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.
- 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.
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Correct answer: D. Not more than 50% of a headwind and not less than 150% of the tailwind.
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- 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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- 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.
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Correct answer: D. Decreased weight, decreased V1, decreased VR.
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- 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.
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Correct answer: C. It decreases slightly as the aircraft speed builds up.
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- 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.
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Correct answer: D. Decreased TOD required and increased field length limited TOM.
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- 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.
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Correct answer: A. Both landing and take off performance will be affected.
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- 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.
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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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- 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.
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Correct answer: B. the length of the take-off run available plus the length of the clearway available.
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- 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
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Correct answer: B. It decreases V1
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- 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.
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Correct answer: D. decreases while the aeroplane speed builds up.
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- 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.
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Correct answer: C. It will decrease the take-off distance required.
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- 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
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Correct answer: B. 970 m
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