HAWKER 800XP SYSTEMS TEST

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AIR-CONDITIONING-Air conditioning is available on the ground, provided

	Either or all of the answers are correct.
	The left engine is running and the left MAIN AIR VALVE switch is in the OPEN position.
	The APU is running and the APU AIR switch is in the OPEN position.
	The right engine is running and the right MAIN AIR VALVE switch is in the OPEN position.

AIR-CONDITIONING-The auxiliary heating valve is controlled by the

	MAIN AIR VALVE switch.
	Temperate switch in the main duct.
	Automatic temperature controller.
	F/DK VLV switch.

AIR-CONDITIONING-Warm air is routed from the primary heat exchanger via a Low Limit Temperature Valve to the inlet of the water seperator when

	Warmer is selected from the cockpit.
	Water seperator inlet air temperature falls to approximatley 0 degrees C.
	Water seperator inlet air temperatue falls to approximatley 2 degrees C.
	Engine A/ICE is selected.

ELECTRICAL-On aircraft with nickel-cadmium batteries, the electrical rating for each main battery is

	30 volts, 24 ampere-hours
	24 volts, 23 ampere-hours
	23 volts, 34 ampere-hours
	28 volts, 23 ampere-hours

ELECTRICAL-The electrical rating for the standby inverter is

	250 va
	125 va
	2,500 va
	1,250 va

ELECTRICAL-Which of the following statements are true regarding the bus-tie contactor.

	The bus tie contactor fails to the closed position.
	The bus tie is automatically opened by a BATT O'HEAT annunciator illumination.
	The bus-tie contactor can be opened manually by positioning the bus tie switch to OPEN.
	The bus tie is automatically opened by a BATT HOT annunciator illumination.

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

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

FLIGHT CONTROLS-Select the correct statement, With the PE bus only powered (double generator failure).

	The only stall warning will be the illumination of the IDNT 3 light.
	The stick pusher will be operative.
	The stick shaker will be operative.
	The stall warning and identification system will operate normally.

FUEL SYSTEM-Fuel carried in the ventral tank must be transferred into the wing tanks when the fuel level in the wing tanks fall to __________ pounds.

	3,300
	3,600
	2,500
	3,000

FUEL SYSTEM-If during normal pressure refueling, an overflow condition exists the MASTER REFUEL VALVE will CLOSE

	True
	False

FUEL SYSTEM-To feed both engines from the right tank, the right boost pump must be operative

	False
	True

HYDRAULIC-The first step in operating the auxiliary hydraulic system is

	Operate the auxiliary hand pump.
	Dump main system pressure.
	Check the Main system pressure is 1,000 psi or below.
	Pull the AUX HYD SYS PULL lever.

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

	True
	False

ICE and RAIN-There will be no engine performance lost if engine anti-icing is used for takeoff

	False
	True

ICE and RAIN-With PS1 failure and PS2 powered the left Rudder Bias Strut will not be heated

	True
	False

LANDING GEAR and BRAKES-The landing gear lever lock solenoid powered by the _____ bus

	PE
	PE2
	PS2
	PS1

LIMITATIONS-The maneuvering speed (Va) is

	196 KIAS
	M 0.66
	182 KIAS
	175 KIAS

LIMITATIONS-The minimum zero fuel weight is

	13,200 lbs.
	14,120 lbs.
	13,100 lbs.
	12,100 lbs.

MASTER WARNING SYSTEM-The red glareshield MWS annunciators will illuminate flashing if

	A red annunciator illuminates.
	Any annunciator on the roof panel illuminates.
	It is pressed.
	If both generators fail.

POWERPLANT-Select the correct statement(s) concerning the automatic performance reserve system (APR)

	The APR O/RIDE switch must be depressed for takeoff.
	The synchronizer controller must be operational for APR operation.
	If electrical power is lost to the APR controller, APR will not be available.
	If operational, except for crew training flights, the APR system must be ARMED for takeoff.

POWERPLANT-The HP spool of the TFE731 engine consists of

	Three radial compressor stages and four axial turbine stages.
	A two-stage axial compressor and a two stage radial turbine.
	One axial compressor stage and one radial turbine stage.
	A single-stage centrifugal compressor and a single-stage axial turbine.

POWERPLANT-To faciliatate an accurate setting of climb power a

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

PRESSURIZATION-Holding the F/DK VLV to the OPEN position fully opens the valve in approximately

	10 seconds.
	20 seconds.
	5 seconds.
	30 seconds.

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

	False
	True

FUEL SYSTEM-The Aux Fuel Transfer valve is electrically operated.

	True
	False