Pre-Flight Planning: Airspeed Flashcards

1
Q

The airspeed indicator receives indication from what aircraft system?

A

Pitot-static system

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2
Q

What is dynamic pressure?

A

Pressure experienced by a body moving through the air or a stationary body experiencing a moving air mass

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3
Q

What is the pressure experienced by a body moving through the air or a stationary body experiencing a moving air mass

A

Dynamic pressure

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4
Q

What pressure is experienced constantly and is a result of the weight of the atmosphere?

A

Static pressure

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5
Q

Static pressure is the result of the…

A

Weight of the atmosphere

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6
Q

Total Pressure formula

A

Total Pressure = Static Pressure + Dynamic Pressure

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7
Q

Static pressure is independent of..

A

Speed

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8
Q

Why is the dynamic pressure less at a higher altitude?

A

Air is less dense at higher altitudes
Reduced dynamic pressure

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9
Q

Dynamic Pressure formula

A

1/2 x Air Density x True Airspeed ^2

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10
Q

How does an airspeed diaphragm respond to changes in dynamic pressure alone?

A

Static pressure is both inside and outside the diaphragm
Diaphragm contracts and expands in changes to dynamic pressure

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11
Q

Air density is often represented by what symbol?

A

Rho (p)

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12
Q

What happens to the TAS of an aircraft climbing at a constant IAS?

A

It must increase

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13
Q

What happens to dynamic pressure for an aicraft climbing at a constant IAS?

A

Dynamic pressure remains constant

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14
Q

Constant TAS for a climbing aircraft means its IAS is what?

A

Decreasing

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15
Q

Two reasons for differences in reading between CAS/RAS and IAS?

A

Instrument error (inherent defects)
Position error (pitot tube usually not aligned with incident airflow)

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16
Q

What factors affect density of air?

A

Pressure altitude and air temperature variations

17
Q

Calculation of a true airspeed on flight computer (process)

A

Calculate pressure altitude using QNH and planned/desired altitude
Use the pressure altitude, OAT and IAS to calculate the TAS

18
Q

How is pressure altitude usually calculated

A

Find difference between QNH and 1013
If QNH < 1013, pressure altitude is higher
If QNH > 1013, pressure altitude is lower