CITATION V, 560 SYSTEMS TEST

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

	True
	False

FIRE PROTECTION-The ENG FIRE switchlight illuminates when

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

FIRE PROTECTION-The fire extinguishing agent in the engine fire bottles is

	Halon
	Oxygen
	CBrF3
	Co2

FIRE PROTECTION-The fire detection and extinguishing system receives electrical power from the emergency DC bus

	False
	True

FIRE PROTECTION-During preflight, the indication that a fire extinguisher bottle has been discharged

	Residue in the engine inlet.
	Gauge on the fire bottle.
	Blow out disc missing on the side of the tail cone.
	Annunciator light in the cockpit.

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

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

FIRE PROTECTION-The lights in the BOTTLE ARMED switchlights are tested by

	Rotary test switch to the ANNU position.
	Rotary test switch to the FIRE WARN position.
	There is no test other than closing the firewall shutoff valve to arm the fire bottles.
	Push to test.

FIRE PROTECTION-The fire detection and extinguishing system receives electrical power from the hot battery bus

	True
	False

FIRE PROTECTION-The fire extinguishing agent in the engine fire bottles is

	Not pressurized.
	Pressurized to 500 psi at 70 degrees F.
	Pressurized to 600 psi at 50 degrees C
	Pressurized to 600 psi at 70 degrees F

FLIGHT CONTROLS-The speedbrakes are held in the extended position by

	Trapped hydraulic pressure.
	Springs.
	Hydraulic system remains pressurized.
	Mechanical locks.

FLIGHT CONTROLS-The trim tab position indicators are inoperative with the battery switch in the EMER position.

	False
	True

FLIGHT CONTROLS-Which statement is true regarding the rudder, elevator and aileron trim tabs

	The rudder tab is a servo tab.
	All are electrically and mechanically actuated.
	There are two aileron trim tabs.
	All have electrical tab position indicators.

LANDING GEAR-While in the air, the LDG GEAR handle cannot be lowered if electrical power is lost

	False
	True

LANDING GEAR-The landing gear uplocks are

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

LANDING GEAR-The landing gear downlocks are disengaged by

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

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

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

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

MASTER WARNING-With the battery as the only source of power, the annunciators are operative when the battery switch is in the EMER position

	True
	False

MASTER WARNING-An annunciator light when illuminated, will extinguish when

	The rotary test switch is reset to OFF.
	The Master Warning Switchlight is depressed.
	The fault is corrected.
	The annunciator is depressed.

MASTER WARNING-The Master Warning Lights illuminate and flash when

	(A) A red annunciator, with the exception of ENG FIRE illuminates.
	(C) Both amber L and R GEN OFF annunciators illuminate.
	(B) An Amber annunciator illuminates.
	(D) Both A and C.

MASTER WARNING-The annunciator lights intensity is varied by the center panel lights rheostat.

	False
	True

MASTER WARNING-The annunciator lights intensity is controlled by the

	The panel lights control switch.
	Center panel lights rheostat.
	Left panel lights rheostat.
	The navigation light switch.

MASTER WARNING-The red light above the Rotary Test Switch illuminates when

	The switch is out of the OFF position.
	When test switch is in the ANNU position.
	Power is available to the switch.
	When the panel light control switch is in the on position.

POWERPLANT-The N1 tape recieves power from the Emergency bus.

	False
	True