efficiency
only at a given combination of
Left around the vertical axis, and to the right around the longitudinal axis ✔Correct Answer-A
propeller rotating clockwise as seen from the rear, creates a spiralling slipstream. The spiralling
slipstream, along with torque effect, tends to rotate the airplane to the
Idle the engine and momentarily turn the ignition off ✔Correct Answer-A way to detect a
broken magneto primary grounding lead is to
The oil level being too low ✔Correct Answer-An abnormally high engine oil temperature
indication may be caused by
Enrich the fuel/air mixture ✔Correct Answer-Applying carburetor heat will
Should not normally happen. Indicates a magneto not grounding in OFF position ✔Correct
Answer-Before shutdown, while at idle, the ignition key is momentarily turned OFF. The engine
continues to run with no interruption; this
Installation and instrument error ✔Correct Answer-Calibrated airspeed is best descried as
indicated airspeed corrected for
Using a lower grade of fuel than recommended ✔Correct Answer-Detonation can be caused
by:
Detonation may occur at high-power settings when: ✔Correct Answer-the fuel mixture ignites
instantaneously instead of burning progressively and evenly
The unburned fuel/air change in the cylinders is subjected to instantaneous combustion
✔Correct Answer-Detonation occurs in a reciprocating aircraft engine when
One hundred eighty (180) degrees turn ✔Correct Answer-Errors in both pitch and bank
indicator or an attitude indicator are usually at a maximum as the aircraft rolls out of a
The circulation of lubricating oil ✔Correct Answer-For internal cooling, reciprocating aircraft
engines are especially dependent on
, Gains altitude with no mixture adjustment ✔Correct Answer-Fouling of spark plugs is more
apt to occur if the aircraft
Exhaust gases leaking into the cockpit ✔Correct Answer-Frequent inspections should be made
of aircraft exhaust manifold-type heating systems to minimize the possibility of
Weight of fuel and weight of air entering the cylinder ✔Correct Answer-Fuel/air ratio is the
ratio between the
Could accidentally start if the propeller is moved with fuel in the cylinder ✔Correct Answer-If
the ground wire between the magneto and the ignition switch becomes disconnected, the
engine
Increased, increased the RPM before increasing the manifold pressure ✔Correct Answer-In
aircraft equipped with constant-speed propellers and normally-aspirated engines, which
procedure should be used to avoid placing undue stress on the engine components? When
power is being:
Will increase the ground roll ✔Correct Answer-Leaving the carburetor heat on during takeoff
Normal operations ✔Correct Answer-Maximum structural cruising speed is the maximum
speed at which an airplane can be operated during
Provide the same area amount of lift at a slower airspeed ✔Correct Answer-One of the main
functions of flaps during the approach and landing is to:
Ratio of thrust horsepower to brake horsepower ✔Correct Answer-propeller efficiency is the:
Decrease the fuel flow to compensate for decreased air density ✔Correct Answer-The basic
purpose of adjusting the fuel/air mixture control at altitude is to:
The most power can be obtained for any given throttle setting ✔Correct Answer-The best
power mixture is the fuel/air ratio at which
Prevents the fuel/air combination from becoming too rich at higher altitudes ✔Correct
Answer-The mixture control can be adjusted, which
A broken magneto ground wire ✔Correct Answer-The most probable reason an engine
continues to run after the ignition switch has been turned off is:
Mixture control ✔Correct Answer-The pilot controls the air/fuel ratio with the:
