When starting engines with ground power, the generator switches should always be ___ to allow both engines to start with ground power. Ground power starts with generator switches ___ will result in a ______ _____ start on the first engine, and a ______- ________ ________ ______ on the second engine.
A
ELECTRICAL
When starting engines with ground power, the generator switches should always be OFF to allow both engines to start with ground power. Ground power starts with generator switches ON will result in a groundpower start on the first engine, and a generator- assistedbatterystart on the second engine.
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2
Q
ELECTRICAL
If both generators fail and the battery switch is placed in the ____ position, ________ bus and hot battery bus items are available for at least ___ minutes.
A
ELECTRICAL
If both generators fail and the battery switch is placed in the EMER position, emergency bus and hot battery bus items are available for at least 30 minutes.
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3
Q
ELECTRICAL
If the battery is the only source of power and the battery and avionics switches are ___, the electrical system will be powered for ___ minutes.
A
ELECTRICAL
If the battery is the only source of power and the battery and avionics switches are ON, the electrical system will be powered for 10 minutes.
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4
Q
ELECTRICAL
An in-flight engine start using the ____ _____ (_____ _______) counts as a ____ ______ cycle. Generator-assisted starts are ________ in flight.
A
ELECTRICAL
An in-flight engine start using the start button (starterassisted) counts as a full battery cycle. Generator-assisted starts are disabled in flight.
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5
Q
ELECTRICAL
If both generators fail, the amber ___ ____ _-_ annunciator illuminates, along with the _______ _______ and _______ _________ lights.
A
ELECTRICAL
If both generators fail, the amber GENOFF L-R annunciator illuminates, along with the MASTERWARNING and MASTER CAUTION lights.
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6
Q
ELECTRICAL
The _______ _________ switch uses ______ ______ to disconnect the aircraft battery, and will slowly _______ the battery when activated. The battery switch must be ___ for this function to operate.
A
ELECTRICAL
The BatteryDisconnect switch uses battery power to disconnect the aircraft battery, and will slowly discharge the battery when activated. The battery switch must be ON for this function to operate.
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7
Q
ELECTRICAL
The CJ3 electrical system uses ____ DC generators for normal power, and a _____ for _____ and _____ power.
A
ELECTRICAL
The CJ3 electrical system uses two DC generators for normal power, and a battery for starting and backup power.
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8
Q
ELECTRICAL
The function of the GCU is to ________, ________, and ______ the DC generators.
A
ELECTRICAL
The function of the GCU is to regulate, parallel, and protect the DC generators.
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9
Q
ELECTRICAL
The main aircraft battery will receive charging power when the _______ and ___ or ____ generator switches are ____ and the engines are ______, or when an operating ______ ______ unit is connected.
A
ELECTRICAL
The main aircraft battery will receive charging power when the battery and one or both generator switches are ON and the engines are running, or when an operating groundpower unit is connected.