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