CAX Written - Aerodynamics & Aircraft Exam Questions With 100% Correct Answers
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Course
Aerodynamics and Aircraft
Institution
Aerodynamics And Aircraft
CAX Written - Aerodynamics & Aircraft
Exam Questions With 100% Correct
Answers
Which is the symbol for the stalling speed or the minimum steady flight speed in a specified
configuration? - answerVS1
Which is the correct symbol fo the stalling speed or the minimum steady flight speed at which
...
CAX Written - Aerodynamics & Aircraft
Exam Questions With 100% Correct
Answers
Which is the symbol for the stalling speed or the minimum steady flight speed in a specified
configuration? - answer✔VS1
Which is the correct symbol fo the stalling speed or the minimum steady flight speed at which
the airplane is controllable? - answer✔VS
Vf - answer✔Design Flap Speed
Vle - answer✔Maximum Landing Gear Extended Speed
Vne - answer✔Never-Exceed Speed
Vy - answer✔Speed for best rate of Climb
If an airplane is listed as utility, it would mean that this airplane could be operated in which of
the following maneuvers? - answer✔Limited Acrobatics, including spins (if approved)
Which is true with respect to operating limitations of a 'restricted' category airplane? -
answer✔No person may operate a 'restricted' category airplane carrying passengers or property
for compensation for hire.
Which is true to operating limitations of a "primary" category airplane? - answer✔No person
may operate a "primary" category airplane carrying passengers or property for compensation for
hire.
The carriage of passengers for hire by a commercial pilot is - answer✔not authorized in a
"limited" category aircraft
No person may operate an aircraft that has an experimental airworthiness certificate -
answer✔when carrying persons or property for hire
The ratio between the total air load imposed on the wing and the gross weight of an aircraft in
flight is known as - answer✔load factor and directly affects stall speed
Load factor is the lift generated by the wings of an aircraft at any given time - answer✔divided
by the total weight of the aircraft
For a given angle of bank, in any airplane, the load factor imposed in a coordinated constant-
attitude turn - answer✔is constant and the stall speed increased
Airplane wing loading during a level coordinated turn in smooth air depends upon the -
answer✔angle of bank
in a rapid recovery from a dive, the effects of load factor would cause the stall speed to -
answer✔increase
If an aircraft with a gross weight of 2,000 pounds was subjected to a 60 deg constant-attitude
bank, the total load would be - answer✔4,000 pounds
While maintaining a constant angle of bank and altitude in a coordinated turn, an increase in
airspeed will - answer✔decrease the rate of turn resulting in no change in load factor
Lift on a wing is most properly defined as the - answer✔force acting perpendicular to the relative
wind
You are making a level turn as a constant bank angle. If you vary the rate of turn, the load factor
will - answer✔remain constant
The need to slow an aircraft below Va is brought about by the following weather phenomenon: -
answer✔Turbulence which causes an increase in stall speed
In theory, if the airspeed of an airplane is doubled while in level flight, parasite drag will become
- answer✔4x greater
As airspeed decreases in level flight below that speed for maximum lift/drag ration, total drag of
an airplane - answer✔increases because of increased induced drag
if the airspeed is increased from 90 knots to 135 knots during a level 60 deg banked turn, the
load factor will - answer✔remain the same but the radius of the turn will increase
Baggage weighing 90 pounds is placed in a normal category airplane's baggage compartment
which is placarded at 100 pounds. if this airplane is subjected to positive load factor of 3.5 G's,
the total load of the baggage would be - answer✔315 pounds and would not be excessive
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