AIRCRAFT INSTRUMENT SYSTEM Flashcards

1
Q

The operating mechanism of most hydraulic pressure gauges is _______.

A

Bourdon tube.

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2
Q

What is the fixed line mark attached to the compass bowl of a magnetic compass
called?

A

Lubber line.

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3
Q

When swinging a magnetic compass, the compensators are adjusted to correct
for______.

A

magnetic influence deviation

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4
Q

The maximum deviation (during level flight) permitted in a compensated
magnetic direction indicator installed on an aircraft certificated under Federal
Aviation Regulation Part 23 is ____________.

A

10.

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5
Q

Magnetic compass bowls are filled with a liquid to___________-.

A

dampen the oscillation of the float.

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6
Q

The maximum altitude loss permitted during an unpressurized aircraft
instrument static pressure system integrity check is______

A

100 feet in 1 minute.

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7
Q

When an aircraft altimeter is set at 29.92 inches Hg on the ground, the altimeter will
read_______________.

A

pressure altitude.

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8
Q

When an aircraft altimeter is set at 29.92 inches Hg on the ground, the altimeter will
read_________.

A

pressure altitude.

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9
Q

A turn coordinator instrument indicates________.

A

both roll and yaw.

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10
Q

Thermocouple leads_________.

A

are designed for a specific installation and may not be altered.

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11
Q

A synchro transmitter is connected to a synchro receiver__________.

A

electrically with wires.

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12
Q

Fuel flow transmitters are designed to transmit data ___________.

A

electrically.

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13
Q

Data transmitted between components in an EFIS are converted into_____.

A

digital signals.

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14
Q

The function of a CRT in an EFIS is to_________ .

A

display alphanumeric data and representations of aircraft instruments.

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15
Q

The function of a symbol generator (SG) in an EFIS is to _________.

A

receive and process input signals from aircraft and engine sensors and send the
data to the appropriate display.

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16
Q

A radar altimeter determines altitude by___________.

A

transmitting a signal and receiving back a reflected signal.

17
Q

How would an airspeed indicator be marked to show the best rate of climb
speed (one engine inoperative)?

A

A blue radial line.

18
Q

What marking color is used to indicate if a cover glass has slipped?

A

white.

19
Q

Aircraft instruments should be marked and graduated in accordance
with____.

A

the specific aircraft maintenance or flight manual

20
Q

The method of mounting aircraft instruments in their respective panels
depends on the_____.

A

design of the instrument case.

21
Q

Cases for electrically operated instruments are made of_________ .

A

Iron or steel cases.

22
Q

When installing an instrument in an aircraft, who is responsible for
making sure it is properly marked?

A

The instrument installer.

23
Q

The red radial lines on the face of an engine oil pressure gauge
indicates_______.

A

minimum and/ or maximum safe operating limits.

24
Q

A certificated mechanic may perform__________.

A

100-hour inspections of instruments.

25
Q

An aircraft instrument panel is electrically bonded to the aircraft structure
to_________.

A

provide current return paths.

26
Q

When performing the static system leakage check required by Section 91.411, the
technician utilizes_____________.

A

negative pressure.

27
Q

If a static pressure system check reveals excessive leakage, the leak(s) may be
located by____________.

A

isolating portions of the line and testing each portion systematically, starting at
the instrument connections.

28
Q

The lubber line on a directional gyro is used to__________.

A

represent the nose of the aircraft.

29
Q

How is a flangeless instrument case mounted in an instrument panel?

A

By an expanding type clamp secured to the back oftie panel and
tightened by a screw from the front of the instrument panel.

30
Q

How would an airspeed indicator be marked to show the best rate of climb
speed (one engine inoperative)?

A

A blue radial line.