Commercial Pilot - Written Verified Multiple Choice
and Conceptual Actual Emended Exam Questions
With Reviewed 100% Correct Detailed Answers
Guaranteed Pass!!Current Update!!
1. As altitude increases, the VNE of helicopter will
A. Increase
B. Decrease
C. Remain the same - ANSWER B. Decrease
2. The anti-torque system fails during cruising flight and a powered approach
landing is commenced. The helicopter yaws to the right just prior to touchdown,
what could the pilot do to help swing the nose to the left?
A. Increase the throttle
B. Decrease the throttle
C. Increase the collective pitch - ANSWER B. Decrease the throttle
3. If anti-torque failure occurred during cruising flight, what would be done to help
straighten out the left yellow prior to touch down?
A. A normal running landing should be made
B. Make a running landing using partial power and left cyclic
,C. Apply available throttle to help swing the nose to the right just prior to
touchdown - ANSWER C. Apply available throttle to help swing the nose to the
right just prior to touchdown
4. Should a helicopter pilot ever be concerned about ground resonance during
takeoff?
A. No; ground resonance occurs only during an autorotation touchdown
B. Yes; although it is more likely to occur on landing, it can occur during takeoff.
C. Yes; but only during slope takeoffs - ANSWER B. Yes; although it is more
likely to occur on landing, it can occur during takeoff.
5. An excessively steep approach angle and abnormally slow closure rates should
be avoided during an approach to a hover, primarily because
A. The airspeed indicator would be unreliable
B. A go around would be very difficult to accomplish
C. Settling with power could develop, particularly during the termination -
ANSWER C. Settling with power could develop, particularly during the
termination
6. During a near vertical power approach into a confined area with the airspeed
near zero, what hazardous condition may develop?
A. Ground resonance
B. Settling with power
C. Blade stall vibration - ANSWER B. Settling with power
,7. Which procedure will result in recovery from settling with power?
A. Increase collective pitch and power
B. In tank testing collective pitch and increase throttle
C. Increase forward speed and reduce collective pitch - ANSWER C. Increase
forward speed and reduce collective pitch
8. In addition of power and settling with power situation produces an
A. Increase in airspeed
B. Even greater rate of descent
C. Increase the cyclic control effectiveness - ANSWER B. Even greater rate of
descent
9. Under which situation is accidental settling with power likely to occur?
A. A steep approach in which the airspeed is permitted to drop to nearly 0
B. It shall approach in which the airspeed is permitted to drop below 10 mph
C. Covering in ground effect during calm wind, high density altitude conditions -
ANSWER A. A steep approach in which the airspeed is permitted to drop to
nearly 0
10. To recover from settling with power condition, the pilot should
A. Apply forward cyclic and simultaneously reduce collective, if of Altitude permits
B. Not apply into dark metal during the recovery
C. Increase rotor rpm, reduce forward airspeed, and minimize maneuvering -
ANSWER A. Apply forward cyclic and simultaneously reduce collective, if of
Altitude permits
, 11. When operating at high forward speed, retreating blade stall is more likely to
occur under conditions of
A. Low gross weight, high density altitude, and smooth air
B. High gross weight, low density altitude, and smoother
C. high gross weight, high density altitude, in turbulent air - ANSWER C. high
gross weight, high density altitude, in turbulent air
12. What are the major indications of a incipient retreating blade stall situation, in
order of occurrence?
A. Low-frequency vibration, Pitch up of the nose, and a role in the direction of the
retreating blade
B. Slow pitch up of the nose, high-frequency vibration, and a tendency for the
helicopter to roll
C. Slow pitch up of the nose, tendency for the helicopter to roll, followed by a
medium frequency vibration - ANSWER A. Low-frequency vibration, Pitch up
of the nose, and a role in the direction of the retreating blade
13. How should a pilot react on the onset of retreating blade stall?
A. Reduce collective pitch, rotor rpm, and forward airspeed
B. Reduce collective pitch, increase rotor rpm, and reduce forward airspeed
C. Increase collective pitch, reduce rotor rpm, and reduce forward airspeed -
ANSWER B. Reduce collective pitch, increase rotor rpm, and reduce forward
airspeed
14. The most power will be required to hover over which surface?
and Conceptual Actual Emended Exam Questions
With Reviewed 100% Correct Detailed Answers
Guaranteed Pass!!Current Update!!
1. As altitude increases, the VNE of helicopter will
A. Increase
B. Decrease
C. Remain the same - ANSWER B. Decrease
2. The anti-torque system fails during cruising flight and a powered approach
landing is commenced. The helicopter yaws to the right just prior to touchdown,
what could the pilot do to help swing the nose to the left?
A. Increase the throttle
B. Decrease the throttle
C. Increase the collective pitch - ANSWER B. Decrease the throttle
3. If anti-torque failure occurred during cruising flight, what would be done to help
straighten out the left yellow prior to touch down?
A. A normal running landing should be made
B. Make a running landing using partial power and left cyclic
,C. Apply available throttle to help swing the nose to the right just prior to
touchdown - ANSWER C. Apply available throttle to help swing the nose to the
right just prior to touchdown
4. Should a helicopter pilot ever be concerned about ground resonance during
takeoff?
A. No; ground resonance occurs only during an autorotation touchdown
B. Yes; although it is more likely to occur on landing, it can occur during takeoff.
C. Yes; but only during slope takeoffs - ANSWER B. Yes; although it is more
likely to occur on landing, it can occur during takeoff.
5. An excessively steep approach angle and abnormally slow closure rates should
be avoided during an approach to a hover, primarily because
A. The airspeed indicator would be unreliable
B. A go around would be very difficult to accomplish
C. Settling with power could develop, particularly during the termination -
ANSWER C. Settling with power could develop, particularly during the
termination
6. During a near vertical power approach into a confined area with the airspeed
near zero, what hazardous condition may develop?
A. Ground resonance
B. Settling with power
C. Blade stall vibration - ANSWER B. Settling with power
,7. Which procedure will result in recovery from settling with power?
A. Increase collective pitch and power
B. In tank testing collective pitch and increase throttle
C. Increase forward speed and reduce collective pitch - ANSWER C. Increase
forward speed and reduce collective pitch
8. In addition of power and settling with power situation produces an
A. Increase in airspeed
B. Even greater rate of descent
C. Increase the cyclic control effectiveness - ANSWER B. Even greater rate of
descent
9. Under which situation is accidental settling with power likely to occur?
A. A steep approach in which the airspeed is permitted to drop to nearly 0
B. It shall approach in which the airspeed is permitted to drop below 10 mph
C. Covering in ground effect during calm wind, high density altitude conditions -
ANSWER A. A steep approach in which the airspeed is permitted to drop to
nearly 0
10. To recover from settling with power condition, the pilot should
A. Apply forward cyclic and simultaneously reduce collective, if of Altitude permits
B. Not apply into dark metal during the recovery
C. Increase rotor rpm, reduce forward airspeed, and minimize maneuvering -
ANSWER A. Apply forward cyclic and simultaneously reduce collective, if of
Altitude permits
, 11. When operating at high forward speed, retreating blade stall is more likely to
occur under conditions of
A. Low gross weight, high density altitude, and smooth air
B. High gross weight, low density altitude, and smoother
C. high gross weight, high density altitude, in turbulent air - ANSWER C. high
gross weight, high density altitude, in turbulent air
12. What are the major indications of a incipient retreating blade stall situation, in
order of occurrence?
A. Low-frequency vibration, Pitch up of the nose, and a role in the direction of the
retreating blade
B. Slow pitch up of the nose, high-frequency vibration, and a tendency for the
helicopter to roll
C. Slow pitch up of the nose, tendency for the helicopter to roll, followed by a
medium frequency vibration - ANSWER A. Low-frequency vibration, Pitch up
of the nose, and a role in the direction of the retreating blade
13. How should a pilot react on the onset of retreating blade stall?
A. Reduce collective pitch, rotor rpm, and forward airspeed
B. Reduce collective pitch, increase rotor rpm, and reduce forward airspeed
C. Increase collective pitch, reduce rotor rpm, and reduce forward airspeed -
ANSWER B. Reduce collective pitch, increase rotor rpm, and reduce forward
airspeed
14. The most power will be required to hover over which surface?
