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Examen

ATPL QUESTIONS WITH CORRECT ANSWERS ONLY.

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Subido en
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Escrito en
2025/2026

ATPL QUESTIONS WITH CORRECT ANSWERS ONLY.

Institución
ATPL
Grado
ATPL










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Institución
ATPL
Grado
ATPL

Información del documento

Subido en
6 de diciembre de 2025
Número de páginas
21
Escrito en
2025/2026
Tipo
Examen
Contiene
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Wizzair Atpl Grade A+ Solutions Exam v v v v v




Approach categories on aircrafts are based upon? - CORRECT ANSWER✔✔A grouping of aircraft based on a
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speed of 1.3 times the stall speed in the landing configuration at maximum gross landing weight. An aircraft
v v v v v v v v v v v v v v v v v v




must fit in only one category. If it is necessary to maneuver at speeds in excess of the upper limit of a speed
v v v v v v v v v v v v v v v v v v v v v v v




range for a category, the minimums for the category for that speed must be used. For example, an aircraft
v v v v v v v v v v v v v v v v v v v




which falls in Category A, but is circling to land at a speed in excess of 91 knots, must use the approach
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Category B minimums when circling to land.
v v v v v v v




Aircraft Aaproach Category A? - CORRECT ANSWER✔✔<91 Max circling speed 90Kts
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Aircraft Category B? - CORRECT ANSWER✔✔91/120 Max circling speed 120Kts
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Aircraft Category C? - CORRECT ANSWER✔✔121/140 Max circling speed 140Kts
v v v v v v v v v




Aircraft Category D? - CORRECT ANSWER✔✔141/165 Max circling speed 165Kts
v v v v v v v v v

,Aircraft Category E? - CORRECT ANSWER✔✔>165
v v v v v




What is ETOPS? - CORRECT ANSWER✔✔Extended twin operations. An operator is granted permission to
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operate a twin engined aircraft type on flight in which the aircraft is more than 60 minutes away from a
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suitable alternative aerodrome in the event that the aircraft suffers an engine failure en route.
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Wha are the various ETOPS categories? - CORRECT ANSWER✔✔Normal extended twin operations (ETOPS)
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categories, vary between 60 and 180 Minutes.
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The first segment on a Takeoff? - CORRECT ANSWER✔✔First Segment: The Climb from 35 feet point until
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the landing gears are fully retracted. Conditions in this segment are:
v v v v v v v v v v v




- landing gear extended
v v v




- flaps in T/O position
v v v v




- Speed = V2
v v v




- Climb gradient for 2 engine A/C = Positive
v v v v v v v v




- Climb gradient for 4 engine A/C = 0.5%
v v v v v v v v




- Takeoff power
v v




The second segment on a Takeoff? - CORRECT ANSWER✔✔Second Segment: Climb from gear retraction
v v v v v v v v v v v v v




point until a height of 400 feet is reached. conditions in this segment are:
v v v v v v v v v v v v v v




- gears retracted
v v




- flaps in T/O position
v v v v




- speed = V2
v v v




- Climb gradient 2 engine a/c 2.4%, and 4 engine a/c 3.0%
v v v v v v v v v v v




- takeoff power
v v

, The third segment on a Takeoff? - CORRECT ANSWER✔✔Third Segment: Its the horizontal distance
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covered after the second segment until the flap retraction speed is reached, to raise the flaps plus the
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distance required to accelerate the aircraft to the flaps up climb speed. It consists of two parts:
v v v v v v v v v v v v v v v v v




First part of 3rd segment: Distance covered before flap retraction, accelerating to flap retraction speed. The
v v v v v v v v v v v v v v v




conditions are:
v v




- gears retracted
v v




- flaps in t/o position
v v v v




- speed increasing from v2 to flap retraction speed
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- Climb gradient 2 engine a/c 1.2%, 4 engine a/c 1.7%
v v v v v v v v v v




- takeoff power
v v




Second part of 3rd segment: Distance covered after flap retraction, accelerating to final t/o climb speed. the
v v v v v v v v v v v v v v v v




conditions are:
v v




- gears retracted
v v




- flaps retracted
v v




- speed, accelerating from flaps retraction to final t/o climb speed
v v v v v v v v v v




- Climb gradient 2 engine a/c 1.2%, 4 engine a/c 1.7%
v v v v v v v v v v




- maximum continuous power
v v v




The fourth segment on a Takeoff? - CORRECT ANSWER✔✔Fourth Segment: the Climb from 400 feet till
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1500 feet is reached, after the end of third segment operating with max continuous power. The conditions
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are:
v




- gears retracted
v v




- flaps retracted
v v




- speed = final t/o climb speed
v v v v v v




- max continous power
v v v




- Climb gradient 2 engine a/c 1.2%, 4 engine a/c 1.7%
v v v v v v v v v v
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