ATPL - Flight Performance and Planning
Exam Questions and Answers with
Verified Solutions | Latest Updated 2026
What affects indicated stall A. Weight, load factor, and power
speed? A. Weight, load factor,
and power B. Load factor,
angle of attack, and power C.
Angle of attack, weight, and
air density
What is load factor? A. Lift C. Lift divided by the total weight
multiplied by the total weight
B. Lift subtracted from the
total weight C. Lift divided by
the total weight
What is a characteristic of A. Pitch oscillations becoming
longitudinal instability? A. progressively greater
Pitch oscillations becoming
progressively greater B. Bank
oscillations becoming
progressively greater C.
Aircraft constantly tries to
pitch down
Maximum range performance B. Increasing altitude or decreasing
of a turbojet aircraft is speed
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
What effect does high relative B. Reciprocating engines will
humidity have upon the experience a significant loss of BHP
maximum 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
What effect would a change in C. As temperature increases, thrust
ambient temperature or air decreases
density have on
gas-turbine-engine
performance? A. As air density
decreases, thrust increases B.
As temperature increases,
thrust increases C. As
temperature increases, thrust
decreases
What effect, if any, does high A. Thrust will be reduced due to the
ambient temperature have decrease in air density
upon the thrust output of a
turbine engine? A. Thrust will
be reduced due to the
Exam Questions and Answers with
Verified Solutions | Latest Updated 2026
What affects indicated stall A. Weight, load factor, and power
speed? A. Weight, load factor,
and power B. Load factor,
angle of attack, and power C.
Angle of attack, weight, and
air density
What is load factor? A. Lift C. Lift divided by the total weight
multiplied by the total weight
B. Lift subtracted from the
total weight C. Lift divided by
the total weight
What is a characteristic of A. Pitch oscillations becoming
longitudinal instability? A. progressively greater
Pitch oscillations becoming
progressively greater B. Bank
oscillations becoming
progressively greater C.
Aircraft constantly tries to
pitch down
Maximum range performance B. Increasing altitude or decreasing
of a turbojet aircraft is speed
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
What effect does high relative B. Reciprocating engines will
humidity have upon the experience a significant loss of BHP
maximum 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
What effect would a change in C. As temperature increases, thrust
ambient temperature or air decreases
density have on
gas-turbine-engine
performance? A. As air density
decreases, thrust increases B.
As temperature increases,
thrust increases C. As
temperature increases, thrust
decreases
What effect, if any, does high A. Thrust will be reduced due to the
ambient temperature have decrease in air density
upon the thrust output of a
turbine engine? A. Thrust will
be reduced due to the
