Aircraft Electrical Systems Flashcards

1
Q

What is the purpose of a circuit breaker?

A

To protect the circuits and wires from fire. The circuit breaker opens the circuit when an overload
exists.

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2
Q

What are the two principles on which circuit breakers operate?

A

Thermal and magnetic

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3
Q

What tool is used to measure the size of unmarked electrical wire?

A

A wire gauge

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4
Q

What are the colors of aircraft position lights and where are they mounted?

A

left wingtip red light, right wingtip green and a white light
mounted on the tail, visible from the rear of the aircraft.

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5
Q

What are the factors to be considered when selecting wire size for electrical power?

A

Allowable power loss, allowable voltage drop , and current-carrying ability.

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6
Q

When is a circuit breaker or fuse designed to open?

A

When an overload or circuit fault exists.

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7
Q

What type of breakers are not acceptable for use in aircraft?

A

Automatic reset type circuit breakers.

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8
Q

What is a slow-blow fuse?

A

A fuse that compensates for surges and high flow current by not blowing for several milliseconds.

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9
Q

What are the three most common faults that occur in an electrical circuit?

A

open circuits, shorted circuits, and low power.

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10
Q

What size electrical conduit should be used for a specific cable bundle?

A

25% larger than the maximum diameter of the wire bundle.

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11
Q

How should electrical switches typically be oriented in the on positon?

A

Up or forward.

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11
Q

What color insulator on a solderless connector is proper for a 10-gauge wire?

A

Yellow.

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12
Q

When should electrical switches be derated from their normal current rating?

A

When using with high rush-in circuits, inductive circuits, and DC motors.

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13
Q

When do DC electric motors draw several times their rated current?

A

During starting

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14
Q

What would cause an AC electrical motor to run too fast?

A

An excessive applied voltage, or the field windings shorted.

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15
Q

What would cause an AC electrical motor to run too slow?

A

low applied voltage, defective wiring, or no lubrication.

16
Q

How is the output voltage of an alternator controlled?

A

By using a voltage regulator to control the exciter field current and thus regulate the exciter output.

17
Q

What should be checked before any aircraft electrical load is increased?

A

The associated wires, conductors, and circuit protection devices should be checked to determine
that the new load will not exceed the rated limits of these units.

18
Q

What is the main advantage of using AC for aircraft electrical power systems?

A

The principle advantage is that the voltage of AC power systems is easily changed by the use of
transformers. Therefore, you can transmit power at high voltage and low current, thus reducing the
size and weight of the wiring in the circuit.

19
Q

In AC power systems, how is DC obtained for battery charging?

A

by the use of rectifiers.

20
Q

How long should bonding jumper wires be made?

A

As short as practicable.

20
Q

What warns pilots of overheating batteries?

A

A thermal sensor in the battery and a light in the cockpit.

21
Q

What should be done to a conduit end when fittings are not used?

A

It should be deburred to prevent wire insulation damage.

21
Q

How can a particular wire in a bundle be identified?

A

By the identification code on the wire.

22
Q

How many terminal lugs can be put on a single stud on a terminal strip in an aircraft?

A

Four.

23
Q

What hardware is used to make bonding or grounding connections to a structure of dissimilar material?

A

A washer of suitable material should be used so the corrosion will occur on the washer.

24
Q

What controls the output voltage of an alternator?

A

A generator control unit (GCU).