Chapter 2 - Pressure Altimeter Flashcards

1
Q

What converts pressure changes into a mechanical movement?

A

Aneroid Capsule

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2
Q

What does an aneroid capsule contain?

A

Contains vacuum or very low pressure

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3
Q

Detail the different types of altimeters

A

Simple
Sensitive
Servo

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4
Q

What are advantages of servo altimeters?

A

Improved accuracy at higher altitudes

Friction in conventional linkage reduced

Digital readout / warnings are easily incorporated

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5
Q

What is an encoder Altimeter?

A

Digitizers send output to the transponder for transmission to ATC, only on 1013 hPa.

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6
Q

What is density altitude?

A

Density Altitude is the height in ISA conditions that has a density corresponding to the actual ambient density. Or in other words, it is Pressure Altitude corrected for ambient conditions.

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7
Q

What is the formula for working out density altitude?

A

Density Altitude = Pressure Altitude +/- 120ft x per 1oC change from ISA

  • If colder than ISA, subtract from Pressure Altitude
  • If warmer than ISA, add to Pressure Altitude
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8
Q

In an unpressurised A/C will the altimeter over or under read?

A

The altimeter will over-read due to the pressure in the cabin being lower than
ambient (aerodynamic suction). N.B. For EASA, assume alternate static port is within the cabin.

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9
Q

In a pressurised A/C will the altimeter over or under read?

A

The altimeter will show the (lower) cabin altitude rather than ambient altitude.

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10
Q

What is Lag error?

A

Response to height changes are not instantaneous:

  • Climb – Under-Read
  • Descent – Over read

Sensitive Altimeter - lag should not exceed 150ft.

Servo-assisted Altimeter - no lag for vertical speeds less than 10 000 ft/min Altitude and time spent at altitude / cold increases the lag.

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11
Q

What are causes of error in altimeter readings?

A

Barometric (atmospheric pressure differs from ISA), Temperature (temp different from ISA), Pressure, Instrument, Lag, Orographic, Blockages

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12
Q

What is the rule of thumb for correcting for density altitude?

A

Density Altitude = 120 ft change in Pressure Altitude per 1C change from ISA for density Altitude

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