CITATION 500/501 SYSTEMS TEST

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AIR-CONDITIONING-The source of bleed air for emergency pressurization is

	Right engine.
	Both engines.
	Left engine.
	The engine producing the most power.

AIR-CONDITIONING-The AIR DUCT O'HEAT annunciator light illuminates when the

	Temperate of the air in the duct to the cabin is excessive.
	Temperate of the air going to the windshield is excessive.
	Aircycle machine shuts down.
	EMER source is selected.

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

	True.
	False.

ELECTRICAL-In flight with both generators on line the battery is isolated from any charging source when

	The battery switch is not in the BATT position.
	The battery switch is in the EMER position only.
	The battery switch is in the OFF position only.
	The battery switch is in the BATT position.

ELECTRICAL-On UNs 275 and above, which of the following statements are true.

	Inverter 1 and inverter 2 share the load equally.
	If selected inverter fails the remaining inverter assumes its load.
	If selected inverter fails, the remaining inverter must be selected to assume the ac load.
	If selected inverter fails the red AC FAIL will illuminate flashing.

ELECTRICAL-An EPU (external power unit) should not be connected with the unit turned off

	False.
	True.

ELECTRICAL-The voltmeter is inoperative when the battery switch is

	In the OFF position
	In the OFF or EMER position
	In the BATT position
	In the EMER position

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

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

FIRE PROTECTION-The ENG FIRE switchlight illuminates when

	The firewall shutoff valve is closed.
	The fire extinguisher is discharged.
	It is depressed.
	An engine fire or overheat condition exists.

FIRE PROTECTION-The proper pressure for the fire bottles can be determined by

	Assuring that at least one gauge reads at least 500 psi.
	Use the formula PRESS X TEMP divided by 80
	Use the adjacent chart to correct pressure gauge reading for pressure altitude.
	Use the adjacent chart to correct pressure gauge reading for temperature.

FUEL SYSTEM-If fuel crossfeed has been selected and normal DC electrical power is lost

	The boost pump for the tank the fuel being crossfed from will be powered be the hot battery bus.
	The motive flow valve will fail open
	The crossfeed valves will fail closed.
	The boost pumps will be energized.

FUEL SYSTEM-Which of the following statements are true, regarding the Fuel System.

	The fuel filters must be inspected prior to the next flight if the FUEL FILT BYPASS annunciator illuminates.
	The fuel boost pump switches should be set to the ON position for take-off and landing.
	The respective engine should be shut down if the FUEL FILT BYPASS annunciator illuminates.
	In the event of DC power loss, the primary ejector pump ceases to operate and the engine flames out.

FUEL SYSTEM-The fuel boost pump switches must be in the NORM position for crossfeed

	False
	True

FUEL SYSTEM-With the respective fuel boost inoperative

	The engine will flameout if running.
	The engine will flameout if the primary ejector pump becomes clogged.
	All of the answers are correct.
	The engine will not start.

HYDRAULIC POWER-With the loss of the main hydraulic system the

	Wheel brakes will not be effected.
	The speedbrakes cannot be retracted.
	Normal wheel brakes will be lost.
	The flaps will be inoperative.

ICE and RAIN-The windshield alcohol system quantity gage

	Is located in the LH NOSE baggage compartment.
	Is inoperative with loss of normal DC power.
	Is located on the copilots instrument panel.
	Is located in the RH NOSE baggage compartment.

ICE and RAIN-Which is the correct statement concerning the surface DE-ICE system

	(B) It should not be activated if OAT is suspected to be below -40 degrees C.
	(D) Both B and C
	(C) Should not be activated until ice accumulation reaches 1/2 inch.
	(A) It should be activated prior to entering icing conditions.

ICE and RAIN-If the W/S AIR O'HEAT annunciator illuminates with the W/S BLEED switch in the ON position.

	(A) The pressure in the duct has exceeded 5 psi, indicating a partially opened or leaking Windshield bleed air solenoid valve.
	(C) The WINDSHIELD BLEED AIR valves should be partially closed to reduce air flow.
	(D) Both B and C
	(B) The Windshield bleed air solenoid valve has been energized closed due to a bleed air temperature of above 146 degrees C.

LANDING GEAR-While actuating the emergency brakes you should

	Apply pedal brakes for directional control.
	None of the answers are correct.
	Pump the emergency brake handle to build up pressure.
	Not apply pedal brakes as it could rupture the brake reservoir..

LANDING GEAR-Prior to towing

	The downlock pins must be inserted in the landing gear.
	The downlock pin must be in the nose gear only.
	The control lock must be disengaged.
	The control lock must be engaged.

LANDING GEAR-The landing gear uplocks are

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

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

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

PRESSURIZATION-Illumination of the CAB ALT 10,000 FT annunciator

	(A) Indicates that the cabin altitude is above 10,000 feet.
	(B) Will trigger the MASTER WARNING light and it cannot be cancelled.
	(D) Both A and C
	(C) Will activate the cabin altitude warning horn.

PRESSURIZATION-Pressurization of the cabin is normally maintained by

	(C) Modulating the cabin temperature.
	(A) Controlling the amount of air entering the cabin.
	(B) Controlling the amount of air leaving the cabin.
	(D) Both A and B

PRESSURIZATION-Loss of normal DC power will cause the Cabin differential pressure to go to Maximum differential.

	True
	False