CITATION 550/551 SYSTEMS TEST

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AIR-CONDITIONING-In otherwise normal conditions and no action has been taken by the crew the EMER PRESS ON annunciator illuminates

	If on the ground the air to the ACM will be shutoff.
	All of the answers are correct.
	The ACM has overheated.
	If in the air, the cabin pressurization source will be emergency pressurization and the ACM has shutdown.

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

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

ELECTRICAL-The battery is automatically disconnected during an EPU (external power) start

	False
	True

ELECTRICAL-The battery is disconnected during an EPU (external power unit) start

	True
	False

ELECTRICAL-If one of the current limiters located between each main and the battery bus is blown before engine start

	(C) The will be no indication if external power is used for start.
	(B) The annunciator panel will not test properly.
	(A) The respective engine start sequence will be inoperative.
	(D) Both A and B.

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

	True
	False

ELECTRICAL-With an external power unit on line, the battery will receive a charge when

	The battery switch is in the EMER position
	All of the answers are correct
	The battery switch is in the BATT position
	The battery switch is in the OFF position

ELECTRICAL-If the BATT O'HEAT annunciator illuminates on the ground (except for test), you should

	Disregard if not flashing
	Switch generators to OFF
	Select battery switch to EMER and proceed as normal
	Not take-off until the proper maintenance procedures have been performed

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 proper pressure for the fire bottles can be determined by

	Assuring that at least one gauge reads at least 500 psi.
	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

FLIGHT CONTROLS-Regarding the control lock

	The airplane may not be towed with the control lock engaged.
	The engines may be started with the control lock engaged.
	If the nose wheel steering is damaged while towing, the airplane may still be flown.
	The flap selector cannot be moved with the control lock engaged.

FLIGHT CONTROLS-With the battery as the only source of power and the battery switch in EMER position

	The flaps are inoperable.
	The flap selector handle cannot by moved.
	The flaps can be lowered only.
	The flaps are operable.

FUEL SYSTEM-Maximum asymmetric fuel differential is

	100 gallons
	400 pounds
	600 pounds
	500 pounds

FUEL SYSTEM-With the respective fuel boost inoperative

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

HYDRAULIC POWER-Approved hydraulic fluids for this system are

	(D) Either A or B.
	(A) Skydrol 500a, b, b4, c, or ld-4
	(B) Hyjet, Hyjet W, III or IV
	(C) MIL-H-5606

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

	Is not affected.
	Nonel of the answers are correct.
	Spring loads to the open position.
	Spring loads to the closed position.

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

	All of the answers are correct
	The WINDSHIELD BLEED AIR valves should be partially closed to reduce air flow.
	The Windshield bleed air solenoid valve has been energized closed due to a bleed air temperature of above 146 degrees C.
	The light will extinguish when the temperate drops.

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.
	(B) The Windshield bleed air solenoid valve has been energized closed due to a bleed air temperature of above 146 degrees C.
	(C) The WINDSHIELD BLEED AIR valves should be partially closed to reduce air flow.
	(D) Both B and C.

ICE and RAIN-Engine bleed air is required for operation of the surface de-ice system

	True
	False

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

	True
	False

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.
	Nonel of the answers are correct
	A new fault will illuminate in the dimmed state.
	Any annunciator will trigger the Master Warning.

POWERPLANT-The oil temp range (degrees C) for takeoff is

	10 to red line
	0 to red line
	40 to 60
	40 to red line

PRESSURIZATION-If the main vacuum source to the pressurization controller is lost, the cabin pressure differential will

	Go to maximum differential allowed by the outflow valves.
	cause the oxygen mask to drop (if armed).
	Be controlled by the altitude limit valves.
	Decrease to zero

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

	False
	True

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

	ISA + 30 degrees C
	ISA + 35 degrees C
	ISA + 39 degrees C
	ISA + 45 degrees C