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AMT 113 INSTRUMENTS EXAM QUESTIONS ANSWERED CORRECTLY LATEST UPDATE 2026

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AMT 113 INSTRUMENTS EXAM QUESTIONS ANSWERED CORRECTLY LATEST UPDATE 2026 The angle-of-attack detector operates from differential pressure when the airstream - Answers is not parallel to the true angle of attack of the aircraft. A barometric altimeter indicates pressure altitude when the barometric scale is set at - Answers 29.92 "Hg. What marking color is used to indicate if a cover glass has slipped? - Answers White. Instrument static system leakage can be detected by observing the rate of change in indication of the - Answers altimeter after suction has been applied to the static system to cause a prescribed equivalent altitude to be indicated. Which of the following causes of aircraft magnetic compass inaccuracies may be compensated for by mechanics? - Answers Deviation. At sea level, when the average atmospheric pressure is 14.7 psi, the barometric pressure is - Answers 29.92 "Hg. A certificated mechanic may perform - Answers 100 hour inspections of instruments A certificated mechanic with airframe and powerplant ratings may - Answers perform minor repairs and minor alterations to aircraft instruments. When selecting hardware for attaching bonding connections to an aircraft structure, which of the following should be considered? - Answers Mechanical strength, ease of installation, amount of current to be carried. Aircraft instrument value should be marked and graduated in accordance with - Answers the specific aircraft maintenance or flight manual. Which condition would be most likely to cause excessive vacuum in a vacuum system? - Answers Vacuum relief valve improperly adjusted. When performing the static system leakage check required by 14 CFR 91.411, the technician utilizes - Answers negative pressure. Aircraft temperature thermocouple leads may - Answers not be altered and are designed for a specific installation. The requirements for testing and inspection of instrument static systems required by 14 CFR 91.411 are contained in - Answers Part 43, appendix E. Where may a person look for the information necessary to determine the required markings on an engine instrument? - Answers Aircraft flight manual or aircraft maintenance manual. How is a flangeless instrument case mounted in an instrument panel? - Answers By an expanding-type clamp secured to the back of the panel and tightened by a screw from the front of the instrument panel. Which instrument condition is acceptable and would not require correction? - Answers Case paint chipped. What must be done to an instrument panel that is supported by shock mounts? - Answers Bonding straps must be installed across the instrument mounts as a current path. A turn coordinator instrument indicates - Answers both roll and yaw The red radial lines on the face of an engine oil pressure gauge indicates - Answers minimum and/ or maximum safe operating limits. Which of the following operating mechanisms would be found in a hydraulic pressure gauge? - Answers Bourdon tube. The maximum deviation (during level flight) permitted in a compensated magnetic direction indicator installed on an aircraft certificated under 14 CFR Part 23 is - Answers 10__degrees__. When an airplane's primary flight control surfaces are set for a particular phase of flight, such as landing or takeoff, the corresponding control-surface indicating system will show - Answers trim position. Which of the following instruments are controlled by gyroscopes? - Answers Attitude indicator, heading indicator, and turn needle of the turn-and-slip indicator. The green arc on an aircraft temperature gauge indicates - Answers the desirable temperature range. Fuel flow transmitters are designed to transmit data - Answers electrically. Which statement regarding an aircraft instrument vacuum system is true? - Answers Dry-type vacuum pumps with carbon vanes are very susceptible to damage from solid airborne particles and must take in only filtered air. An airspeed indicator measures the differential between - Answers pitot and static air pressure. Which instruments are connected to an aircraft's pitot-static system? - Answers Vertical speed indicator, altimeter, and airspeed indicator. When an aircraft altimeter is set at 29.92 "Hg on the ground, the altimeter will read - Answers pressure altitude. An aircraft instrument panel is electrically bonded to the aircraft structure to - Answers provide current return paths. Which procedure should the aviation mechanic use if a vacuum-operated instrument glass is found to be loose? - Answers Install another instrument. The operation of an angle of attack indicating system is based on detection of differential pressure at a point where the airstream flows in a direction - Answers not parallel to the true angle of attack of the aircraft. Instrument panel shock mounts absorb - Answers low-frequency, high-amplitude shocks. Stall warning systems are generally designed to begin warning the pilot when a stall - Answers is imminent A synchro transmitter is connected to a synchro receiver - Answers electrically with wires. The pneumatic (reed) type stall warning system installed in some light aircraft is activated by - Answers negative air pressure. An aircraft magnetic compass is swung to up-date the compass correction card when - Answers equipment is added that could effect compass deviation. If a static pressure system check reveals excessive leakage, the leak(s) may be located by - Answers isolating portions of the line and testing each portion systematically starting at the instrument connections. Data transmitted between components in an EFIS are converted into - Answers digital signals. Cases for electrically operated instruments are made of - Answers Iron or steel cases. Which instruments are connected to an aircraft's static pressure system only? - Answers Vertical speed indicator and altimeter. Turbine engine exhaust gas temperatures are measured by using - Answers chromel/alumel thermocouples. Aircraft instrument panels are generally shock-mounted to absorb - Answers low-frequency, high-amplitude shocks. The method of mounting aircraft instruments in their respective panels depends on the - Answers design of the instrument case. What will be the result if the instrument static pressure line becomes disconnected inside a pressurized cabin during cruising flight? - Answers The altimeter and airspeed indicator will both read low. Which of the following instruments will normally have range markings? - Answers Cylinder head temperature gauge and airspeed indicator. The lubber line on a directional gyro is used to - Answers represent the nose of the aircraft. Magnetic compass bowls are filled with a liquid to - Answers dampen the oscillation of the float. What does a reciprocating engine manifold pressure gauge indicate when the engine is not operating? - Answers The existing atmospheric pressure. Who is authorized to repair an aircraft instrument? - Answers A certificated repair station approved for that class instrument. Bonding connections should be tested for - Answers resistance value. Which of the following will cause inaccuracies in a magnetic compass that may be compensated for by an aircraft mechanic? - Answers Deviation. The function of a symbol generator (SG) in an EFIS is to - Answers receive and process input signals from aircraft and engine sensors and send the data to the appropriate display. What is the fixed line mark attached to the compass bowl of a magnetic compass called? - Answers Lubber line.

Meer zien Lees minder
Instelling
AMT 113
Vak
AMT 113

Voorbeeld van de inhoud

AMT 113 INSTRUMENTS EXAM QUESTIONS ANSWERED CORRECTLY LATEST UPDATE 2026

The angle-of-attack detector operates from differential pressure when the airstream - Answers is not
parallel to the true angle of attack of the aircraft.
A barometric altimeter indicates pressure altitude when the barometric scale is set at - Answers
29.92 "Hg.
What marking color is used to indicate if a cover glass has slipped? - Answers White.
Instrument static system leakage can be detected by observing the rate of change in indication of the
- Answers altimeter after suction has been applied to the static system to cause a prescribed
equivalent altitude to be indicated.
Which of the following causes of aircraft magnetic compass inaccuracies may be compensated for by
mechanics? - Answers Deviation.
At sea level, when the average atmospheric pressure is 14.7 psi, the barometric pressure is - Answers
29.92 "Hg.
A certificated mechanic may perform - Answers 100 hour inspections of instruments
A certificated mechanic with airframe and powerplant ratings may - Answers perform minor repairs
and minor alterations to aircraft instruments.
When selecting hardware for attaching bonding connections to an aircraft structure, which of the
following should be considered? - Answers Mechanical strength, ease of installation, amount of
current to be carried.
Aircraft instrument value should be marked and graduated in accordance with - Answers the specific
aircraft maintenance or flight manual.
Which condition would be most likely to cause excessive vacuum in a vacuum system? - Answers
Vacuum relief valve improperly adjusted.
When performing the static system leakage check required by 14 CFR 91.411, the technician utilizes -
Answers negative pressure.
Aircraft temperature thermocouple leads may - Answers not be altered and are designed for a
specific installation.
The requirements for testing and inspection of instrument static systems required by 14 CFR 91.411
are contained in - Answers Part 43, appendix E.
Where may a person look for the information necessary to determine the required markings on an
engine instrument? - Answers Aircraft flight manual or aircraft maintenance manual.
How is a flangeless instrument case mounted in an instrument panel? - Answers By an expanding-
type clamp secured to the back of the panel and tightened by a screw from the front of the
instrument panel.
Which instrument condition is acceptable and would not require correction? - Answers Case paint
chipped.
What must be done to an instrument panel that is supported by shock mounts? - Answers Bonding
straps must be installed across the instrument mounts as a current path.
A turn coordinator instrument indicates - Answers both roll and yaw
The red radial lines on the face of an engine oil pressure gauge indicates - Answers minimum and/ or
maximum safe operating limits.
Which of the following operating mechanisms would be found in a hydraulic pressure gauge? -
Answers Bourdon tube.
The maximum deviation (during level flight) permitted in a compensated magnetic direction indicator
installed on an aircraft certificated under 14 CFR Part 23 is - Answers 10__degrees__.
When an airplane's primary flight control surfaces are set for a particular phase of flight, such as
landing or takeoff, the corresponding control-surface indicating system will show - Answers trim
position.
Which of the following instruments are controlled by gyroscopes? - Answers Attitude indicator,
heading indicator, and turn needle of the turn-and-slip indicator.
The green arc on an aircraft temperature gauge indicates - Answers the desirable temperature range.
Fuel flow transmitters are designed to transmit data - Answers electrically.
Which statement regarding an aircraft instrument vacuum system is true? - Answers Dry-type
vacuum pumps with carbon vanes are very susceptible to damage from solid airborne particles and
must take in only filtered air.
An airspeed indicator measures the differential between - Answers pitot and static air pressure.

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AMT 113
Vak
AMT 113

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