HAWKER 800 SYSTEMS TEST
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1
AIR-CONDITIONING-The duct temperature limiter is inoperative when the CABIN TEMP selector is in the MANUAL position.
False
True
2
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.
3
AIR-CONDITIONING-The cooling turbine requires______________for proper operation
Bleed air
AC power
Ram air
DC power
4
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.
5
ELECTRICAL-Either of the 3 constant frequency inverters are capable of supplying all essential AC power requirements
True
False
6
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.
7
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.
8
FIRE PROTECTION- Power for both fire extinguisher SHOT 2 circuits is supplied by bus bar ____.
PE2
PS2
PS1
PE
9
FLIGHT CONTROLS - The electric elevator trim system must be on and operable for takeoff.
False
True
10
FLIGHT CONTROLS - In flight, if one Rudder Bias strut has failed or is isolated, the Vmca is ________KIAS.
145
112
125
115
11
FUEL SYSTEM - The wing tanks must be fueled to full if fuel is carried in the ventral tank.
False
True
12
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.
13
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
14
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.
15
ICE AND RAIN - The ambient temperature will determine the electrical load (amps) for pitot heaters.
True
False
16
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.
17
ICE AND RAIN - The cockpit forward side windows are _____ heated
Radiant.
Bleed air
Electrically
Not
18
LIMITATIONS - Both crew seats shall be locked in the__________ position for Take-off and Landing.
Fore or Aft
Aft
Fore
Fore and Aft
19
LIMITATIONS - The maximum speed with the flaps at 15 degrees is
220 KIAS
175 KIAS
160 KIAS
210 KIAS
20
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.
21
MASTER WARNING - What do white annunciators indicate?
Associated system malfunction.
A system failure.
Associated system is inoperative.
Completed operations and system status.
22
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.
23
POWERPLANT - The electrical source for the oil pressure indicators is
Battery.
115 volt AC inverter.
DC power system.
6 volt AC transformer.
24
PRESSURIZATION SYSTEM - The CABIN ALTITUDE warning horn, when activated, cannot be cancelled until the cabin altitude is reduced
True
False
25
PRESSURIZATION SYSTEM - The MANUAL CABIN ALTITUDE CONTROL knob and GROUND TEST VALVE lever is effective only if the automatic controller fails
False
True
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