TAKEOFF – Air – DGCA Question Bank For Politics

#1. Flight planning has been completed for a take-off using 10 degree flap deflection. The climb limited TOM is 4550 Kg, and the Field length limited TOM is 5650 Kg. If the aircraft is loaded to a mass of 5000 Kg, which of the following statements is correct?

15 degree flap deflection will increase both limits.

15 degree flap deflection will increase climb limit and decrease field length limit.

5 degree flap deflection will decrease both limits.

5 degree flap deflection will increase climb limit and decrease field length limit.

#2. The end of the first segment is?

At 400 feet gross height.

At flap retraction altitude.

At gear up altitude.

Above the obstacle dcmain at flap retraction height.

#3. Take-off performance is best with?

Low altitude, low temperature, low humidity.

High altitude, high temperature, high humidity.

Low altitude, low temperature, high humidity.

High altitude, low temperature, low humidity.

#4. Why does the take-off climb chart (table 4.5) in the CAP 698 not take account of headwinds and tailwinds?

Because it is already factorised into the calculations.

Because headwinds and tailwinds do not affect climb gradient.

Because headwinds and tailwinds do not affect ROC.

#5. To what speed is VMBE referenced?

V2 for air speed.

VLOF For ground speed.

V1 for ground speed.

VR for ground speed.

#6. To what speed is the limiting tyre speed referenced ?

VLOF for ground speed.

V2 for air speed.

VAT for ground speeds.

V1 for ground speeds.

#7. A contaminated runway will?

lncrease TORR and decrease TODR.

lncrease TODR more than TORR.

lncrease TORR more than TODR.

lncrease TORR but not affect TODR.

#8. lncreasing ambient pressure?

lncrease take-off run and decrease climb gradient.

lncrease take-off run and climb gradient.

Decrease take-off run and climb gradient.

Decrease take-off run and increase climb gradient.

#9. lncreasing pressure altitude will?

lncrease take-off run and climb gradient.

lncrease take-off run and decrease climb gradient.

Decrease take-off run and climb gradient.

Decrease take-off run and increase climb gradient.

#10. If TOM is field limited?

VMBE is too high.

Mass equals field limited mass but is greater than climb limited mass.

Mass equals climb limited mass.

Mass equals field limited mass.

#11. If an engine fails after V1?

Continue or abort depending on which engine has failed.

Continue or abort depending on mass.

Abort.

Continue.

#12. Take-off performance calculations have been made based on on field limited mass at 30° flap angle. If 25° is inadvertently set?

The calculated V, will be too low.

The aircraft will overrun the stopway if take-off is abandoned at V1.

VR will be found to be too low.

V2 will be found to be too high.

#13. A field is said to be balanced when?

EMDA = TODA.

TODA= TORA.

EMDA=TORA.

EMDA = 1.33 TODA

#14. The take-off distance is?

From BRP to screen height.

From BRP to end of clearway.

From BRP to end of stopway.

From BRP to 400 feet height.

#15. Increasing upward runway slope will?

lncrease TORR and TODR.

lncrease TORR and TODA.

Decrease TORR and TODR.

Increases TODR and EMDA.

#16. Increasing flap angle from 10° to 20° will?

Decrease V2 and VLoF.

lncrease V2 and VLoF.

Increase V2 and decrease VLoF.

Decrease V2 and increase VLoF.

#17. Decreasing flap angle from 15° to 5° will?

Decrease V2 and VLoF.

Increase V2 and VLoF.

lncrease V2 and decrease VLoF.

Decrease V2 and increase VLoF.

#18. Increasing flap angle beyond the normal take-off setting will?

Decrease VLoF and TODR.

lncrease VLoF and TODR.

Decrease VLoF and increase TODR.

lncrease VLoF and decrease TODR.

#19. A headwind will ........TORR and ..........TODR?

Increase Increase.

Increase Decrease.

Decrease Decrease.

Decrease Increase.

#20. A headwind will.. ...... V2 and .......... VLOF?

increase Not affect.

Not affect Decrease.

Decrease Decrease.

Not affect Not affect.

#21. A tailwind will ........TORR and .......... TODR?

Increase Increase.

Not affect Decrease.

Decrease Decrease.

Not affect Not affect.

#22. A tailwind will.. ...... V2 and ....... VLoF?

Increase Not affect.

Not affect Decrease.

Decrease Decrease.

Not affect Not affect.

#23. For take-off from a contaminated runway it is necessary to?

lncrease VR and V2 by a safety factor of 1.3.

Increase VR and V2 by a safety factor of 1 .I.

Use the standard VR and V2.

Increase V1, VR and V2.

#24. The value of VR depends upon?

Mass, air density, and flap angle.

Mass, air temperature, and runway slope.

C of G position, mass, and runway slope.

Runway condition, runway slope and aircraft mass.

#25. The value of VR depends upon?

Mass, air density, and runway condition.

Mass, air temperature, and flap angle.

C of G position, mass, and runway slope.

Runway condition, runway slope and aircraft mass.

#26. Flight planning has been completed for a take-off using 10 degree flap deflection. The climb limited TOM is 4500 Kg, and the Field length limited TOM is 5000 Kg. If the aircraft is loaded to a mass of 5000 Kg, which of the following statements is correct?

Using 5 degrees of flap might increase the climb limited mass sufficiently to enable take-off to be made at the new mass.

Using 20 degrees of flap might increase the climb limited mass sufficiently to enable take-off to be made at the new mass.

Using 5 degrees of flap will increase the climb limited mass but will decrease the field length limited mass.

Using 20 degrees of flap will increase the climb limited mass but will decrease the field length limited mass.

#27. Flight planning has been completed for a take-off using 10 degree flap deflection. The climb limited TOM is 5000 Kg, and the Field length limited TOM is 4500 Kg. If the aircraft is loaded to a mass of 5000 Kg, which of the following statements is correct?

Using 5 degrees of flap might increase the climb limited mass sufficiently to enable take-off to be made at the new mass.

Using 20 degrees of flap might increase the climb limited mass sufficiently to enable take-off to be made at the new mass.

Using 5 degrees of flap will decrease the climb limited mass but will increase the field length limited mass.

Using 20 degrees of flap will decrease the climb limited mass but will increase the field length limited mass.

#28. Flight planning has been completed for an early morning take-off using 10 degree flap at a mass of 4300 Kg. The climb limited TOM is 5000 Kg, the Field length limited TOM is 4500 Kg. The take-off is then delayed due to traffic problems. Which of the following statements is correct?

Take-off perfqrmance will be degraded if OAT increases.

Take-off performance will be improved if OAT increases.

Take-off performance will be unaffected by changes in OAT.

Decreases in take-off performance due to increasing OAT can be overcome by reducing flap deflection.

#29. Operating from a slush contaminated runway will require ........ compared to operating from the same runway in dry conditions?

Unchanged V1, increased VR decreased weight.

Decreased V1, decreased VR decreased weight.

Increased V1, increased VR unchanged weight.

Decreased V1, unchanged VR decreased weight.

#30. An MRJT aircraft at mass 52000 Kg is to take-off from a runway contaminated with 6 mm of standing water. Take-off performance calculations indicate a dry runway field limited take-off mass of 52000 Kg. The effect of the contamination will be to?

lncrease V1 and VR but not affect mass.

Decrease V1 mass, and VR.

lncrease V1 and decrease VR and mass.

Decrease V1 but not affect VR or mass.

#31. A defective anti-skid system will?

Reduce take-off performance.

Reduce landing performance.

Reduce both take-of and landing performance.

Not affect take-off nor landing performance.

#32. An aircraft is cleared for take-off using either 5, 10, or 15 degrees of flap, the normal setting being 10 degrees. Take-off using the 5 degree setting might be appropriate for?

Long runway, low pressure altitude and close obstacles.

Long runway, high pressure altitude and close obstacles.

Short runway, low pressure altitude and distant obstacles.

Short runway, high pressure altitude and distant obstacles

#33. An aircraft is cleared for take-off using either 5, 10, or 15 degrees of flap, the normal setting being 10 degrees. Use of the 15 degree setting will . . ... compared to the standard setting?

Decrease take-off run, TODR and obstacle clearance.

lncrease take-off run, TODR and obstacle.clearance.

lncrease take-off run and decrease TODR and obstacle clearance.

Decrease take-off run and increase TODR and obstacle clearance.

#34. If atmospheric pressure increases whilst other factors remain unchanged, take-off distance required will ...... and climb performance will ...... ?

Increase increase.

Increase decrease.

Decrease decrease.

Decrease increase.

#35. Decreased ambient temperature causes?

Decreased VMBE masslimit.

Increased climb limited mass limit.

Decreased field length limited mass limit.

Decreased climb limited mass limit.

#36. Increasing flap setting from 5 degrees to 15 degrees will?

IncreaseV2

Decrease V2.

lncrease V2 if not limited by VMBE.

Decrease V2 if not limited by VMCA.

#37. When taking-off in high temperatures or at high pressure altitudes?

Tyre speeds become more limiting.

Tyre speeds become less limiting.

Tyre speeds are not affected.

Tyre speeds may become more or less limiting depending on runway condition.

#38. The 2 second time interval between VEF and V1 is?

Not required for jet engines.

To allow the propeller to automatically feather.

To allow the engine to run down so that no thrust is produced.

To allow for the failure to be detected.

#39. From commencement of the take-off run to screen height is?

Gross TODR.

Net TODR.

Gross TOR.

Measured TOD.

#40. What is TORR?

The distance between the BRP and the lift off point.

The calculated distance between BRP and the point at which VLOF is achieved.

The distance between BRP and the point at which screen height IS achieved.

The calculated distance between BRP and the point at which screen weight is achieved.

#41. What is the TODR?

The distance between the BRP and the lift off point.

The calculated distance between BRP and the point at which VLOF is achieved.

The distance between BRP and the point at which screen height is achieved.

The calculated distance between BRP and the point at which screen weight is achieved.

#42. The minimum acceptable value for V2 is?

1.1 VMC.

1.1 Vs for 4 engine turbo-props and jets with provision for significant reduction in one-engineinoperative stalling speed.

1.25 Vs for 2 and 3 engine turbo-props and jets without provision for significant reduction in oneengine- inoperative stalling speeds.

VMCG.

#43. The minimum acceptable value for V2 is?

1.15VMc.

1.2 Vs for 4 engine turbo-props and jets with provision for significant reduction in one-engineinoperative stalling speed.

1.25 Vs for 2 and 3 engine turbo-props and jets without provision for significant reduction in oneengine- inoperative stalling speeds.

VMCG

#44. The minimum acceptable value for V2 is?

1.15 VMC.

1.1'5 Vs for 4 engine turbo-props and jets with provision for significant reduction in one-engineinoperative stalling speed.

1 .I5 Vs for 2 and 3 engine turbo-props and jets without provision for significant reduction in oneengine- inoperative stalling speeds.

VMCG

#45. The minimum value of VR is?

V1.

105% VMC.

The speed required to attain V2 by the end of the clearway.

VMCG.

#46. The minimum value of VR is?

1.1 V1.

115% VMC.

The speed required to attain V, by screen height.

VMCG.

#47. ATC require a class A aircraft to conduct a 20° banked turn as soon as possible after lift-off. What is the minimum allowable height for the commencement of this turn and by what margin must the aircraft clear obstacles during the turn?

35 ft 35 ft.

50 ft 50 ft.

400 ft 35 ft.

400ft 50 ft.

#48. When taking-off from a contaminated runway?

Rotate at the normal VR.

lncrease VR by 10%.

lncrease VR by 10 Kts.

Decrease VR by 10% or 10 Kts, whichever is greater.

#49. An error is made carrying out the take-off performance calculations, resulting in the calculated V1 figure of 160 Kts, being 10 kts too high. Which of the following statements is true?

If an engine fails at 155 Kts and the take-off is abandoned the aircraft will overrun.

If an engine fails at 155 Kts and the take-off is continued the aircraft will not achieve screen height.

If an engine fails at 150 kts and the take-off is abandoned the aircraft will overrun.

Engine failures at any speed up to the calculated V, can be dealt with safely by continuing the ta ke-off

#50. The minimum value of VR is?

V1.

110% VMC.

The speed required to attain V, the end of the TORA.

VMCG.

#51. An error is made carrying out the take-off performance calculations, resulting in the calculated figure of 140 Kts, being 10 kts too low. Which of the following statements is true?

If an engine fails at 145 Kts and the take-off is abandoned the aircraft will overrun.

If an engine fails at 155 Kts and the take-off is continued the aircraft will not achieve screen height.

If an engine fails at 150 kts and the take-off is abandoned the aircraft will overrun.

Engine failures at any speed up to the calculated V, can be dealt with safely by abandoning the take-off.

#52. An error is made carrying out the take-off performance calculations, resulting in the calculated figure of 160 Kts, being 10 kts too high Which of the following statements is true?

If an engine fails at 145 Kts and the take-off is abandoned the aircraft will overrun.

If an engine fails at 155 Kts and the take-off is continued the aircraft will not achieve screen height.

If an engine fails at 150 kts and the take-off is abandoned the aircraft will overrun.

Engine failures at any speed above the calculated V, can be dealt with safely by continuing the take-off.

#53. What proportion of a headwind should be taken into account when calculating take-off performance for a single engine propeller aircraft of 3000 Kg mass, when operating from a dry paved runway?

15%

50%

100%

150%

#54. What proportion of a tailwind should be taken into account when calculating take-off performance for a single engine propeller aircraft of 3000 Kg mass, when operating from a dry paved runway?

15%

100%

50%

150%

#55. An aerodrome has a runway of 4000 m and the first obstacle is 1500 meters from the end of the take-off run. What is the maximum take-off distance that may be assumed to be available.

4500 M.

5500 M.

5000 M.

6500 M.

#56. Defective anti-skid systems?

Decrease maximum landing mass.

Decrease field limited TOW.

Decrease both field limited TOW and maximum landing mass.

lncrease maximum TOW but decrease maximum landing mass.

#57. Defective anti-skid systems? 1. lncrease LDR. 2. lncrease TORA. 3. lncrease ASDR. 4. lncrease TORR.

1, 2 and 3.

2 and 4.

1 and 3.

1,2 and 4.

#58. TODR is?

The distance between BRP and achieving VLoF.

'The distance between BRP and achieving VMU.

The calculated distance between BRP and the achievement of screen height.

The calculated distance between BRP and the achievement of VLoF.

#59. TORR is?

The distance between BRP and achieving VLOF.

The distance between BRP and achieving VMU.

The calculated distance between BRP and screen height.

The calculated distance between BRP and the achievement of VLoF.

#60. Minimum acceptable obstacle clearance for class A aircraft in the obstacle domain is .... increasing to ...... in turns above 400 ft using bank angles of ..... ?

35ft 50ft 15° to 35°.

50ft 65ft 15° to 25°.

35ft 50ft 15° to 25°.

35ft 75ft 15° to 30°.

#61. Minimum acceptable all engines operating gradient for a twin piston aircraft at screen height in the takeoff is?

4%

2%

1.5%

3.5%

#62. A light piston twin climbs at a gradientof 10% from the screen height of 15m (50 ft). There is an obstacle 900 m high, 3280 m from the screen. By how much will the aircraft clear the obstacle?

100 m.

115 m.

85 m.

It does not clear the obstacle.

#63. During certification testing of a twin engine jet aircraft the true take-off distances were 1547 m with all engines operating, and 1720 m with the critical engine inoperative at V,. What distance would be used for certification purposes?

1547 m.

1720 m.

1978 m.

1779 m.

#64. If an aircraft takes-off using the wet V, instead of the dry V, how will TODR and climb performance be affected?

Increased improved.

Increased degraded.

Decreased degraded.

Decreased improved.

#65. Can take-off be carried out if V, is less than VMCG?

NO.

YES.

Only VMCG is decreased to equal V1.

Only if V1 is increased to equal VMCG.

#66. V2 is?

Take-off safety speed.

Fourth segment commencement speed.

The lowest speed at which control can be maintained following a single engine failure during takeoff.

The speed at which an aircraft lifts off the ground.

#67. Which of the following is true of the increased V2 procedure?

It increases the maximum TOW.

It decreases the maximum TOW.

It increases TODR and climb performance at any given TOW.

It can be used to increase climb performance only if the field length limited mass is less than the climb limited mass.

#68. Wind component at take-off does not affect?

Climb gradient.

Obstacle limited TOW.

Field length limited TOW.

Rate of climb.

#69. TODA is?

Declared runway length.

Declared runway plus stopway length.

Declared runway length plus clearway.

Declared runway plus stopway plus clearway.

#70. The first segment ends?

When the gear is fully retracted.

When the flaps are fully retracted.

At 1500 ft above runway level.

At 400 ft above runway level.

#71. Can a stopway be included in take-off run required (TORR) calculations?

NO.

YES.

Only if the clearway is longer than the stopway.

Only if the clearway is shorter than the stopway

#72. Reduced thrust take-off should not be used?

Temperature is more than ISA + 7ºC

When it is dark.

When the runway is wet.

When anti-skid system is unserviceable.

#73. Can anti skid systems be used for take-off and landing?

YES.

NO.

Take-off only.

Landing only.

#74. An increase in OAT will . . .. Field length limited TOW and . . ... climb limited TOW?

Increase increase.

Increase decrease.

Decrease decrease.

Decrease increase.

#75. What will happen to ASDA if anti-skid is Unserviceable?

Nothing.

Increase.

Decrease.

lncrease or decrease depending on slope.

#76. The distance to be maintained between aircraft is greatest when?

Taking-off heavy.

Landing heavy.

Taking-off light.

Landing light.

#77. Reduced thrust take-off should not be used?

Temperature is less than ISA.

When it is raining.

At night.

When the runway is icy or very slippery.

#78. Reduced thrust take-off should not be used?

Temperature is less than ISA.

When thrust reverse systems are unserviceable.

At night.

At pressure altitudes above 3500 ft amsl. .

#79. Variable thrust take-off procedures should not be used?

Temperature is greater than ISA.

When increased V2 procedure is being used.

At night..

At pressure altitudes above 5000 ft amsl.

#80. Assumed temperature take-off procedures should not be used?

Temperature is greater than ISA.

At night.

When the PMC is switched off or unserviceable.

At pressure altitudes above 10000 ft amsl.

#81. Assumed temperature take-off procedures should not be used?

On upward sloping runways.

At night.

When the runway is contaminated.

When the runway is wet.

#82. The maximum thrust reduction that may be used when conducting a reduced thrust take-off is?

10%.

20%.

25%.

30%.

#83. The assumed temperature take-off procedure can be used only when?

The runway is dry.

The available distance greatly exceeds that required.

The field length limited mass is too low.

The climb limited mass is too low.

#84. The purpose of the reduced thrust take-off procedure is to?

Conserve engine life.

Reduce TORR.

Reduce fuel consumption.

Reduce TODR.

#85. VMBE is most likely to be a limiting factor when?

There is a tailwind.

There is a headwind.

Pressure altitude is low.

Air temperature is low.

#86. VMBE is most likely to be a limiting factor when?

There is a wet runway.

There is a headwind.

Pressure altitude is high.

Air temperature is low.

#87. VMBE is most likely to be a limiting factor when?

There is a wet runway.

There is a headwind.

Pressure altitude is low.

Air temperature is high.

#88. Tyre speed is likely to be greatest when?

QFE is low.

QFE is high.

QNH is high.

OAT is low.

#89. During certification test flying of a one hundred and twenty seat, twin jet aircraft, the distance from BRP to VLOF is 1500 m with all engines operating, and 2000 m with one engine out. Which of the following figures is most likely to be the one used for TORR certification purposes?

1500 M.

1725 M.

2000 M.

2100 M.

#90. During certification test flying of a one hundred and twenty seat, twin jet aircraft, the distance from BRP to VLoF on a wet runway is 1500 m with all engines operating, and 2000 m with one engine out. Which of the following figures is most likely to be the one used for TORR certification purposes?

1500 M.

2000 M.

1700 M.

2500 M.

#91. During certification test flying of a one hundred and twenty seat, twin jet aircraft, the distance from BRP to Screen height from a dry runway is 1500 m with all engines operating, and 2000 m with one engine out. Which of the following figures is most likely to be the one used for TODR certification purposes?

1500 M.

1725 M.

2000 M.

3300 M.

#92. During certification test flying of a one hundred and twenty seat, twin jet aircraft, the distance from BRP to Screen height from a contaminated runway is 1500 m with all engines operating, and 2000 m with one engine out. Which of the following figures is most likely to be the one used for TODR certification purposes?

1500 M.

1725 M.

2000 M.

1850 M.

#93. If the mass of an aircraft was greater than that calculated, which of the following speeds would be found to be greater than expected during the take-off?

VLOF

VR.

V1.

V2.

#94. Which of the flowing conditions is best suited to the use of low flap angles?

High field elevation, high temperature, long runway, distant obstacles.

High field elevation, low temperature, short runway, no obstacles.

Low field elevation, high temperature, long runway, close obstacles.

Low field elevation, low temperature, short runway, no obstacles.

#95. A depth of 5 mm of standing water will ..... .. field length limited mass, compared with a dry runway?

Decrease.

Increase.

Not change.

Increase or decrease depending on aircraft type.

#96. What is the takeoff run required for a class B aircraft, with one engine inoperative?

Distance from BRP to VLOF.

Distance from BRP to V2.

Distance from BRP to rr~idp oint between Vr and 35 ft screen height.

Distance between BRP and mid point between VLoF and 35 ft screen height.

#97. What term is used for the distance from BRP to screen height?

Gross TODR.

Net TODR.

Gross TOD.

Measured TOD.

#98. What is the measured TOD?

BRP to screen height.

BRP to mid point between VLOF and screen height.

BRP to first obstacle.

VLoFto screen height.

#99. An aircraft is prepared for take-off from runway 09 which has a 1 % downward slope. The take-off mass is limited by VMBE. If the effects of winds are ignored, what will happen if operations are switched to runway 27, immediately before take-off?

Mass must be reduced or VMBE will be exceeded.

VMBE will be decreased so mass must be reduced.

VMBE will not change but mass need not be changed because it is known to be within limits.

Mass may be increased because VMBE has increased.

#100. During a take-off, where is the reference point zero located?

Where the aircraft reaches screen height.

Where the aircraft reaches V1.

Where the aircraft reaches VLOF.

Where the aircraft reaches V2.

#101. If conditions are such that equal VMCA what will happen to V2 if Rap angle is increased beyond the standard setting for take-off?

Decrease.

Remain unchanged.

Increase.

Decrease if not limited by VMCG.

#102. When taking -off from a runway with 5 mm of standing water, field limited mass will . . ... and V1 will . . .. Compared to a damp runway?

Increase increase.

Increase decrease.

Decrease decrease.

Decrease increase.

Dgca Question Bank For Pilots

Results

#1. Flight planning has been completed for a take-off using 10 degree flap deflection. The climb limited TOM is 4550 Kg, and the Field length limited TOM is 5650 Kg. If the aircraft is loaded to a mass of 5000 Kg, which of the following statements is correct?

#2. The end of the first segment is?

#3. Take-off performance is best with?

#4. Why does the take-off climb chart (table 4.5) in the CAP 698 not take account of headwinds and tailwinds?

#5. To what speed is VMBE referenced?

#6. To what speed is the limiting tyre speed referenced ?

#7. A contaminated runway will?

#8. lncreasing ambient pressure?

#9. lncreasing pressure altitude will?

#10. If TOM is field limited?

#11. If an engine fails after V1?

#12. Take-off performance calculations have been made based on on field limited mass at 30° flap angle. If 25° is inadvertently set?

#13. A field is said to be balanced when?

#14. The take-off distance is?

#15. Increasing upward runway slope will?

#16. Increasing flap angle from 10° to 20° will?

#17. Decreasing flap angle from 15° to 5° will?

#18. Increasing flap angle beyond the normal take-off setting will?

#19. A headwind will ........TORR and ..........TODR?

#20. A headwind will.. ...... V2 and .......... VLOF?

#21. A tailwind will ........TORR and .......... TODR?

#22. A tailwind will.. ...... V2 and ....... VLoF?

#23. For take-off from a contaminated runway it is necessary to?

#24. The value of VR depends upon?

#25. The value of VR depends upon?

#26. Flight planning has been completed for a take-off using 10 degree flap deflection. The climb limited TOM is 4500 Kg, and the Field length limited TOM is 5000 Kg. If the aircraft is loaded to a mass of 5000 Kg, which of the following statements is correct?

#27. Flight planning has been completed for a take-off using 10 degree flap deflection. The climb limited TOM is 5000 Kg, and the Field length limited TOM is 4500 Kg. If the aircraft is loaded to a mass of 5000 Kg, which of the following statements is correct?

#28. Flight planning has been completed for an early morning take-off using 10 degree flap at a mass of 4300 Kg. The climb limited TOM is 5000 Kg, the Field length limited TOM is 4500 Kg. The take-off is then delayed due to traffic problems. Which of the following statements is correct?

#29. Operating from a slush contaminated runway will require ........ compared to operating from the same runway in dry conditions?

#30. An MRJT aircraft at mass 52000 Kg is to take-off from a runway contaminated with 6 mm of standing water. Take-off performance calculations indicate a dry runway field limited take-off mass of 52000 Kg. The effect of the contamination will be to?

#31. A defective anti-skid system will?

#32. An aircraft is cleared for take-off using either 5, 10, or 15 degrees of flap, the normal setting being 10 degrees. Take-off using the 5 degree setting might be appropriate for?

#33. An aircraft is cleared for take-off using either 5, 10, or 15 degrees of flap, the normal setting being 10 degrees. Use of the 15 degree setting will . . ... compared to the standard setting?

#34. If atmospheric pressure increases whilst other factors remain unchanged, take-off distance required will ...... and climb performance will ...... ?

#35. Decreased ambient temperature causes?

#36. Increasing flap setting from 5 degrees to 15 degrees will?

#37. When taking-off in high temperatures or at high pressure altitudes?

#38. The 2 second time interval between VEF and V1 is?

#39. From commencement of the take-off run to screen height is?

#40. What is TORR?

#41. What is the TODR?

#42. The minimum acceptable value for V2 is?

#43. The minimum acceptable value for V2 is?

#44. The minimum acceptable value for V2 is?

#45. The minimum value of VR is?

#46. The minimum value of VR is?

#47. ATC require a class A aircraft to conduct a 20° banked turn as soon as possible after lift-off. What is the minimum allowable height for the commencement of this turn and by what margin must the aircraft clear obstacles during the turn?

#48. When taking-off from a contaminated runway?

#49. An error is made carrying out the take-off performance calculations, resulting in the calculated V1 figure of 160 Kts, being 10 kts too high. Which of the following statements is true?

#50. The minimum value of VR is?

#51. An error is made carrying out the take-off performance calculations, resulting in the calculated figure of 140 Kts, being 10 kts too low. Which of the following statements is true?

#52. An error is made carrying out the take-off performance calculations, resulting in the calculated figure of 160 Kts, being 10 kts too high Which of the following statements is true?

#53. What proportion of a headwind should be taken into account when calculating take-off performance for a single engine propeller aircraft of 3000 Kg mass, when operating from a dry paved runway?

#54. What proportion of a tailwind should be taken into account when calculating take-off performance for a single engine propeller aircraft of 3000 Kg mass, when operating from a dry paved runway?

#55. An aerodrome has a runway of 4000 m and the first obstacle is 1500 meters from the end of the take-off run. What is the maximum take-off distance that may be assumed to be available.

#56. Defective anti-skid systems?

#57. Defective anti-skid systems? 1. lncrease LDR. 2. lncrease TORA. 3. lncrease ASDR. 4. lncrease TORR.

#58. TODR is?

#59. TORR is?

#60. Minimum acceptable obstacle clearance for class A aircraft in the obstacle domain is .... increasing to ...... in turns above 400 ft using bank angles of ..... ?

#61. Minimum acceptable all engines operating gradient for a twin piston aircraft at screen height in the takeoff is?

#62. A light piston twin climbs at a gradientof 10% from the screen height of 15m (50 ft). There is an obstacle 900 m high, 3280 m from the screen. By how much will the aircraft clear the obstacle?

#63. During certification testing of a twin engine jet aircraft the true take-off distances were 1547 m with all engines operating, and 1720 m with the critical engine inoperative at V,. What distance would be used for certification purposes?

#64. If an aircraft takes-off using the wet V, instead of the dry V, how will TODR and climb performance be affected?

#65. Can take-off be carried out if V, is less than VMCG?

#66. V2 is?

#67. Which of the following is true of the increased V2 procedure?

#68. Wind component at take-off does not affect?

#69. TODA is?

#70. The first segment ends?

#71. Can a stopway be included in take-off run required (TORR) calculations?

#72. Reduced thrust take-off should not be used?

#73. Can anti skid systems be used for take-off and landing?

#74. An increase in OAT will . . .. Field length limited TOW and . . ... climb limited TOW?

#75. What will happen to ASDA if anti-skid is Unserviceable?

#76. The distance to be maintained between aircraft is greatest when?

#77. Reduced thrust take-off should not be used?

#78. Reduced thrust take-off should not be used?