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Exam (elaborations)

AVIT 323 block 12- Dilse UPDATED Exam Questions and CORRECT Answers

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AVIT 323 block 12- Dilse UPDATED Exam Questions and CORRECT Answers Define adverse yaw - CORRECT ANSWER - The tendency of an airplane to yaw away from the direction of aileron roll input -aileron deflection causes it Define overbanking tendency - CORRECT ANSWER - When the top wing moves faster than the bottom wing causes a banking tendency

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Institution
AVIT 323
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AVIT 323

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Uploaded on
January 19, 2025
Number of pages
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Written in
2024/2025
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AVIT 323 block 12- Dilse UPDATED Exam
Questions and CORRECT Answers
Define adverse yaw - CORRECT ANSWER - The tendency of an airplane to yaw away
from the direction of aileron roll input
-aileron deflection causes it


Define overbanking tendency - CORRECT ANSWER - When the top wing moves faster
than the bottom wing causes a banking tendency


In a 60 degree bank turn, what happens to the aircraft - CORRECT ANSWER - -a 3000
pound aircraft will act like a 6000 pound aircraft
-2 G's will be pulled


Definition of load factor - CORRECT ANSWER - -the ratio between the lift and the
weight of an aircraft.
Load Factor = Lift / Weight (expressed in number of "Gs")


Definition of safety factor - CORRECT ANSWER - describes the structural capacity of a
system beyond the expected loads or actual loads
-Safety factor is the ultimate load factor


Definition of ultimate load factor - CORRECT ANSWER - -the Limit Load multiplied by
a prescribed Safety Factor of 1.5


Definition of limit load factor - CORRECT ANSWER - -the maximum load factor
authorized during flight


What affects the radius and rate of a turn - CORRECT ANSWER - Bank and Airspeed

, Static stability - CORRECT ANSWER - -INITIAL tendency to return to the equilibrium
condition following a disturbance


Types of static stability - CORRECT ANSWER - -Positive: when it goes back to trimmed
state
-Neutral: stays at the disturbance attitude
-Negative: changes to a more dramatic attitude once disturbed


Dynamic stability - CORRECT ANSWER - -TIME HISTORY of an aircrafts response to a
disturbance
-In order to have any type of dynamic stability, you must have positive static stability.


Longitudnal stabilty - CORRECT ANSWER - up/down
Pitch stability:
-ALONG the longitudinal
-AROUND the lateral axis


Forward CG - CORRECT ANSWER - -Poor performance
Greater distance between the elevator and the CG, making the TDF greater, therefore needing
more lift.
Greater lift required, more drag= slower AS


Aft CG - CORRECT ANSWER - -Better performance
Smaller distance between the elevator and the CG, making the TDF Less, therefore needing less
lift.
Less lift required, Less drag= greater AS


Directional stability - CORRECT ANSWER - Yawing left/right
Yaw stability:

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