Flight Instruments Flashcards

1
Q

Pitot Static System has 3 instruments =

A

1) Airspeed indicator
2) Altimeter
3) Vertical Speed indicator

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2
Q

What does the pitot tube measure?

A

Dynamic Pressure (the speed that air enters the tube)
*ONLY talks to the airspeed indicator

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3
Q

Static Port in the pitot static system does what?

A

allows pressure in the pitot static system to equalize with outside atmosphere.
–Measures static outside air

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4
Q

Airspeed Indicator

A

uses both pitot & static sources.
–determines pressure outside and then takes speed at which it is moving through the pitot to determine airspeeding

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5
Q

IAS =

A

Indicated Airspeed
–uncorrected airspeed read from the indicator.
–This is what we actually reference when we fly.

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6
Q

CAS =

A

Calibrated Airspeed
–IAS when corrected for instrument & install error in pitot static pressure system

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7
Q

TAS =

A

True Airspeed
–Calibrated airspeed then corrected with density & temperature.

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8
Q

EAS

A

Equivalent Airspeed
–Calibrated airspeed corrected for compressibility factor 250knots & above

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9
Q

Pitot blockage =

A

ASI will “act like altimeter”
increase in a climb & decrease in a descent.
–will not affect vertical airspeed or altimeter

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10
Q

Static blockage =

A

ASI will “act opposite of altimeter”
decrease in a climb & increase in a descent.
*Altimeter will freeze & airspeed will read zero.

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11
Q

Fixing a blockage

A

1) focus on flying
2) determine cause
a) pitot blocked = try the pitot heat
OR switch to alternate pitot
b) static blockage = switch altnerate static source.
Emergency –> can break face ops VSI which will allow to read the static pressure in the plane.

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12
Q

Airspeed indicator errors
1) Position errors

A

Higher angles of attack = relative air is not head on = seems slower than it is.
Use airspeed correction chart in POH to compensate.

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13
Q

Airspeed indicator errors
2) Density error

A

ASI is calibrated to standard atmospheric conditions @ sea level.
To correct = add 2% of your airspeed / 1,000ft altitude.

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14
Q

Vertical speed indicator

A

measures rate of climb/descend.
100s ft/min

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15
Q

Altimeter errors
–blocks of pitot tube
–changes in temp
–changes in pressure

A

1) If static port were partially blocked = under read.
2) Statis port completely blocked = freeze.
3) Flying from warm to cold = being bold (it will over-read)
4) High pressure to relatively low pressure = over-read
high to low –> look out below!

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16
Q

Altimeter errors
–Mechanical
–Hysterisis
–Reversal
–Mountain Effect

A

1) Mechanical - misalignment or slip in gears/links
2) Hysterisis = Lag in instruments due to elastic properties of materials used in aneroids
3) Reversal = during abrupt or rapid attitude changes.
4) Mountain effect = decrease pressure due to air flowing through mountains. Due to downdrafts.

17
Q

Altimeter encoding

A

relays altitude info to the transponder through altitude encoder. = ATC can see your position and altitude via the transponder.
Only works when switched to ALT - done prior to take off on every flight.

18
Q

Indicated Altitude

A

The altitude read off of the altimeter

19
Q

Pressure Altitude

A

altitude displayed on the altimeter when subscale is set to standard atmospheric conditions (29.92”hg)

20
Q

Density Altitude

A

Pressure altitude corrected for temperature “the altitude the plane thinks it is”

21
Q

True Altitude

A

Exact height above mean sea level (MSL)

22
Q

Absolute Altitude

A

Exact height over the surface of the earth

23
Q

Magnetic Variation

A

Angle between the true meridian & magnetic meridian

24
Q

Magnetic Dip

A

Tendency of the compass to align itself with the earth magnetic lines

25
Q

Magnetic compass error with turning (north & south)

A

Turn North = Lags.
–turns in the opposite direction
Turn South = Leads.
–turns extra
**North lags & South leads

ONLY trust magnetic compass in straight & level, unaccelerated flight

26
Q

Magnetic compass error with acceleration/deceleration

A

When heading East/West
-Accelerating = compass reads more north.
-Deceleration = compass reads more south.
**ANDS = acceleration north, deceleration south

ONLY trust magnetic compass in straight & level, unaccelerated flight

27
Q

What instruments use Gyroscopes

A

Attitude indicator
Heading indicator
Turn coordinator

28
Q

which Gyroscopes are powered by an aircraft vacuum system verse electronically?

A

Airplanes vacuum system =
Attitude & heading indicators
Electronically = Turn coordinator

29
Q

Heading Indicator

A

must be re-adjusted every 15mins.
unusual attitude may result in the gyro tumbling = erratic indications - just wait for it to settle.

30
Q

Attitude indicator

A

artificial horizon
provides indication of pitch & bank.

31
Q

Attitude indicator ERRORS

A

1) Acceleration = can falsely indicate nose up
2) Deceleration = falsely indicate nose down

32
Q

Turn Coordinator

A

electrically powered gyro.
info on roll, yaw & rate of turn
–rate of turn NOT amount of bank
Ball = if turn is coordinated or not.

33
Q

Skid =

A

Too much rudder or not enough aileron.
No practical value & can lead to spins.

34
Q

Slip =

A

Not enough rudder or too much aileron.
Slips are performed for crosswind landing & to shed excess altitude without gaining airspeed.

35
Q

Turn bank indicator

A

also electronically powered
–gives turn & yaw info - where as the turn coordinator also detects roll.

36
Q

Flight instruments
1) Control
2) Performance

A

Control =
Attitude Indicator
Tachometer/Manifold Pressure

Performance =
ASI
VSI
Altimeter
Heading indicator
Turn coordinator

37
Q

Selective Radial Scan

A

The attitude indicator is always the center of your scan.
from there radiate to other instruments depending on the task.

38
Q

Scanning - what 3 questions should you always ask yourself?

A

1) What info do I need?
2) Which instruments give me that info?
3) Is the info reliable?