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Project #4 - C172S Electrical System Interactive Trainer

A highly detailed cockpit of a C172S airplane showcasing its electrical system panels and instruments. The scene should include the various switches, busses and gauges with a clear focus on the electrical system. The setting should be realistic and inviting for aviation enthusiasts.

C172S Electrical System Quiz

Test your knowledge of the C172S electrical system with this interactive quiz! Designed for both aviation enthusiasts and students, this quiz features multiple-choice questions that cover various aspects of the aircraft's electrical components and their functions.

You'll explore topics such as standby power, bus systems, and circuit operations. Get ready to enhance your expertise!

Multiple-choice questions
Covering essential aircraft electrical knowledge
Engaging and informative

15 Questions4 MinutesCreated by FlyingEagle321

What position must the STBY BATT switch be in for the system to automatically provide standby power to the ESS BUS in the event of an emergency?

OFF

TEST

ARM

What busses can the EXTERNAL POWER provide power to?

X-FEED BUS

ELEC BUS 1

ESS BUS

ALL BUSSES

Where are the alternator current, standby battery current, and main bus voltage displayed?

ACU

Standby Battery Panel

Engine Indication System (EIS)

Main Voltmeter

What is the purpose of the X-FEED BUS?

Allow power to flow from either ELEC BUS 1 or ELEC BUS 2 to the ESS BUS

Ensure power is available from either ELEC BUS 1 or ELEC BUS 2 to both AVN BUS 1 and AVN BUS 2

Allow power to crossfeed from one primary bus to the other

Ensure power is available from either ELEC BUS 1 or ELEC BUS 2 for the ALT FIELD and WARN circuits

Where can the IGNITION SWITCH get power from?

MAIN BATTERY or EXTERNAL POWER

EXTERNAL POWER

MAIN BATTERY

ALTERNATOR

What switches must be ON for the MFD to have power?

BAT MASTER and ALT MASTER

BAT MASTER and STBY BATT ARM

BAT MASTER only

BAT MASTER and AVIONICS BUS 2

During normal operation, what Bus feeds power to the AVIONICS BUS 2?

ELEC BUS 2

AVN BUS 1

ELEC BUS 1

ESS BUS

If the ALT FIELD circuit breaker trips offline during flight, where does electrical power come from to power all the systems?

EXTERNAL POWER

BATTERY

ALTERNATOR

STANDBY BATTERY

It is possible to turn ON the BAT MASTER switch without turning ON the ALT MASTER switch

True

False

It is possible to turn OFF the BAT MASTER switch without turning OFF the ALT MASTER switch

True

False

If the AVN 1 circuit breaker trips offline causing the AVN BUS 1 to lose power, do the ADC/AHRS systems lose power and shutdown?

What are you talking about?

Yes, because they are powered from AVN BUS 1

No, because they also receive power from ESS BUS

No, because they receive power from AVN BUS 2

If all systems are operating normally, how is power provided the ESS BUS?

From X-FEED BUS

From ELEC BUS 1

From ELEC BUS 2

From ELEC BUS 1 and ELEC BUS 2

What switch must be turned ON in order to allow battery voltage to the ELEC BUS 1 and ELEC BUS 2?

AVIONICS BUS 1 / AVIONICS BUS 2

STBY BATT ARM

BAT MASTER

ALT MASTER

What provides power to the ESSENTIAL BUS (ESS BUS) in the event that both FEEDER A and FEEDER B circuit breakers trip offline?

EXTERNAL POWER

ALTERNATOR

BATTERY

STANDBY BATTERY

What switches must be ON for the PFD to have power?

BAT MASTER and STBY BATT ARM

BAT MASTER only

BAT MASTER and ALT MASTER

BAT MASTER and AVIONICS BUS 1

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