ATPL - AGK SET 3 (92/137) Exam
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Solutions | Latest Updated 2026
125. Which maximum range C. Airspeed.
factor decreases as weight
decreases? A. Angle of attack.
B. Altitude. C. Airspeed.
126. Which procedure A. Increase speed for a headwind.
produces the minimum fuel
consumption for a given leg of
the cruise flight? A. Increase
speed for a headwind. B.
Increase speed for a tailwind.
C. Increase altitude for a
headwind, decrease altitude
for a tailwind.
127. At what speed, with C. A speed greater than that for
reference to L/DMAX, does L/DMAX.
maximum range for a jet
airplane occur? A. A speed less
than that for L/DMAX. B. A
speed equal to that for
L/DMAX. C. A speed greater
than that for L/DMAX.
128. Maximum range B. Increasing altitude or decreasing
performance of a turbojet speed.
aircraft is obtained by which
, procedure as aircraft weight
reduces? A. Increasing speed
or altitude. B. Increasing
altitude or decreasing speed.
C. Increasing speed or
decreasing altitude.
129. What is the reason for A. It permits a relatively constant
variations in geometric pitch angle of attack along its length
along a propeller or rotor when in cruising flight.
blade? A. It permits a
relatively constant angle of
attack along its length when in
cruising flight. B. It prevents
the portion of the blade near
the hub or root from stalling
during cruising flight. C. It
permits a relatively constant
angle of incidence along its
length when in cruising flight.
130. Under normal operating A. High RPM and low MAP.
conditions, which combination
of MAP and RPM produce the
most severe wear, fatigue, and
damage to high performance
reciprocating engines? A. High
RPM and low MAP. B. Low RPM
and high MAP. C. High RPM
and high MAP.
131. What effect does high B. Reciprocating engines will
relative humidity have upon experience a significant loss of BHP.
the maximum power output of
Questions and Answers with Verified
Solutions | Latest Updated 2026
125. Which maximum range C. Airspeed.
factor decreases as weight
decreases? A. Angle of attack.
B. Altitude. C. Airspeed.
126. Which procedure A. Increase speed for a headwind.
produces the minimum fuel
consumption for a given leg of
the cruise flight? A. Increase
speed for a headwind. B.
Increase speed for a tailwind.
C. Increase altitude for a
headwind, decrease altitude
for a tailwind.
127. At what speed, with C. A speed greater than that for
reference to L/DMAX, does L/DMAX.
maximum range for a jet
airplane occur? A. A speed less
than that for L/DMAX. B. A
speed equal to that for
L/DMAX. C. A speed greater
than that for L/DMAX.
128. Maximum range B. Increasing altitude or decreasing
performance of a turbojet speed.
aircraft is obtained by which
, procedure as aircraft weight
reduces? A. Increasing speed
or altitude. B. Increasing
altitude or decreasing speed.
C. Increasing speed or
decreasing altitude.
129. What is the reason for A. It permits a relatively constant
variations in geometric pitch angle of attack along its length
along a propeller or rotor when in cruising flight.
blade? A. It permits a
relatively constant angle of
attack along its length when in
cruising flight. B. It prevents
the portion of the blade near
the hub or root from stalling
during cruising flight. C. It
permits a relatively constant
angle of incidence along its
length when in cruising flight.
130. Under normal operating A. High RPM and low MAP.
conditions, which combination
of MAP and RPM produce the
most severe wear, fatigue, and
damage to high performance
reciprocating engines? A. High
RPM and low MAP. B. Low RPM
and high MAP. C. High RPM
and high MAP.
131. What effect does high B. Reciprocating engines will
relative humidity have upon experience a significant loss of BHP.
the maximum power output of
