Aircraft Instrument Flashcards

1
Q

Combined system
that utilizes the
static air pressure
and the dynamic
pressure due to
the motion of the
aircraft through
the air

A

Pitot-Static Instruments

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2
Q

An instrument that measures
the height of an aircraft
above a given pressure leve

A

Altimeter

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3
Q

read directly from the
altimeter (uncorrected) when it is set to the
current altimeter setting.

A

Indicated altitude

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4
Q

the vertical distance of the
aircraft above sea level. Often expresses as
feet above mean sea level (MSL)

A

True altitude

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5
Q

the vertical distance of an
aircraft above the terrain, or above ground
level (AGL)

A

Absolute altitude

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6
Q

: the altitude indicated when
the altimeter setting window is adjusted to
29.92” Hg or 1013 hPa. This is the altitude
above the standard datum plane.

A

Pressure altitude

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7
Q

pressure altitude corrected for
variations from standard temperature. If
temperature is above standard, density
altitude is higher than pressure altitude and
vice versa

A

Density altitude

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8
Q

Sometimes called a vertical
velocity indicator (VVI),
indicates whether the aircraft
is climbing, descending, or in
level flight.

A

Vertical Speed Indicator (VSI)

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9
Q

Rate of climb or descent is
indicated in

A

feet per minute
(fpm)

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10
Q

A sensitive, differential
pressure gauge that
measures and promptly
indicates the difference
between pitot and static
pressure.

A

Airspeed Indicator (ASI)

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11
Q

Measures the aircraft’s
speed through air

A

Airspeed Indicator (ASI)

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12
Q

direct instrument
reading obtained, uncorrected for variations in atmospheric density, installation error, or
instrument error.

A

Indicated airspeed (IAS)

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13
Q

IAS corrected for
installation error and instrument error

A

Calibrated airspeed (CAS)

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14
Q

CAS corrected for altitude
and nonstandard temperature.

A

True airspeed (TAS)

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15
Q

actual speed of the
airplane over the ground

A

Groundspeed (GS)

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16
Q

stalling speed in the
landing configuration

A

VS0

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17
Q

stalling speed in a
specific configuration

18
Q

flap operating
speed

19
Q

: maximum flap
extended speed

20
Q

normal
operating range of the
airplane

21
Q

maximum structural
cruising speed. Do not
exceed this speed except
in smooth air.

22
Q

caution range

A

Yellow arc

23
Q

never exceed speed

24
Q

Design maneuvering speed; the maximum
speed at which the structural design’s limit
load can be imposed without causing
structural damage.

25
Q

Landing gear operating speed; the
maximum speed for extending or retracting
the landing gear.

26
Q

Landing gear extended speed; the
maximum speed at which an aircraft can be
safely flown with the landing gear extended

27
Q

Decision speed; the maximum speed at
which the pilot must take the first action in
order to stop the airplane within the remaining
accelerate stop distance.

28
Q

Take-off safety speed; referenced airspeed
obtained after lift-off at which the required
one-engine inoperative climb performance
can be achieved.

29
Q

Rotate speed; the speed at which rotation
is initiated with the intention of becoming
airborne

30
Q

Lift-off speed; the speed at which the
airplane first becomes airborne which is at the
moment when the main wheels have left the
runway.

31
Q

Best angle-of-climb speed; the airspeed at
which an aircraft gains the greatest amount of
altitude in a given field.

32
Q

Best rate-of-climb speed; the airspeed that
provides the most altitude gain in a given
period of time

33
Q

the
principle that a
gyroscope remains in a
fixed position in the
plane in which it is
spinning.

A

Rigidity in Space

34
Q

the tilting
or turning of a gyro in
response to a
deflective force

A

Precession

35
Q

mounted at an angle, or
canted, so it can initially show roll rate.

A

Turn Coordinator

36
Q

shows only the rate of
turn in degrees per second

A

Turn-and-slip Indicator

37
Q

shows the aircraft’s
coordination, when
it is centered
between the two
lines, the aircraft is
coordinated.

A

Inclinometer (ball)

38
Q

With a miniature aircraft
and horizon bar, displays
a picture of the attitude
of the aircraft.

A

Attitude Indicator

39
Q

The relationship of the
miniature aircraft to the
horizon bar is the same
as the relationship of the
real aircraft to the actual
horizon

A

Attitude Indicator

40
Q

A mechanical instrument
designed to facilitate the
use of the magnetic
compass.

A

Heading Indicator