CITATION 500/501 SYSTEMS TEST
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1
ELECTRICAL-The purpose of the battery bus is to
2
ELECTRICAL-The power relay is integral to the GCU (generator control unit).
3
ELECTRICAL-Which statement is correct, With the battery switch in the OFF position
4
ELECTRICAL-On UNs 274 and below, which of the following statements are true?
5
ELECTRICAL-LH START button illumination is an indication of
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ELECTRICAL-Starter limitations are
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ELECTRICAL-For an EPU (external power unit) start the
8
FIRE PROTECTION-The BOTTLE 1 ARMED or the BOTTLE 2 ARMED switchlights when illuminated, indicates that
9
FIRE PROTECTION-The FIRE WARN switch light when illuminated will trigger the MASTER WARNING-True
10
FIRE PROTECTION-If an engine fire extinguishing bottle is depleted, depressing the ENG FIRE switch light will arm that bottle.
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HYDRAULIC POWER-The Citation hydraulic system is classified as an open center system
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HYDRAULIC POWER-The hydraulic system bypass valve is
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HYDRAULIC POWER-Depressing an ENG FIRE switchlight
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HYDRAULIC POWER-Closing of a hydraulic firewall shutoff valve is indicated by
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HYDRAULIC POWER-If electrical power is lost, the hydraulic system bypass valve
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LANDING GEAR-The landing gear uplocks are
17
LANDING GEAR-The landing gear downlocks are disengaged by
18
LANDING GEAR-The gear warning horn cannot be silenced when one or more gears are not locked down and.
19
MASTER WARNING-The Rotary Test Switch is inoperative in flight..
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MASTER WARNING-With the annunciators in the dimmed state (panel lights on),
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LIMITATIONS-The Maximum speed for autopilot operation is
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LIMITATIONS-The Maximum altitude for take-off and landing is
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LIMITATIONS-For take-off and landing, the maximum water/Slush on runway is
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LIMITATIONS-The Maximum temperature for take-off and landing is
25
LIMITATIONS-The Minimum temperature for take-off and landing is
 
   
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