CITATION 500/501 SYSTEMS TEST

First name:		Last name:
E Mail:		Affiliate:

ELECTRICAL-The purpose of the battery bus is to

	Act as a bus tie for the hot battery and two main DC buses.
	Provide power for the Emergency bus.
	Provide power for the emergency lights.
	Provide power for the standby gyro.

ELECTRICAL-The power relay is integral to the GCU (generator control unit).

	True.
	False.

ELECTRICAL-Which statement is correct, With the battery switch in the OFF position

	The battery bus is powered.
	The generators will trip off line.
	The hot battery bus is powered.
	The emergency exit lights will illuminate.

ELECTRICAL-On UNs 274 and below, which of the following statements are true?

	Both inverters are on for normal operation.
	With the crossover switch in X OVER, the No 2 inverter powers both the flight director AC bus and the radar AC bus.
	The XOVER inverter powers both AC buses.
	With the crossover switch in NORM, the No 1 inverter powers both the flight director AC bus and the radar AC bus.

ELECTRICAL-LH START button illumination is an indication of

	Starter failure.
	The start circuit is energized.
	The panel lights are turned on.
	The start circuit is deenergized.

ELECTRICAL-Starter limitations are

	Three engine starts in one hour with a 3 minute rest between starts
	Three engine starts in 30 minutes with a 30 second rest between starts
	Three engine starts in one hour with a 30 second rest between starts
	Three engine starts in one hour with a 45 second rest between starts

ELECTRICAL-For an EPU (external power unit) start the

	battery switch should be placed in the OFF position
	generator switches have no effect on an EPU start
	generator switches should be placed in the OFF position
	generator switches should be placed in the GEN position

FIRE PROTECTION-The BOTTLE 1 ARMED or the BOTTLE 2 ARMED switchlights when illuminated, indicates that

	The respective bottle is armed and its agent will be directed to side with the illuminated F/W SHUTOFF annunciator.
	The No 2 bottle is armed and is for the right engine.
	The No 1 bottle is armed and is for the left engine.
	The respective bottle has been discharged.

FIRE PROTECTION-The FIRE WARN switch light when illuminated will trigger the MASTER WARNING-True

	False
	True

FIRE PROTECTION-If an engine fire extinguishing bottle is depleted, depressing the ENG FIRE switch light will arm that bottle.

	False
	True

HYDRAULIC POWER-The Citation hydraulic system is classified as an open center system

	True
	False

HYDRAULIC POWER-The hydraulic system bypass valve is

	(C) Energized closed
	(D) Both A and B
	(B) Spring loaded open.
	(A) Spring loaded closed.

HYDRAULIC POWER-Depressing an ENG FIRE switchlight

	Arms the fire-extinguishing system.
	Shuts off hydraulic fluid to the pump.
	All of the answers are correct.
	Trips the generator field relay.

HYDRAULIC POWER-Closing of a hydraulic firewall shutoff valve is indicated by

	A warning bell
	Illumination of the applicable F/W SHUTOFF annunciator.
	Illumination of the HYD PRESS ON annunciator.
	A warning horn.

HYDRAULIC POWER-If electrical power is lost, the hydraulic system bypass valve

	Spring loads to the open position.
	Spring loads to the closed position.
	None of the answers are correct.
	Is not affected.

LANDING GEAR-The landing gear uplocks are

	(D) Both A and B
	(B) Hydraulically disengaged.
	(C) Electrically actuated.
	(A) Mechanically held engaged by springs.

LANDING GEAR-The landing gear downlocks are disengaged by

	Mechanical linkage to the LDG GEAR handle.
	Hydraulic pressure being applied to the retract side of the actuators.
	Removing the external downlock pins.
	Action of the squat switches.

LANDING GEAR-The gear warning horn cannot be silenced when one or more gears are not locked down and.

	Flaps are extended beyond 15 degree position
	Either throttle is retarded below 70% turbine RPM.
	Airspeed is less than 150 KIAS
	Both throttles are retarded below 70% turbine RPM.

MASTER WARNING-The Rotary Test Switch is inoperative in flight..

	False
	True

MASTER WARNING-With the annunciators in the dimmed state (panel lights on),

	A new fault will illuminate bright until the Master Warning Switchlight is pressed.
	A new fault will illuminate in the dimmed state.
	Any annunciator will trigger the Master Warning.
	None of the answers are correct.

LIMITATIONS-The Maximum speed for autopilot operation is

	.60 Mach
	110 KIAS
	No Limit
	Vmo\Mmo

LIMITATIONS-The Maximum altitude for take-off and landing is

	9,000 ft
	14,000 ft
	No Limit
	10,000 ft

LIMITATIONS-For take-off and landing, the maximum water/Slush on runway is

	0.25 inch
	1.0 inch
	0.75 inch
	0.50 inch

LIMITATIONS-The Maximum temperature for take-off and landing is

	ISA +30 deg C
	ISA +39 deg C
	ISA +49 deg C
	ISA+10 deg C

LIMITATIONS-The Minimum temperature for take-off and landing is

	ISA-10 deg C
	ISA -54 deg C
	ISA -30 deg C
	ISA -39 deg C