HAWKER 700 SYSTEMS TEST
First name:   Last name:  
E Mail:   Affiliate:  
1
AIR-CONDITIONING-Air from the auxiliary heating valve, when opened
2
AIR-CONDITIONING-Air for heat exchanger cooling is achieved through
3
ELECTRICAL-The APU generator is cooled by
4
ELECTRICAL-Failure of the No 1 inverter will result in
5
ELECTRICAL-The electrical power for windscreen heating is supplied by
6
ELECTRICAL-Which of the following statements are true regarding external battery charging
7
FIRE PROTECTION-Select the correct statement concerning the REAR BAY O/HEAT annunciator
8
FLIGHT CONTROLS-Trim tab position indicators require electrical power
9
FUEL-Pressure refueling/defueling is prohibited with the APU running
10
FUEL-Maximum refuel rate is_____ US gal per minute
11
FUEL-With only one fuel boost pump operating, the auxiliary fuel will transfer to the wing tanks in approximately _____ minutes
12
FUEL-Each wing tank has a usable capacity of _______ U.S. gallons
13
HYDRAULIC-The main hydraulic reservoir is located in the rear bay
14
HYDRAULIC-The HYD SYS O/HEAT illuminates when
15
ICE AND RAIN-The deicing fluid pump is powered by the _____ bus
16
ICE AND RAIN-There will be no engine performance lost if airframe deicing is used for takeoff
17
LANDING GEAR AND BRAKES-During emergency brake operation, before selecting emergency brakes, anti-skid (maxaret) protection is available
18
LIMITATIONS-The maneuvering speed (Va) is
19
MWS-To extinguish an illuminated roof panel annunciator
20
MWS-The MWS dimming circuit can be bypassed by
21
POWERPLANT-The automatic performance reserve system (APR) when armed will provide
22
POWERPLANT-Engine cranking is provided by a
23
PRESSURIZATION-The ram air valve opening can be varied (stopped) to any position between open and closed
24
PRESSURIZATION-Select the correct statements concerning the DUMP VALVE lever
25
PRESSURIZATION-Power for the fan-operated venturi motor is furnished from the
 
   
Copyright 2000-2007 by S2 Software, all rights reserved