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JEPPESEN COMMERCIAL EOC EXAM 2024/2025 WITH 100% ACCURATE SOLUTIONS
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JEPPESEN COMMERCIAL EOC EXAM 2024/2025 WITH 100% ACCURATE SOLUTIONS
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JEPPESEN COMMERCIAL EOC EXAM 2024/2025 WITH 100%ACCURATE SOLUTIONS
Frequent inspections should be made of aircraft exhaust manifold-type
heating systems to minimize the possibility of__________.
exhaust gases leaking into the cockpit
a power loss due to back pressure in the exhaust system
a cold-running engine due to the heat withdrawn by the heater - Precise
Answer ✔✔exhaust gases leaking into the cockpit
In small airplanes, normal recovery from spins may become difficult if
the__________.
CG is too far rearward, and rotation is around the longitudinal axis
CG is too far rearward, and rotation is around the CG
spin is entered before the stall is fully developed - Precise Answer
✔✔CG is too far rearward, and rotation is around the CG
,To maintain altitude during a turn, the angle of attack must be increased
to compensate for the decrease in the__________.
forces opposing the resultant component of drag
vertical component of lift
horizontal component of lift - Precise Answer ✔✔vertical component of
lift
Which is correct with respect to rate and radius of turn for an airplane
flown in a coordinated turn at a constant altitude?
For a specific angle of bank and airspeed, the rate and radius of turn will
not vary.
To maintain a steady rate of turn, the angle of bank must be increased as
the airspeed is decreased.
The faster the true airspeed, the faster the rate and larger the radius of
turn regardless of the angle of bank. - Precise Answer ✔✔For a specific
angle of bank and airspeed, the rate and radius of turn will not vary.
While maintaining a constant angle of bank and altitude in a coordinated
turn, an increase in airspeed will__________.
,decrease the rate of turn resulting in a decreased load factor
decrease the rate of turn resulting in no change in load factor
increase the rate of turn resulting in no change in load factor - Precise
Answer ✔✔decrease the rate of turn resulting in no change in load
factor
Select the correct statement regarding stall speeds.
Power-off stalls occur at higher airspeeds with the gear and flaps down.
In a 60°; the airplane stalls at a lower airspeed with the gear up.
Power-on stalls occur at lower airspeeds in shallower banks. - Precise
Answer ✔✔Power-on stalls occur at lower airspeeds in shallower banks.
What is the stall speed of an airplane under a load factor of 2 Gs if the
unaccelerated stall speed is 60 knots?
66 knots
74 knots
, 84 knots - Precise Answer ✔✔84 knots
The angle of attack of a wing directly controls the__________.
angle of incidence of the wing
amount of airflow above and below the wing
distribution of pressures acting on the wing - Precise Answer
✔✔distribution of pressures acting on the wing
The ratio between the total airload imposed on the wing and the gross
weight of an aircraft in flight is known as__________.
load factor and directly affects stall speed
aspect load and directly affects stall speed
load factor and has no relation with stall speed - Precise Answer
✔✔load factor and directly affects stall speed
The reason for variations in geometric pitch (twisting) along a propeller
blade is that it__________.
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