The Pitot - Static System Flashcards

1
Q

If no alt static source is available, and the main static vent is blocked, what method can be used allow a static input?

A

By breaking the VSI glass

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2
Q

Static pressure and dynamic pressure combined is called?

A

Total pressure, or pitot pressure.

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3
Q

which instruments require dynamic pressure to function?

A

The ASI and Mach Meter

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4
Q

Pitot pressure = ?

A

Static pressure + dynamic pressure

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5
Q

Dynamic pressure =

A

pitot pressure - static pressure

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6
Q

Light aircraft can include a way of obtaining static and dynamic pressure in a cheaper way, this device is called?

A

Pitot/Static head, it combines static and dynamic pressure in one unit.

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7
Q

Position error, also referred to as pressure error, is caused by?

A

Changes in aircraft configuration, which can create turbulence around the static vents.

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8
Q

Position error, also referred to as pressure error, can be overcome by?

A

Removing the static vents from the pitot head and locating them on either side of the fuselage, this arrangement also minimises manoeuvre induced error.

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9
Q

If the static is blocked in a descent:

A

· VSI will show zero

· Altimeter continues to display the reading at which the blockage occurred

· The IAS will increase

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10
Q

PUDSOD:

A

Pitot blocked

Underread

Descent

Static blocked

Overread

Descent

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11
Q

When the alternate static source pressure is used, the following instrument indications are observed:

A
  1. The altimeter indicates a slightly higher altitude than actual
  2. The ASI indicates an airspeed greater than the actual airspeed
  3. The VSI shows a momentary climb and then stabilizes if the altitude is held constant
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11
Q

When the alternate static source pressure is used, the following instrument indications are observed:

A
  1. The altimeter indicates a slightly higher altitude than actual
  2. The ASI indicates an airspeed greater than the actual airspeed
  3. The VSI shows a momentary climb and then stabilizes if the altitude is held constant
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