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ASA 117 – Basic Celestial Endorsement Questions And Correct Answers (Verified Answers) Pl, Exams of Advanced Education

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ASA 117 – Basic Celestial Endorsement Questions And Correct Answers (Verified Answers) Pl, Exams of Advanced Education

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Uploaded on
December 24, 2025
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ASA 117 – Basic Celestial Endorsement Questions And Correct Answers
(Verified Answers) Pl, Exams of Advanced Education




The Acute angle A is the angle of?

1. incedence

2. attack

3. dihedral - ANSWER2. Attack



The term "angle of attack" is defined as

1. between the wing chord line and the relative wind

2. between the airplane's climb angle and the horizon

3. formed be the longitudinal axis of the airplane - ANSWER1. between the
wing chord line and the relative wind



The angle between the chord line of an airfoil and the relative wind is known
as the angle of

1. lift

2. attack

3. incidence - ANSWER2. Attack

, The term "angle of attack" is defined as the angle between the

1. chord line of the wing and the relative wind

2. airplanes longitudinal axis and that of the air striking the air foil

3. airplane's center line and the relative wind - ANSWER1. chord line of the
wing and the relative wind



The angle of attack at which an airfoil stalls will

1. Increase if the CG is moved forward

2. remain the same regardless of gross weight

3. change with an increase in gross weight - ANSWER2. remain the same
regardless of gross weight



What is the effect of advancing the throttle in flight?

1. Both aircraft groundspeed and angle of attack will increase

2. airspeed will remain relatively constant but the aircraft will climb

3. The aircraft will accelerate, which will cause a turn to the right - ANSWER2.
airspeed will remain relatively constant but the aircraft will climb



Which statement relates to Bernoulli's principle?

1. For every action there is an equal and opposite reaction.

2. An additional upward force is generated as the lower surface of the wing
deflects air downward.

3. Air traveling faster over the curved upper surface of an airfoil causes lower
pressure on top of the surface. - ANSWER3. Air traveling faster over the
curved upper surface of an airfoil causes lower pressure on top of the surface
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