HAWKER 800XP SYSTEMS TEST

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AIR-CONDITIONING-As more air passes through the cooling turbine, the outlet air becomes hotter

	False
	True

ELECTRICAL-Control and operating power for the No 2 inverter is supplied from the

	PE bus
	PS2 bus
	No 3 battery
	PS1 bus

ELECTRICAL-The electrical power for windscreen heating is supplied by

	The windscreen transformer rectifier.
	A static inverter.
	Engine driven alternators.
	The engine driven generators.

ELECTRICAL-Which of the following statements are true regarding external battery charging:

	The EXTernal BATTery CHG switch should be selected to OFF when the indicated rates of charge is less than 5 amps.
	Charging will automatically cease if ground supply voltage become abnormal.
	Charging will automatically cease if a battery becomes hot.
	All of the answers are correct

FIRE PROTECTION-The detectors in each engine nacelle sends a signal to its respective

	Both red MWS lights
	ENG1 (or 2) FIRE warning light on the roof panel, respective red hp cock warning light and ENG FIRE repeater.
	All of the answers are correct
	The fire warning bell

FUEL SYSTEM-A fuel anti-icing additive is required for fuel temperatures below _______.

	-32 deg C.
	-32 deg F.
	-40 deg C.
	-40 deg F.

FUEL SYSTEM-The boost pumps receive electrical power from the

	Hot Battery Bus
	PE or PS1 and PS2
	XE
	PS1 and PS2

FUEL SYSTEM-The ventral tank may be gravity fueled.

	True
	False

HYDRAULIC-During preflight a minimum pressure of _________ psi on the emergency brake or main system accumulator is required to properly set the parking brake

	1,000
	950
	1,750
	2,300

HYDRAULIC-The auxiliary hydraulic reservoir quantity is

	6 U.S. pints
	2 U.S. pints
	4 U.S. pints
	7 U.S. pints

ICE and RAIN-If engine anti-ice is required, it should be switched on prior to setting take-off power.

	False
	True

ICE and RAIN-The cockpit windscreens (2) are _____ heated

	(C) Bleed air
	(A) Not
	(B) Electrically
	(D) Both B and C

ICE and RAIN-To avoid an airspeed restriction, the windscreen heat must be on for

	5 minutes with OAT below -10 degrees C, and 15 minutes with OAT below -20 degrees C.
	10 minutes with OAT above 21 degrees C, and 30 minutes with OAT below 21 degrees C.
	10 minutes with OAT above 15 degrees C, and 20 minutes with OAT below 15 degrees C.
	5 minutes with OAT above 15 degrees C, and 30 minutes with OAT below 15 degrees C.

LANDING GEAR and BRAKES-If the nose gear does not lock down during extension, the indication will be

	All three red annunciator lights on the annunciator panel are illuminated.
	The mechanical nose gear indicator on the right console is extended.
	The red N GEAR annunciator on the right console is illuminated.
	The red N GEAR light on the annunciator panel is on and the mechanical indicator on the pedestal is not extended.

LANDING GEAR and BRAKES-The main gear outer doors are

	Mechanically operated.
	Hydraulically operated.
	None of the answers are correct.
	Electrically operated.

LIMITATIONS-The maximum landing gear operating speed (Vlo) is

	175 KIAS
	220 KIAS
	210 KIAS
	160 KIAS

LIMITATIONS-The maximum speed with the flaps at 45 degrees is

	220 KIAS
	175 KIAS
	210 KIAS
	165 KIAS

MASTER WARNING SYSTEM-The master warning system is powered by the

	PS2 bus
	XE bus
	PE bus
	PS1 bus

PNEUMATICS-Electrical power for the HP BLEED on-off valves is supplied by the

	XE Bus.
	PE Bus.
	PS1 and PS2 bus respectively.
	PS2 Bus.

POWERPLANT-Engine synchronization will be available when selected and

	(B) The left engine fuel computer is operating.
	(A) Both fuel computer are operating normally.
	(C) The APR system is not armed.
	(D) Both A and C.

POWERPLANT-The ITT gauges receives electrical power from

	XE bus
	An additional inverter if the normal AC power system is not available.
	DC power system.
	XS1 and XS2 respectively.

POWERPLANT-To faciliatate an accurate setting of climb power a

	Green light in the ITT indicator illuminates.
	A green light in the N2 indicator illuminates.
	MWS annunciator illuminates.
	APR ARMED annunciator illuminates.

PRESSURIZATION-Power for the fan-operated venturi motor is furnished from the

	XS2 bus
	XS1 bus
	PE bus
	PS1 bus

PRESSURIZATION-The function of the fan-operated venturi in the pressurization system is to

	Determine reference pressure for the automatic controller.
	Provide a vacuum to hold the outflow valves open on the ground.
	Provide pre-pressurization prior to lift-off.
	Determine control pressure during the flight mode.

PRESSURIZATION-Which of the following statements are true concerning the cabin pressurization dump valve?

	The dump valve may be used to control pressurization should the normal and manual systems be ineffective.
	All of the answers are correct.
	The dump valve opening can be varied to any position between DUMP and SHUT.
	The dump valve lever must be fully in the DUMP position for the ram air valve to open.