CITATION 500/501 SYSTEMS TEST

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ELECTRICAL-The electrical source for the entrance door flood light is

	The hot battery bus.
	LH main bus.
	The emergency batteries.
	Battery bus.

ELECTRICAL-Which of the following statements are true regarding a generator-assist start.

	The battery is automatically disconnected during a generator .assisted start
	A generator assisted counts as 1/3 of a battery start.
	The turbine RPM for the engine providing the assist needs to be above 50%.
	Providing the opposite generator is on line, a starter assisted air start is a generator assisted start.

ELECTRICAL-The left or right power relay is opened by

	A reverse current of (10% of total load).
	Undervoltage.
	All of the answers are correct.
	Placing the generator switch to OFF.

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

	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.
	If selected inverter fails the remaining inverter assumes its load.
	Inverter 1 and inverter 2 share the load equally.

ELECTRICAL-With the battery switch selected to EMER a good battery should supply power to the hot battery and emergency buses for approximately

	30 minutes.
	1 hour.
	55 minutes.
	25 minutes.

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

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

ELECTRICAL-The emergency bus is powered when

	The hot battery bus is powered
	The battery switch is in the OFF position
	The generators are on line regardless of the battery switch position
	The battery switch is not in the OFF position

ELECTRICAL-Continuous ground operation of the starter-generator above ______amps is prohibited

	325
	400
	300
	150

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 lights in the BOTTLE ARMED switchlights are tested by

	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.
	Rotary test switch to the ANNU position.

FLIGHT CONTROLS-The flaps are actuated by

	One AC electric motor.
	One DC electric motor.
	Hydraulic pressure.
	Two DC motors.

HYDRAULIC POWER-The wheel brake hydraulic system is independent of the main hydraulic system.

	True
	False

HYDRAULIC POWER-Depressing an ENG FIRE switchlight

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

HYDRAULIC POWER-Hydraulic system operation is indicated by illumination of the

	None of the answers are correct.
	HYD LEVEL LO annunciator.
	HYD PRESS ON annunciator.
	L or R HYD PRESS LO annunciator.

ICE and RAIN-The windshield alcohol system quantity gage

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

ICE and RAIN-Regarding the P/S HTR OFF light

	Illumination of the light could indicate loss of electrical power to one of the pitot tubes.
	It will illuminate if the PITOT&STATIC switch is OFF.
	If power is lost to both the static ports on the pilots system, the light will illuminate.
	All of the answers are correct

ICE and RAIN-Switching on both engine anti-ice systems in flight will increase the reading on each ammeter by

	10 amps
	20 amps
	120 amps
	5 amps

ICE and RAIN-With the engine operating the T 1 probe is heated continuously

	False
	True

LANDING GEAR-The purpose of the fusible plug incorporated in each main gear wheel is to

	Deflate the tire by melting in case of an overheated brake.
	Release pressure if the tire is overserviced.
	Deflate the tire if the maximum tire speed is exceeded.
	Deflate the tire in case of hydroplaning.

LANDING GEAR-In flight, when the LDG GEAR handle is positioned UP or DOWN.

	The hydraulic bypass valve is not affected.
	The hydraulic bypass valve is energized closed.
	The hydraulic bypass valve is energized open.
	The HYD PRESS ON annunciator light extinguishes.

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.

MASTER WARNING-The Master Warning Lights illuminate and flash when

	(D) Both A and C
	(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.

LIMITATIONS-Maximum speed with flaps fully extended is

	202 KIAS
	176 KIAS
	150 KIAS
	160 KIAS

LIMITATIONS-The Maximum tire speed is

	165 knots
	185 knots
	175 knots
	155 knots

LIMITATIONS-The Maximum demonstrated crosswind component is

	25 knots
	35 knots
	30 knots
	25 mph