HAWKER 700 SYSTEMS TEST

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AIR-CONDITIONING-The auxiliary heating valve must be closed for landing

	False
	True

AIR-CONDITIONING-The auxiliary heating valve must be closed for takeoff

	True
	False

ELECTRICAL-If all three generators are on line, and the bus tie contactor closed, the approximate load distribution will be

	One half the load will be on the left generator and the remaining one half split between the right and APU generator.
	Equal between all generators.
	Split between the main generators.
	One half the load will be on the left generator and one half will be on the APU generator.

ELECTRICAL-The maximum continuous (main engine) generator load limit is

	350 amps
	300 amps
	400 amps
	250 amps

ELECTRICAL-The No 1 transformer is powered by the

	XE bus
	PE bus
	XS2 bus
	XS1 bus

ELECTRICAL-With both main inverters operating, and the standby inverter switch in the ARMED position

	The No 1 inverter supplies the XS1 and XE buses.
	The No 1 inverter supplies the XS1, XS2 and XE buses.
	The No 1 inverter supplies the XS1 bus only.
	The standby inverter supplies the XE bus.

ELECTRICAL-With both main inverters operating, and with the standby inverter switch in the OFF position

	The No 2 inverter supplies the XS2 and XE buses.
	The No 1 inverter supplies the XS1 bus only.
	The No 1 inverter supplies the XS1 and XE buses.
	The No 1 inverter supplies the XS1, XS2 and XE buses.

FLIGHT CONTROLS-Concerning the rudder bias system, the actuators and solenoid valves are protected from icing by heating elements controlled by the_________ switches.

	PITOT/VANE Heat.
	Rudder bias.
	Engine anti-ice.
	APR

FUEL SYSTEM-During flight including take-off and landing, the maximum allowable difference in weight between the wing tanks is ________ pounds

	Varies with gross weight.
	500
	800
	400

FUEL SYSTEM-During refueling operations, an overpressure situation in excess of 45 psi will

	(B) Close all open refuel valves in the refuel system.
	(A) Close the MASTER REFUEL valve.
	(D) Both A and B are correct.
	(C) Close the shut-off valve in the refueling coupling.

FUEL SYSTEM-The boost pumps receive electrical power from the

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

FUEL SYSTEM-The electrical power for the fuel quantity indicators is supplied by the _____ bus.

	XE
	PE
	XS1
	PS1

FUEL SYSTEM-With only one fuel boost pump operating, the auxiliary fuel transfer to the wing tanks can take more than _____ minutes

	5
	18
	20
	10

HYDRAULIC-The purpose of the pressure-maintaining valve in the main hydraulic system is

	To maintain 2,300 psi in the main accumulator for operation of the landing gear.
	To maintain 2,300 psi in the main accumulator for normal brake operation.
	To maintain 2,300 psi in the main accumulator for operation of the emergency brakes.
	To maintain 2,450 psi in the main accumulator for normal brake operation.

HYDRAULIC-Which of the following hydraulic fluids are approved for use in the main and auxiliary systems

	DTD-585
	DTD-585B
	MIL-H-5606
	Any of the answers are correct.

ICE and RAIN-The rudder bias heat is activated by

	The ignition switches.
	The PITOT/VANE HEAT switches.
	The APR switch.
	The ENG A/ICE switches.

ICE and RAIN-The rudder bias strut heaters are powered from the ________ bus bar(s).

	PE
	PS1 and PS2
	PS1 and PS2 or PE
	XS1

LANDING GEAR and BRAKES-The green standby main gear down lights on the right console are powered by the

	PE2 bus
	PS1 bus
	PE bus
	PS2 bus

LIMITATIONS-The maximum Mach number with Mach Trim Off and auto-pilot not engaged is

	.73 IMN
	.68 IMN
	.78 IMN
	.80 IMN

MASTER WARNING SYSTEM-The MWS dimming circuit can be bypassed by

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

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

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

POWERPLANT-Engine synchronization will be available when selected and

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

POWERPLANT-The TFE731 combustor section is defined as a

	Reverse flow annular combustor.
	Can-annular combustor.
	Can-type combustor.
	Straight flow annular type.

PRESSURIZATION-The F/DK VLV switch is spring loaded from the OPEN to the STOP position

	True
	False

PRESSURIZATION-The function of the _____________ is to amplify control pressures from the pressure controller to the Outflow/Safety valves

	Outflow/Safety valves.
	Pneumatic Relays.
	Pressure regulator.
	Ram air valve