OPS DISPATCH EXAM 2025/2026 EXAM
QUESTIONS AND ANSWERS | 100%
PASS
As aircraft weight decreases with fuel burn, to maintain long range cruise,
the pilot must
a) increase thrust and reduce airspeed
b) maintain thrust and increase airspeed
c) reduce thrust to maintain best L/D ratio
d) reduce thrust and reduce airspeed - 🧠 ANSWER ✔✔reduce thrust and
airspeed
In cruise, an airplane increases power to accelerate and increase speed.
What happens to the angle of attack if the aircraft maintains altitude?
a) angle of attack decreases
b) angle of attack increases
c) increase angle of attack until stable, and then decrease
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,d) no change - 🧠 ANSWER ✔✔a) angle of attack decreases
which of the following has the greatest impact on speed of sound?
a) pressure
b) temperature
c) airfoil shape
d) wind - 🧠 ANSWER ✔✔temperarture
what happens to the angle of attack when the aircraft is transitioning from
climb into a level cruising attitude?
a)it increases
b) it decreases
c) remains the same
d) goes to 0 - 🧠 ANSWER ✔✔it decreases
What is the angle of incidence?
a) the angle between the chord line of the wing and the relative airflow
b) the angle between the chord line of the wing and the lateral axis
c) the angle between the chord line of the wing and the longitudinal axis
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,d) the angle between the chord line of the wing and the thrust vector - 🧠
ANSWER ✔✔the angle between the chord line of the wing and the
longitudinal axis
which of the following can change the critical angle of attack?
a) weight of the aircraft
b) airfoil shape
c) load factor
d) airspeed - 🧠 ANSWER ✔✔airfoil shape
in turbulence, a vertical gust affects stall speed of an aircraft primarily due
to the change in
a) angle of attacks
b) center of gravity
c) boundary layer
d) airflow density - 🧠 ANSWER ✔✔angle of attacks
how would a higher pressure altitude affect the landing distance of an
aircraft?
a)increase landing distance
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619652435. TERMS OF USE. PRIVACY STATEMENT. ALL RIGHTS RESERVED 3
, b) reduces landing distance
c) has no effect - 🧠 ANSWER ✔✔increase landing distance
in regards to low level wind shear, which of the following is true?
a) increase in headwind or decrease in tailwind will result in decreased IAS
b) decrease in headwind or increase in tailwind will result in decreased IAS
c) decrease in headwind or increase in tailwind will result in increased IAS
d) none of the above - 🧠 ANSWER ✔✔decrease in headwind or increase in
tailwind will result in decreased IAS
how would wind shear affect climb?
a) sudden increase or decrease of airspeed
b) cause turbulence due to violent air movement
c) increase or decrease climb rate
d) all of the above - 🧠 ANSWER ✔✔all of the above
weight added to an aircraft will:
a) increase landing distance
b) decrease landing distance
COPYRIGHT©NINJANERD 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER:
619652435. TERMS OF USE. PRIVACY STATEMENT. ALL RIGHTS RESERVED 4
QUESTIONS AND ANSWERS | 100%
PASS
As aircraft weight decreases with fuel burn, to maintain long range cruise,
the pilot must
a) increase thrust and reduce airspeed
b) maintain thrust and increase airspeed
c) reduce thrust to maintain best L/D ratio
d) reduce thrust and reduce airspeed - 🧠 ANSWER ✔✔reduce thrust and
airspeed
In cruise, an airplane increases power to accelerate and increase speed.
What happens to the angle of attack if the aircraft maintains altitude?
a) angle of attack decreases
b) angle of attack increases
c) increase angle of attack until stable, and then decrease
COPYRIGHT©NINJANERD 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER:
619652435. TERMS OF USE. PRIVACY STATEMENT. ALL RIGHTS RESERVED 1
,d) no change - 🧠 ANSWER ✔✔a) angle of attack decreases
which of the following has the greatest impact on speed of sound?
a) pressure
b) temperature
c) airfoil shape
d) wind - 🧠 ANSWER ✔✔temperarture
what happens to the angle of attack when the aircraft is transitioning from
climb into a level cruising attitude?
a)it increases
b) it decreases
c) remains the same
d) goes to 0 - 🧠 ANSWER ✔✔it decreases
What is the angle of incidence?
a) the angle between the chord line of the wing and the relative airflow
b) the angle between the chord line of the wing and the lateral axis
c) the angle between the chord line of the wing and the longitudinal axis
COPYRIGHT©NINJANERD 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER:
619652435. TERMS OF USE. PRIVACY STATEMENT. ALL RIGHTS RESERVED 2
,d) the angle between the chord line of the wing and the thrust vector - 🧠
ANSWER ✔✔the angle between the chord line of the wing and the
longitudinal axis
which of the following can change the critical angle of attack?
a) weight of the aircraft
b) airfoil shape
c) load factor
d) airspeed - 🧠 ANSWER ✔✔airfoil shape
in turbulence, a vertical gust affects stall speed of an aircraft primarily due
to the change in
a) angle of attacks
b) center of gravity
c) boundary layer
d) airflow density - 🧠 ANSWER ✔✔angle of attacks
how would a higher pressure altitude affect the landing distance of an
aircraft?
a)increase landing distance
COPYRIGHT©NINJANERD 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER:
619652435. TERMS OF USE. PRIVACY STATEMENT. ALL RIGHTS RESERVED 3
, b) reduces landing distance
c) has no effect - 🧠 ANSWER ✔✔increase landing distance
in regards to low level wind shear, which of the following is true?
a) increase in headwind or decrease in tailwind will result in decreased IAS
b) decrease in headwind or increase in tailwind will result in decreased IAS
c) decrease in headwind or increase in tailwind will result in increased IAS
d) none of the above - 🧠 ANSWER ✔✔decrease in headwind or increase in
tailwind will result in decreased IAS
how would wind shear affect climb?
a) sudden increase or decrease of airspeed
b) cause turbulence due to violent air movement
c) increase or decrease climb rate
d) all of the above - 🧠 ANSWER ✔✔all of the above
weight added to an aircraft will:
a) increase landing distance
b) decrease landing distance
COPYRIGHT©NINJANERD 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER:
619652435. TERMS OF USE. PRIVACY STATEMENT. ALL RIGHTS RESERVED 4
