HAWKER 800 SYSTEMS TEST

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AIR-CONDITIONING-The duct temperature limiter is inoperative when the CABIN TEMP selector is in the MANUAL position.

	False
	True

AIR-CONDITIONING-To prevent cabin pressurization while using ground Air-conditioning, you should

	Assure either a DV window or the door is open.
	Assure the PRESSN GEAR switch is in the O/RIDE position.
	Assure the PRESSN GEAR switch is in the AUTO position.
	Assure the outflow valves are closed.

AIR-CONDITIONING-The cooling turbine requires______________for proper operation

	Bleed air
	AC power
	Ram air
	DC power

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

	The bus tie is automatically opened by an undervoltage condition on the main bus bar.
	The bus tie is automatically opened by an overvoltage condition on the main bus bar.
	The bus-tie contactor can be manually opened by positioning the bus tie switch to OPEN.
	All of the answers are correct.

ELECTRICAL-Either of the 3 constant frequency inverters are capable of supplying all essential AC power requirements

	True
	False

ELECTRICAL-If one of the 500A feeder cable current limiters were to blow in flight, the indication would be

	Illumination of the respective GEN FAIL annunciator.
	If selected, the respective battery voltmeter would read less than bus voltage (battery not being charged).
	Illumination of the BATTERY NO CHG annunciator.
	Illumination of the BUS TIE OPEN annunciator.

FIRE PROTECTION- The engine fire warning bell can be silenced by

	Firing Extinguisher Shot 1.
	Depressing the respective BELL CNCLD switchlight.
	Selecting the respective HP cock to SHUT.
	Selecting the respective LP cock to SHUT.

FIRE PROTECTION- Power for both fire extinguisher SHOT 2 circuits is supplied by bus bar ____.

	PE2
	PS2
	PS1
	PE

FLIGHT CONTROLS - The electric elevator trim system must be on and operable for takeoff.

	False
	True

FLIGHT CONTROLS - In flight, if one Rudder Bias strut has failed or is isolated, the Vmca is ________KIAS.

	145
	112
	125
	115

FUEL SYSTEM - The wing tanks must be fueled to full if fuel is carried in the ventral tank.

	False
	True

HYDRAULIC POWER - The AUX HYD LO LEVEL illuminates when

	None of the answers are correct.
	The auxiliary reservoir quantity is reduced by 1 pint or more.
	The auxiliary reservoir quantity is reduced by 1/2 pint or more.
	Pressure in the auxiliary system has dropped to below 1,000 psi.

HYDRAULIC POWER - The main hydraulic reservoir capacity is _______.

	Either or all of the answers are correct
	2.4 U.S gallons
	2 imperial gallons
	9.1 liters

HYDRAULIC POWER - Select the correct statement(s) concerning the pressure filter

	All of the answers are correct.
	The filter will not bypass if it becomes clogged.
	The pressure filter is common to both engine driven pumps.
	A button on top of the filter protrudes if the filter becomes restricted sufficiently to cause a pressure drop between inlet and outlet pressures.

ICE AND RAIN - The ambient temperature will determine the electrical load (amps) for pitot heaters.

	True
	False

ICE AND RAIN - If the aircraft is cold soaked below -10 degrees C and the time requirement for windscreen heat on is not met, then a speed restriction of __________ is required.

	230 KIAS until an altitude of 6,000 feet.
	210 KIAS until an altitude of 10,000 feet.
	250 KIAS until an altitude of 10,000 feet.
	257 KIAS below 8,000 feet.

ICE AND RAIN - The cockpit forward side windows are _____ heated

	Radiant.
	Bleed air
	Electrically
	Not

LIMITATIONS - Both crew seats shall be locked in the__________ position for Take-off and Landing.

	Fore or Aft
	Aft
	Fore
	Fore and Aft

LIMITATIONS - The maximum speed with the flaps at 15 degrees is

	220 KIAS
	175 KIAS
	160 KIAS
	210 KIAS

MASTER WARNING - If the ANN DIM FAIL annunciator illuminates

	The DIM O/RIDE switch should be set to DIM OVRD.
	No action required.
	There is a new fault on the overhead panel.
	You should press the ANN DIM FAIL light.

MASTER WARNING - What do white annunciators indicate?

	Associated system malfunction.
	A system failure.
	Associated system is inoperative.
	Completed operations and system status.

POWERPLANT - Select the correct statement (s) concerning the �ENG 1 CMPTR� or �ENG 2 CMPTR� annunciators

	It will illuminate steady when the associated engines fuel computer has failed.
	It will illuminate steady when the associated engines control switch is moved to the OFF or OVSD PROT position.
	All of the answers are correct.
	It will blink continuously when the function select on the respective DEEC is not set to position 1.

POWERPLANT - The electrical source for the oil pressure indicators is

	Battery.
	115 volt AC inverter.
	DC power system.
	6 volt AC transformer.

PRESSURIZATION SYSTEM - The CABIN ALTITUDE warning horn, when activated, cannot be cancelled until the cabin altitude is reduced

	True
	False

PRESSURIZATION SYSTEM - The MANUAL CABIN ALTITUDE CONTROL knob and GROUND TEST VALVE lever is effective only if the automatic controller fails

	False
	True