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FAA Written and Private Pilot Final Exam with all Correct & 100% Verified Answers |Latest Version |Already Graded A+

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FAA Written and Private Pilot Final Exam with all Correct & 100% Verified Answers |Latest Version |Already Graded A+

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FAA Written and Private Pilot Final Exam with all Correct
& 100% Verified Answers |Latest Version |Already
Graded A+

Who certifies and regulates pilots? ✔Correct Answer-Federal Aviation Administration

The four forces acting on an airplane in flight are ✔Correct Answer-Lift
Weight
Thrust
Drag

Which statement relates to Bernoulli's principle? ✔Correct Answer-Air traveling faster over
the curved upper surface of an airfoil causes lower pressure on the top surface

The two parts of the wing which maneuver the aircraft are the ✔Correct Answer-Flaps from
the wing root to the midpoint and the ailerons from the midpoint to the wingtip

When are the four forces that act on an airplane in equilibrium? ✔Correct Answer-During
unaccelerated flight

Select the four flight fundamentals involved in maneuvering an aircraft ✔Correct Answer-
Aircraft power, pitch, bank, and trim

The ______ controls movement about the pitch axis, the ______ controls the movement about
the roll axis, and the ______ controls the movement about the yaw axis. ✔Correct Answer-
Elevator
Aileron
Rudder

When executing an emergency approach to land in a single-engine airplane, it is important to
maintain a constant glide speed because variations in glide speed ✔Correct Answer-nullify all
attempts at accuracy in judgment of gliding distance and landing spot.

What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level
flight? ✔Correct Answer-Lift equals weight and thrust equals drag

Form drag is ✔Correct Answer-created by any structure which protrudes into the relative
wind (Wing strut or landing gear)

An airplane said to be inherently stable will ✔Correct Answer-require less effort to control

, What causes an airplane (except T-tail) to pitch nosedown when power is reduced and controls
aren't adjusted? ✔Correct Answer-The downwash on the elevators from the propeller
slipstream is reduced and elevator effectiveness is reduced

What is the purpose of the rudder on an airplane? ✔Correct Answer-To control yaw

Which basic flight maneuver increases the load factor on an airplane as compared to straight-
and-level flight? ✔Correct Answer-Turns

One of the main functions of flaps on a wing is to ✔Correct Answer-mitigate a stall by
increasing the camber of the wing

Moving the weight of an airplane to the most aft CG will cause the airplane to be ✔Correct
Answer-less stable at all speeds

During a spin to the left, which wing(s) is/are stalled? ✔Correct Answer-Both wings are stalled

The angle of attack at which an airplane wing stalls will ✔Correct Answer-remain the same
regardless of gross weight

Are the stall recovery procedures the same for all Airplanes? ✔Correct Answer-Yes, Max
power-Reduce angle of attack-Roll wings level

What is ground effect? ✔Correct Answer-The result of the interference of the surface of the
Earth with the airflow patterns about an airplane

Floating caused by the phenomenon of ground effect will be most realized during an approach
to land when at ✔Correct Answer-less than the length of the wingspan above the surface

The greatest wingtip vortices strength occurs when the generating aircraft is ✔Correct
Answer-heavy, clean, and slow

One purpose of having two spark plugs per cylinder and wires from both magnetos connected
to one of the spark plugs in all four cylinders is ✔Correct Answer-Redundancy

Wingtip vortices created by large aircraft tend to ✔Correct Answer-sink below the aircraft
generating turbulence

When landing behind a large aircraft, the pilot should avoid wake turbulence by staying
✔Correct Answer-above the large aircraft's final approach path and landing beyond the aircraft's
touchdown point

In what flight condition is torque effect the greatest in a single-engine airplane? ✔Correct
Answer-Low airspeed, high power, high angle attack

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