SYS106 Flashcards
What electrical component allows isolation of the generator and battery buses?
The bus tie switch
The starter/generator is regulated and monitored by:
The Generator Control Unit (GCU) located in the rear cockpit.
Generator power is controlled by the ______ switch.
generator control (GEN)
The rear cockpit avionics bus receives power through the:
front cockpit avionics bus
Circuit breakers labeled FWD AVI and AFT AVI control front and rear cockpit avionics buses and are located on the front cockpit:
battery bus and generator bus circuit breaker panels
A circuit breaker labeled AFT BAT on the front cockpit battery bus circuit breaker panel controls the
rear cockpit battery bus
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
an avionics master switch
An amber __________ light on the annunciator panel in each cockpit will indicate an open bus tie switch
BUS TIE
Circuit breakers protecting systems and equipment operating from the battery bus are located on the __________ panel in each cockpit.
left console
Each circuit breaker is marked with the maximum __________ it will allow to pass before popping.
current load in amps
Battery power is controlled through ___________ switch on the right forward switch panel in either cockpit
a battery
A switch labeled AUX BAT on the front cockpit left console test panel is positioned forward to test the
__________ during preflight checks
auxiliary battery
External power is controlled by the ______ switch and distributed on the ________ bus.
battery, battery
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.
false
__________ lights can be detached and relocated to the right canopy rail for use as an area or map light.
Utility
The landing light will only come on when the landing light switch is activated and the landing gear
is down and locked
When switched on, white position lights at the trailing edge of each wingtip
are constantly illuminated
The generator provides ____ VDC power, and is capable of supplying __________ amps
28, 300
The generator can be controlled from either cockpit through use of the generator
control switch
If a component or circuit malfunctions, the affected __________ will open, shutting off current flow to that
component or circuit.
circuit breaker
The battery can be controlled from either cockpit through use of the __________ switch
battery
Light output from the instruments, control panels, and displays can be adjusted by using dimming controls
located on the __________ panel in each cockpit.
trim control
The taxi light is located aft and inboard of the
right main landing gear strut
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.
left side of the front
The starter/generator provides 28 volts DC, while the battery and auxiliary battery are __________ VDC units.
24
