SYS106

Question 1

What electrical component allows isolation of the generator and battery buses?

Answer 1

The bus tie switch

Question 2

The starter/generator is regulated and monitored by:

Answer 2

The Generator Control Unit (GCU) located in the rear cockpit.

Question 3

Generator power is controlled by the ______ switch.

Answer 3

generator control (GEN)

Question 4

The rear cockpit avionics bus receives power through the:

Answer 4

front cockpit avionics bus

Question 5

Circuit breakers labeled FWD AVI and AFT AVI control front and rear cockpit avionics buses and are located on the front cockpit:

Answer 5

battery bus and generator bus circuit breaker panels

Question 6

A circuit breaker labeled AFT BAT on the front cockpit battery bus circuit breaker panel controls the

Answer 6

rear cockpit battery bus

Question 7

Except for the back-up UHF control head and UHF transceiver, power for all avionics and radio systems in both cockpits is furnished through __________ on the right forward switch panel in the front cockpit

Answer 7

an avionics master switch

Question 8

An amber __________ light on the annunciator panel in each cockpit will indicate an open bus tie switch

Answer 8

BUS TIE

Question 9

Circuit breakers protecting systems and equipment operating from the battery bus are located on the __________ panel in each cockpit.

Answer 9

left console

Question 10

Each circuit breaker is marked with the maximum __________ it will allow to pass before popping.

Answer 10

current load in amps

Question 11

Battery power is controlled through ___________ switch on the right forward switch panel in either cockpit

Answer 11

a battery

Question 12

A switch labeled AUX BAT on the front cockpit left console test panel is positioned forward to test the
__________ during preflight checks

Answer 12

auxiliary battery

Question 13

External power is controlled by the ______ switch and distributed on the ________ bus.

Answer 13

battery, battery

Question 14

Lighting for EFIS displays, the RMU, the AOA indexer, and the GPS control panel is adjusted using the knob
labeled INSTR PANEL on the trim control panel.

Answer 14

false

Question 15

__________ lights can be detached and relocated to the right canopy rail for use as an area or map light.

Answer 15

Utility

Question 16

The landing light will only come on when the landing light switch is activated and the landing gear

Answer 16

is down and locked

Question 17

When switched on, white position lights at the trailing edge of each wingtip

Answer 17

are constantly illuminated

Question 18

The generator provides ____ VDC power, and is capable of supplying __________ amps

Answer 18

28, 300

Question 19

The generator can be controlled from either cockpit through use of the generator

Answer 19

control switch

Question 20

If a component or circuit malfunctions, the affected __________ will open, shutting off current flow to that
component or circuit.

Answer 20

circuit breaker

Question 21

The battery can be controlled from either cockpit through use of the __________ switch

Answer 21

battery

Question 22

Light output from the instruments, control panels, and displays can be adjusted by using dimming controls
located on the __________ panel in each cockpit.

Answer 22

trim control

Question 23

The taxi light is located aft and inboard of the

Answer 23

right main landing gear strut

Question 24

A fault occurs in the circuit controlling the anti-collision lights. The COLL circuit breaker will pop on the battery
bus circuit breaker panel located on the __________ cockpit.

Answer 24

left side of the front

Question 25

The starter/generator provides 28 volts DC, while the battery and auxiliary battery are __________ VDC units.

Answer 25

24