FREE LIBRARY MEDIA AND STUDY GAMES ABOUT STUFF3

PDF Download

FREE LIBRARY MEDIA AND STUDY GAMES ABOUT STUFF3

EXAM QUESTIONS

Actual Qs and Ans Expert-Verified Explanation

This Exam contains:

-Guarantee passing score -59 Questions and Answers -format set of multiple-choice -Expert-Verified Explanation Question 1: In what flight condition must an airplane be placed in order to spin?

Answer:

Stalled Question 2: Loading an airplane to the most aft CG will cause the airplane to be:

Answer:

less stable at all speeds.Question 3: Which action will result in an airplane exceeding its critical angle of attack?

Answer:

Demanding more Gs than the wing can provide at a given airspeed.Question 4: As altitude increases, the indicated airspeed at which an airplane stalls in the same

configuation will:

Answer:

remain the same

Question 5: What important airspeed limitation is not color coded on the airspeed indicator?

Answer:

Maneuvering speed.Question 6: Wingtip vortices created by aircraft tend to:

Answer:

sink below the aircraft generating turbulence.Question 7: If severe turbulence is encountered, the aircraft's airspeed should be reduced

below:

Answer:

Maneuvering speed.Question 8: With the flaps in the cruise position, what is the positive load factor limit for the DA20?

Answer:

+4.4

Question 9: How does the wake turbulence vortex circulate around each wingtip?

Answer:

Outward, upward, and around each tip.Question 10: What is the relationship of lift, drag, thrust and weight when the airplane is in straight and level, unaccelerated flight?

Answer:

Lift equald weight and thrust equals drag.Question 11: Bank angles exceeding ___ degrees are prohibited by Doss procedures.

Answer:

60

Question 12: What must a pilot be aware of as a result of ground effect?

Answer:

Induced drag decreases; therefore, any excess speed at the point of flare may cause considerable floating.

Question 13: Which statement about adverse yaw is most correct?

Answer:

Adverse yaw can be seen during aileron deflection, when more lift on the rising wing results in more induced drag on that wing which pulls the nose toward the rising wing.

Question 14: What is the purpose of the rudder on an airplane?

Answer:

To control yaw.

Question 15: What describes "pitch"?

Answer:

Control of the airplane about the lateral axis by using the elevator to raise and lower the nose in relation to the natural horizon.

Question 16: What is ground effect?

Answer:

The result of the interference of the surface of the Earch with the airflow patterns about an airplane.

Question 17: What best describes "roll"?

Answer:

Control of the airplane about the longitudinal axis by use of the ailerons to attain a desired bank angle Question 18: The airplane is trimmed for straight-and-level unaccelerated flight. The control stick is momentarily pushed forward then released. The airplane enters a series of self-damping pitch oscillations and eventually returns to straight and level flight.

Answer:

Positive static and dynamic stability Question 19: In what flight condition is torque effect the greatest in a single-engine airplane?

Answer:

Low airspeed, high power, high angle of attack.

Question 20: Which V-speed represents maneuvering speed?

Answer:

Va

Question 21: With the flaps in the CRUISE position, what is the negative load factor limit for the DA20?

Answer:

-2.2 Question 22: The airplane will stall at higher indicated airspeed when excessive maneuvering loads are imposed by steep turns, pull-ups, or other abrupt changes in its flightpath; this is

called:

Answer:

Accelerated stall.Question 23: Lift produced by an airfoil is the net force developed perpendicular to the:

Answer:

relative wind.

Question 24: What force makes an airplane turn?

Answer:

The horizontal component of lift.Question 25: How does frost affect the lifting surfaces of an airplane on takeoff?

Answer:

Frost may prevent the airplane from becoming airborne at normal takeoff speed.

Question 26: Which would likely result in a slipping turn?

Answer:

Increasing the rate of turn without using rudder.

Question 27: What is the definition of Va?

Answer:

The design maneuvering speed.

Question 28: During a spin to the left, which wing is stalled?

Answer:

Both wings are stalled during a spin.