ATPL - AGK SET 3 Exam | Questions with 100%
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Terms in this set (45)
125. Which maximum range factor C. Airspeed.
decreases as weight decreases?
A. Angle of attack.
B. Altitude.
C. Airspeed.
126. Which procedure produces the A. Increase speed for a headwind.
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 reference to C. A speed greater than that for L/DMAX.
L/DMAX, does 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 performance of B. Increasing altitude or decreasing speed.
a turbojet 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 variations A. It permits a relatively constant angle of attack
in geometric pitch along a propeller along its length when in cruising flight.
or rotor 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 relative B. Reciprocating engines will experience a
humidity have upon the maximum significant loss of BHP.
power output of modern aircraft
engines?
A. Neither turbojet nor reciprocating
engines are affected.
B. Reciprocating engines will
experience a significant loss of BHP.
C. Turbojet engines will experience a
significant loss of thrust.
132. Where is the critical altitude of a A. The highest altitude at which a desired manifold
supercharged-reciprocating engine? pressure can be obtained.
A. The highest altitude at which a
desired manifold pressure can be
obtained.
B. Highest altitude where the mixture
can be leaned to best power ratio.
C. The altitude at which maximum
allowable BMEP can be obtained.
133. What is controlled by the waste B. Exhaust gas discharge.
gate of a turbocharged-
reciprocating engine?
A. Supercharger gear ratio.
B. Exhaust gas discharge.
C. Throttle opening.
Correct Answers | Verified | Latest Update 2026
Save
Terms in this set (45)
125. Which maximum range factor C. Airspeed.
decreases as weight decreases?
A. Angle of attack.
B. Altitude.
C. Airspeed.
126. Which procedure produces the A. Increase speed for a headwind.
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 reference to C. A speed greater than that for L/DMAX.
L/DMAX, does 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 performance of B. Increasing altitude or decreasing speed.
a turbojet 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 variations A. It permits a relatively constant angle of attack
in geometric pitch along a propeller along its length when in cruising flight.
or rotor 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 relative B. Reciprocating engines will experience a
humidity have upon the maximum significant loss of BHP.
power output of modern aircraft
engines?
A. Neither turbojet nor reciprocating
engines are affected.
B. Reciprocating engines will
experience a significant loss of BHP.
C. Turbojet engines will experience a
significant loss of thrust.
132. Where is the critical altitude of a A. The highest altitude at which a desired manifold
supercharged-reciprocating engine? pressure can be obtained.
A. The highest altitude at which a
desired manifold pressure can be
obtained.
B. Highest altitude where the mixture
can be leaned to best power ratio.
C. The altitude at which maximum
allowable BMEP can be obtained.
133. What is controlled by the waste B. Exhaust gas discharge.
gate of a turbocharged-
reciprocating engine?
A. Supercharger gear ratio.
B. Exhaust gas discharge.
C. Throttle opening.
