DGCA Performance: Take-Off Questions

237 exam-style Take-Off questions for the DGCA Performancepaper (CPL & ATPL). The first 12 are free below with answers and explanations — sign up free to practise all of them with progress tracking.

  1. Q1

    How is wind considered in the take-off performance data of the Aeroplane Operations Manuals?

    • AUnfactored headwind and tailwind components are used.
    • BNot more than 80% headwind and not less than 125% tailwind.
    • CSince take-offs with tailwind are not permitted, only headwinds are considered
    • DNot more than 50% of a headwind and not less than 150% of the tailwind.
    Show answer

    Correct answer: D. Not more than 50% of a headwind and not less than 150% of the tailwind.

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  2. Q2

    What will be the influence on the aeroplane performance if aerodrome pressure altitude is increased?

    • AIt will increase the take-off distance.
    • BIt will decrease the take-off distance.
    • CIt will increase the take-off distance available.
    • DIt will increase the accelerate stop distance available.
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    Correct answer: A. It will increase the take-off distance.

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  3. Q3

    The affect of a contaminated runway on the field limit mass :

    • ADecreased weight, increased V1, increased VR
    • BDecreased weight, same V1, increased VR.
    • CDecreased weight, same V1, same VR.
    • DDecreased weight, decreased V1, decreased VR.
    Show answer

    Correct answer: D. Decreased weight, decreased V1, decreased VR.

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  4. Q4

    How does the thrust from a fixed propeller change during the take-off run of an aircraft?

    • AIt remains constant.
    • BIt increases slightly as the aircraft speed builds up.
    • CIt decreases slightly as the aircraft speed builds up.
    • DIt only varies with changes in mass.
    Show answer

    Correct answer: C. It decreases slightly as the aircraft speed builds up.

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  5. Q5

    The required Take-off Distance (TOD) and the field length limited Take-off Mass (TOM) are different for the zero flap case and take-off position flap case. What is the result of flap setting in take-off position compared to zero flap position?

    • AIncreased TOD required and decreased field length limited TOM.
    • BIncreased TOD required and increased field length limited TOM.
    • CDecreased TOD required and decreased field length limited TOM.
    • DDecreased TOD required and increased field length limited TOM.
    Show answer

    Correct answer: D. Decreased TOD required and increased field length limited TOM.

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  6. Q6

    When operating with anti-skid inoperative:

    • ABoth landing and take off performance will be affected.
    • BOnly landing performance will be affected.
    • COnly take off performance will be affected.
    • DNeither take off or landing performance will be affected.
    Show answer

    Correct answer: A. Both landing and take off performance will be affected.

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  7. Q7

    The take-off run is defined as:

    • Adistance to V1 and then to stop, assuing the engine failure is recognised at V1
    • Bdistance from brake release to the point where the aircraft reaches V2
    • Cthe horizontal distance from the start of the take-off roll to a point equidistant between VLOF and 35 ft
    • Dthe distance to 35 ft with an engine failure at V1 or 1.15 times the all engine distance to 35 ft.
    Show answer

    Correct answer: C. the horizontal distance from the start of the take-off roll to a point equidistant between VLOF and 35 ft

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  8. Q8

    The take-off distance available is:

    • Athe total runway length, without clearway even if this one exists.
    • Bthe length of the take-off run available plus the length of the clearway available.
    • Cthe runway length minus stopway.
    • Dthe runway length plus half of the clearway.
    Show answer

    Correct answer: B. the length of the take-off run available plus the length of the clearway available.

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  9. Q9

    What effect does a downhill slope have on the take-off speeds?

    • AIt has no effect on V1
    • BIt decreases V1
    • CIt increases V1
    • DIt increases the IAS for take-off
    Show answer

    Correct answer: B. It decreases V1

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  10. Q10

    During take-off, the thrust of a fixed pitch propeller:

    • Aincreases slightly while the aeroplane speed builds up
    • Bvaries with mass changes only.
    • Chas no change during take-off and climb.
    • Ddecreases while the aeroplane speed builds up.
    Show answer

    Correct answer: D. decreases while the aeroplane speed builds up.

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  11. Q11

    What will be the effect on an aeroplane’s performance if aerodrome pressure altitude is decreased?

    • AIt will increase the take-off distance required
    • BIt will increase the take-off ground run.
    • CIt will decrease the take-off distance required.
    • DIt will increase the accelerate stop distance.
    Show answer

    Correct answer: C. It will decrease the take-off distance required.

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  12. Q12

    The take-off distance of an aircraft is 800m in a standard atmosphere with no wind and at 0 ft pressure altitude. Using the following corrections: ± 20 m / 1 000 ft field elevation - 5 m / kt headwind + 10 m / kt tail wind ± 15 m / % runway slope ± 5 m / °C deviation from standard temperature The take-off distance from an airport at 2 000 ft elevation, temperature 21°C, QNH 1013.25 hPa, 2% up-slope, 5 kt tail wind is:

    • A810 m
    • B970 m
    • C890 m
    • D870 m
    Show answer

    Correct answer: B. 970 m

    This Explanation is Coming Soon

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