2101 - FINALS

Question 1

1.When the speed to perform this check is obtained, momentarily turn the ignition switch to the ______

Answer 1

off position

Question 2

It is used to controls the rate of charge to the battery by stabilizing the generator or alternator electrical output.

Answer 2

voltage regulator

Question 3

Each generator supplies how many volts to Alternating Current (AC) to its own bus?

Answer 3

115V 400Hz

Question 4

What is the meaning of CSD?

Answer 4

Constant Speed drive

Question 5

This supply is known as split operation that means the AC power sources are never ____

Answer 5

connected in parallel

Question 6

On the ground, the aircraft electrical network can be supplied by an _______

Answer 6

External Power source

Question 7

What is the meaning of ECAM?

Answer 7

electronic centralize for aircraft monitoring

Question 8

What is the meaning of GPCU?

Answer 8

Ground Power Control Unit

Question 9

The ______ will extend automatically to pressurize the blue hydraulic system, which powers theEMERgencyGenerator, if the A/C speed is sufficient and AC BUS 1 and 2 are no longer supplied.

Answer 9

Ram air turbine

Question 10

At the start/end of each flight, the battery is connected/disconnected from the electrical distribution bus through the _______

Answer 10

solenoid contact

Question 11

A battery master switch on the flight deck is used to control the _____

Answer 11

Solenoid

Question 12

14. When replacing or preparing a magneto for installation, the first concern is with the

Answer 12

internal timing of the magneto

Question 13

This angular displacement from the neutral position, known as ______

Answer 13

The E-gap angle

Question 14

The magneto drop should be even for both magnetos and is generally in the area of a _____drop for each magneto

Answer 14

25-75 rpm drop

Question 15

It is used to help determine the exact instant that the magneto points open. There are two general types of timing lights in common use.

Answer 15

timing lights

Question 16

The engine is usually timed by using the No. 1 cylinder on the_____.

Answer 16

Compression stroke

Question 17

The ignition switch check is usually made at____.

Answer 17

700 rpm

Question 18

This is the devices are mounted to the crankshaft flange and use a timing plate.

Answer 18

timing disk

Question 19

When the starter gear hub is installed correctly, the timing marks are marked on it that line up with the mark on the__

Answer 19

Starter

Question 20

On an engine that has no starter gear hub, the timing mark is normally on the ____

Answer 20

No. 1 piston is at top dead center.

Question 21

The piston is in a position where a straight line can be drawn through the center of the crankshaft journal, the crankpin, and

Answer 21

the piston pin

Question 22

A piston in top center has little value from a timing standpoint because the corresponding crankshaft position may vary from ______ for this piston position.

Answer 22

1° to 5°

Question 23

It is used to control electrical power between the aircraft generator and the distribution bus.

Answer 23

generation circuit

Question 24

30.It is used to supply power for engine starting and to provide a secondary power supply in the event of an alternator (or generator) failure.

Answer 24

Battery Circuit

Question 25

Give an examples of an equipment that commonly uses the aircraft electrical system for its source of energy

Answer 25

Position lights
Anticollision lights
Landing lights
Taxi lights
Interior cabin lights
Instrument lights
Radio equipment
Turn indicator
Fuel gauges
Electric fuel pump
Stall warning system
Pitot heat
Starting motor