HAWKER 700 SYSTEMS TEST

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AIR-CONDITIONING-Air from the auxiliary heating valve, when opened

	(C) Can provide emergency pressurization air.
	(D) Both A and C.
	(A) Bypasses all other air-conditioning ducts in the rear bay.
	(B) Supplies additional heated air to the pilots foot outlets only.

AIR-CONDITIONING-Air for heat exchanger cooling is achieved through

	A spring loaded inward opening relief door which allows air from the rear bay to enter if the dorsal intake becomes blocked.
	The dorsal intake duct by a fan driven by the cooling turbine while on the ground.
	The dorsal intake duct by ram air when airborne.
	Any of the answers are correct.

ELECTRICAL-The APU generator is cooled by

	Ram air
	Bleed air.
	External fan.
	Ambient air and integral fan.

ELECTRICAL-Failure of the No 1 inverter will result in

	Loss of power on the XS1 bus.
	Illumination of the XS1 FAIL annunciator.
	A supply to the XS1 bus from the XS2 bus.
	Standby inverter operation to power the XS2 bus.

ELECTRICAL-The electrical power for windscreen heating is supplied by

	An engine driven alternator.
	A static inverter.
	The engine driven generators.
	The windshield transformer rectifier.

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

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

FIRE PROTECTION-Select the correct statement concerning the REAR BAY O/HEAT annunciator

	It will illuminate if two or more of the six thermal switches in the rear bay senses an overheat condition.
	All of the answers are correct.
	If it illuminates it will trigger the red MWS indicators on the glare shield.
	It can be extinguished by depressing either red MWS indicator on the glare shield.

FLIGHT CONTROLS-Trim tab position indicators require electrical power

	True
	False

FUEL-Pressure refueling/defueling is prohibited with the APU running

	True
	False

FUEL-Maximum refuel rate is_____ US gal per minute

	55
	144
	60
	100

FUEL-With only one fuel boost pump operating, the auxiliary fuel will transfer to the wing tanks in approximately _____ minutes

	18
	20
	10
	5

FUEL-Each wing tank has a usable capacity of _______ U.S. gallons

	635
	612.5
	600
	700

HYDRAULIC-The main hydraulic reservoir is located in the rear bay

	False
	True

HYDRAULIC-The HYD SYS O/HEAT illuminates when

	Fuel/oil cooler is malfunctioning.
	Reservoir fluid temperature reaches 90 degrees C.
	Pump inlet fluid temperature reaches 90 degrees C.
	Return fluid temperature reaches 90 degrees C.

ICE AND RAIN-The deicing fluid pump is powered by the _____ bus

	PE
	PS1
	PE2
	PS2

ICE AND RAIN-There will be no engine performance lost if airframe deicing is used for takeoff

	True
	False

LANDING GEAR AND BRAKES-During emergency brake operation, before selecting emergency brakes, anti-skid (maxaret) protection is available

	False
	True

LIMITATIONS-The maneuvering speed (Va) is

	182 KIAS
	192 KIAS
	M 0.66
	175 KIAS

MWS-To extinguish an illuminated roof panel annunciator

	Position the DIM O/RIDE switch to NORM.
	The fault must be corrected.
	Press the look up annunciator.
	Press either red MWS glareshield annunciator.

MWS-The MWS dimming circuit can be bypassed by

	Press the ANN DIM FAIL light capsule.
	Positioning the MWS dimmer switch fully clockwise.
	Positioning the DIM O/RIDE switch to O/RIDE.
	Positioning the DIM O/RIDE switch to NORM.

POWERPLANT-The automatic performance reserve system (APR) when armed will provide

	Increased take-off thrust during high-altitude, hot day operation.
	Maximum continuous thrust if N2 differential is 5 % or more.
	Automatic thrust increase if both fuel computers fail during take-off.
	Increased thrust if N2 differential is 5%.

POWERPLANT-Engine cranking is provided by a

	Pheumatic starter.
	Starter-generator through the accessory gearbox.
	Starter-generator through the planetary gearbox.
	DC starter motor through the transfer gearbox.

PRESSURIZATION-The ram air valve opening can be varied (stopped) to any position between open and closed

	False
	True

PRESSURIZATION-Select the correct statements concerning the DUMP VALVE lever

	(D) Both B and C.
	(B) It electrically controls the ram air valve.
	(C) It manually controls the dump valve.
	(A) It electrically controls the dump valve.

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

	PE bus
	XS1 bus
	XS2 bus
	PS1 bus