05 Take Off - General Principles Flashcards

1
Q

What are the following distances during the take-off?

  • TOR (take off run)
  • TOD (take off distance)
A
  • TOR is from brakes released until Vlof

- TOD is from brakes released until the screen height is reached

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2
Q

What is the screen height for the following AC class’?

  • Class A
  • Class B
A
  • Class A: 35 ft

- Class B: 50 ft

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3
Q

Describe Vr

A

Vr is the speed at rotation

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4
Q

Describe Vlof

A

Vlof is the speed at lift off

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5
Q

What type of speed is Vr and Vlof (TAS, IAS etc.) and why?

A
  • Vr and Vlof are IAS (or CAS if the AC has a flight computer)
  • They are IAS’ and not TAS as different AF conditions can result in achieving the same IAS at different TAS
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6
Q

At the very beginning of the TOR, what is the biggest cause of drag?

A

Wheel Drag

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7
Q

During the TOR what type of drag predominates?

A

Lift induced drag

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8
Q

During the TOR what happens to Thrust, and subsequently acceleration, and why?

A
  • As speed increases, Thrust decreases and so acceleration decreases
  • This is because momentum drag starts to take effect but the Ram effect does not yet take place to counter it
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9
Q

When is an AC said to be at it’s Runway Limited Take-Off Mass (RLTOM)?

A

When the TOD = TODA

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10
Q

What percentage of the Headwind and Tailwind components is it mandatory to be factored in?

A
  • 50% headwind

- 150% tailwind

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11
Q

What is the formula for calculating the:

  • Head/Tailwind component
  • Crosswind component
A
  • Head/Tailwind component = Wind Speed * Cos (theta)

- Crosswind component = Wind Speed * Sin (theta)

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12
Q

Describe the two types of drag associated with runway contamination

A
  • Displacement drag: the wheels must move the contaminant out of the path of the AC
  • Impingement drag: contaminant which is sprayed up from the wheels onto the AC, adding weight and a force acting in the opposite direction of the AC
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13
Q

When is an AC said to be at its Climb Limited Take Off Mass?

A

When the mass of the AC is such that is can only just achieve the minimum required climb gradient

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14
Q

What factors effect the Climb Limited Take Off Mass (CLTOM)?

A
  • Weight
  • Altitude
  • Temperature
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15
Q

What is Vr in relation to V1?

A

Vr must be equal to or higher than V1

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16
Q

Describe V1

A
  • V1 is the decision speed

- Once this speed is reached the AC will take off

17
Q

How is the certificated take of distance established?

A

The greater of:

  • All engine TOD x 1.15
  • Engine failure at V1 TOD
18
Q

What is the effect of using engine bleed air on take off distance?

A

Using engine bleed air will reduce the available thrust and increase the take-off distance

19
Q

How does wind effect:

  • CLTOM
  • OLTOM
A
  • Has no effect on CLTOM

- A tail wind will reduce OLTOM and a head wind will increase OLTOM

20
Q

What is a Balanced Field Take Off?

A

Where OEI TODR = OEI ASDR

One Engine Inoperative