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WorksheetsA320 SYSTEMS TEST
Total questions: 79
Worksheet time: 22mins
Name
Class
Date
1.
The temperature selection range is from
a)
10°C to 35°C
b)
18°C to 30°C
c)
12°C to 28°C
d)
15°C to 32°C
2.
After the engine start, the Pack Flow Control Valves automatically open, however on the ground, reopening of the valves is delayed for ______________ after the first engine start
a)
30 seconds
b)
45 seconds
c)
60 seconds
d)
15 seconds
3.
During flight below ___________, the Ram Air Valve can provide an emergency source of conditioned air during non-pressurized flight.
a)
10,000 feet
b)
15,000 feet
4.
When the aircraft is parked and the packs are not operating, ______________ conditioned air may be supplied directly to the mixing unit by a ground connection.
a)
high pressure
b)
low pressure
5.
Each Pack Flow Control Valve is ___________-operated and ____________-controlled
a)
pneumatically ; electrically
b)
electrically ; electrically
c)
electrically ; pneumatically
d)
hydraulically ; electrically
6.
How many slat segments are installed on the leading edge of each wing?
a)
3
b)
6
c)
2
d)
5
7.
Which of the secondary flight controls can be mechanically operated?
a)
Spoilers
b)
High Lift Devices
c)
THS
d)
Ailerons
8.
A ________ light may be used to advise the crew of a temporary system operation, such as when the APU is available.
a)
green
b)
white
c)
amber
d)
blue
9.
What are the names of the control laws that are used to operate the flight controls?
a)
Normal, Initial, Abnormal
b)
Normal, Alternate, Direct
c)
Normal, Back-up, Cable
d)
Fast, Medium, Slow
10.
The aircraft is equipped with ________ hydraulic systems.<br /><br />
a)
3
b)
2
c)
4
d)
5
11.
The APU is located in the ___________________ of the aircraft.
a)
unpressurized tailcone
b)
pressurized tailcone
12.
When the APU BLEED switch is ON and bleed air is available, the APU bleed valve will open and the APU AVAIL memo is replaced with ______________.
a)
APU RUN
b)
APU BLEED
13.
The APU GEN pushbutton switch is located on the Electrical Panel and is normally in the ON position.
a)
true
b)
False
14.
During APU start, when the RPM of the APU reaches about ____, the blue ON light in the APU START switch will extinguish and the green AVAIL light will come on.
a)
0.65
b)
0.75
c)
0.95
d)
0.85
15.
Can APU bleed air be used for supplying the packs during takeoff?
a)
Yes
b)
No
16.
After takeoff, an AP can be engaged when above ______ AGL and can remain engaged until the completion of the AUTO LAND rollout.<br /><br />
a)
500’
b)
50’
c)
1000’
d)
100’
17.
During manual flight with A/THR in the SPEED mode, the pilot must manually move the thrust levers to IDLE during the flare. As a crew reminder, a “RETARD” automatic call is provided at ____ AGL.
a)
50’
b)
20’
c)
100’
d)
200’
18.
The OP CLB mode is a _________ mode that commands a climb to the FCU altitude without regard to the computed FMS profile.
a)
Managed
b)
Selected
19.
The “managed” mode that provides lateral guidance along the F-PLN is the _______ mode.
a)
NAV
b)
ROUTE
20.
During A/THR operations, if the pilot needs additional thrust at any time, movement of the thrust levers forward of the ___________ allows manual thrust control.
a)
CLB detent
b)
IDLE detent
21.
When the Speed is in a “selected” mode, the speed target selected on the FCU is displayed in _______ on the PFD.
a)
Green
b)
Magenta
c)
Blue
22.
When the aircraft reaches the CRZ FL as set on PROG page, the AP/FD goes into the _____________ mode.
a)
SRS
b)
ALT CRZ
23.
An Emergency Evacuation system alert can be activated from the Flight Deck or the Cabin. <br />The Flight Deck EVAC controls are located on ______________.<br />
a)
the pedestal
b)
the overhead panel
c)
the center instrument panel
24.
The Flight Crew can call the F/A Stations or the Ground Crew by use of Pushbuttons on the ______________.
a)
CALLS panel
b)
RMP
25.
The cockpit recording system stops automatically ____ minutes after the second engine shutdown.
a)
10
b)
5
c)
2
d)
3
26.
The PA Reception Key is always selected on __________ to record cabin announcements.
a)
ACP 2
b)
ACP 3
c)
ACP 1
27.
The COCKPIT CALL buzzer stops when the button is released, and the call lights will go out in ___________ if they are not first reset by pushing the RESET button.
a)
60 seconds
b)
30 seconds
c)
90 seconds
28.
If the APU generator is selected ON, it _________ take over until the other equipment (EXT PWR, engines) is removed.
a)
will
b)
will not
29.
Any one generator is capable of supplying all essential AC power to the aircraft.
a)
true
b)
false
30.
On the ECAM, the __________ indications show items that are not powered, _________ items are powered, and arrows show the direction of current flow.<br /><br />
a)
green ; amber
b)
red ; blue
c)
green ; blue
d)
amber ; green
31.
The three AC generators are each rated at ______________.
a)
400 KVA
b)
30 KVA
c)
90 KVA
d)
20 KVA
32.
When the APU generator comes online, it automatically disconnects the external power.
a)
true
b)
false
33.
For DC power, there are 2 normal TR’s and ________ for Essential Power.
a)
1 TR
b)
2 TR's
34.
The Emergency Generator is driven by hydraulic pressure from the ________ hydraulic system.
a)
green
b)
red
c)
blue
35.
How many smoke detector(s) are installed in each lavatory?
a)
One
b)
Two
36.
How many smoke detector(s) are located in the avionics bay, and where is(are) they located?
a)
Two, extraction duct
b)
One, extraction duct
c)
Three, blower duct
37.
Does automatic APU fire extinguishing occur on the ground?
a)
Yes
b)
No
38.
The APU FIRE Light will illuminate __________ and an external warning horn sounds when an APU Fire is detected.
a)
Amber
b)
Red
39.
How many fire extinguishing bottles are available for each engine?
a)
2
b)
3
c)
1
40.
If the pilot holds full lateral side stick, the angle of bank will increase and maintain _____________.
a)
45 degrees
b)
67 degrees
c)
80 degrees
41.
There are ______ Slat surfaces on the leading edge of the wing and ______ Flap sections on the trailing edge
a)
Six; three
b)
Four ; two
c)
Five ; two
42.
The Load Factor Limitation in Alternate Law is similar to that under Normal Law.
a)
true
b)
False
43.
On the PFD, two sets of green parallel dash symbols display the pitch attitude protection limits for _______ nose up and _______nose down.
a)
30 degrees ; 15 degrees
b)
30 degrees ; 30 degrees
c)
45 degrees ; 30 degrees
44.
During flight, which of the five spoiler panels operate as speedbrakes?
a)
2 outboard panels (4, 5)
b)
2 inboard panels (1, 2)
c)
3 center panels (2, 3, and 4)
45.
Normal Law has three modes for three phases of flight. <br />These modes are<br />
a)
GROUND, FLIGHT, TAKEOFF
b)
GROUND, FLIGHT, FLARE
c)
GROUND, FLIGHT, CLIMB
46.
There are three Flight Control Laws that are used by the EFCS; these Laws are Normal, Alternate, and Standby.
a)
true
b)
false
47.
Which fuel tank normally provides fuel to the APU?
a)
right
b)
center
c)
left and right
d)
left
48.
The wing tank pumps are located in the ___________ of the wing tanks.
a)
outer section
b)
inner section
c)
inner and outer section
49.
The fuel quantity indications appear on the ______________.
a)
ECAM FUEL PAGE
b)
ECAM CRUISE PAGE
50.
Where is the refuel/defuel receptacle on the aircraft?
a)
Under the leading edge of the right wing
b)
Under the leading edge of the left wing
51.
How many fuel pumps are installed in the entire fuel system?
a)
4
b)
5
c)
3
d)
6
52.
The Blue system is normally pressurized by ______________.
a)
the Engine 1 pump
b)
An electric pump
c)
the Engine 2 pump
d)
Ram Air Turbine (RAT)
53.
The PTU activates automatically when the pressure differential between the Green and Yellow hydraulic systems exceeds ___________
a)
250 PSI
b)
750 PSI
c)
500 PSI
d)
300 PSI
54.
The RAT can be manually deployed by the crew.
a)
true
b)
false
55.
Normal brakes are pressurized by the ___________, while alternate and parking brakes are pressurized by the _____________.
a)
Yellow system, green system
b)
Blue system, yellow system
c)
Green system, yellow system
56.
What is the primary purpose of the electric motor driven pump in the yellow hydraulic system?
a)
Operate the cargo door
b)
Provide hydraulic pressure when the engines are not running
c)
Pressurize the green system through the PTU
57.
The Green system is normally pressurized by a pump driven by ___________.<br /><br />
a)
Engine 1
b)
Engine 2
58.
What is the normal operating pressure for the hydraulic systems?
a)
2500 PSI
b)
2000 PSI
c)
3500 PSI
d)
3000 PSI
59.
Flight Control Protection Symbols display in ________ on the PFD at +/- 67 bank, to mark the bank limits.
a)
White
b)
Green
c)
Red
d)
Amber
60.
Question = When the aircraft is above 2500 ft., the displays are amber if the vertical speed exceeds __________ ft/min.
a)
5000
b)
7000
c)
6000
d)
10000
61.
Regardless of the V2 speed, the FD pitch command for the SRS mode will be to maintain at least V2 __________ for a normal takeoff.
a)
+10 knots
b)
+15 knots
c)
+5 knots
62.
The E/WD display always has priority over the SD display.
a)
true
b)
false
63.
The EFIS control panel allows the pilot to select one of ______ desired modes on the ND.
a)
3
b)
5
c)
4
64.
A ________ diamond is used to display the aircraft track.
a)
Blue
b)
Red
c)
Yellow
d)
Green
65.
The ________ position provides a view of the route in a North up orientation.<br />Weather Radar and Terrain displays are not available in this mode.<br />
a)
PLAN
b)
ARC
c)
ILS
d)
VOR
66.
The maximum steering angle available through use of the Steering Hand Wheels is ___, while the maximum steering angle available through use of the rudder pedals is ___.
a)
+/- 75 degrees ; +/- 6 degrees
b)
+/- 80 degrees ; +/- 8 degrees
c)
+/-65 degrees ; +/- 6 degrees
d)
+/-70 degrees ; +/- 5 degrees
67.
A Tow Control Lever is positioned for pushback and tow which allows ground personnel to turn the nose wheel up to ________.
a)
+/- 85 degrees
b)
+/- 80 degrees
c)
+/- 95 degrees
d)
+/- 75 degrees
68.
A green arc appears over the hottest wheel when one brake temperature exceeds ____________.
a)
100 degrees F
b)
150 degrees C
c)
125 degrees C
d)
100 degrees C
69.
The Autobrake MED mode sends progressive pressure to the brakes __________ after Ground Spoiler deployment
a)
4 seconds
b)
5 seconds
c)
2 seconds
d)
6 seconds
70.
A DECEL light illuminates when the deceleration value is at least ________ of the selected rate.
a)
0.8
b)
0.75
c)
0.85
d)
0.9
71.
The Navigation mode (NAV) is the normal mode that continuously supplies data to the ADIRUs. It operates as long as _____ valid satellite signals remain available.
a)
6
b)
4
c)
3
d)
8
72.
The DDRMI powered compass is normally driven by _____________.
a)
ADIRU 1
b)
ADIRU 2
c)
ADIRU 3
73.
Normally, the GPS 1 receiver supplies _________________.
a)
ADIRU 1 and 3
b)
ADIRU 3
c)
ADIRU 1
d)
ADIRU 2
74.
A back-up tuning method (Standby) is available on the ______ when the normal Auto and Manual tuning methods are inoperative.
a)
ACPs
b)
ACARS
c)
MCDU
d)
RMPs
75.
When Standby tuning is selected on the RMP, the blue data lines on the Radio Nav page ___________.
a)
are blank
b)
display amber
c)
display white
76.
The cabin oxygen masks are released by a door that can be opened ______________.
a)
electrically and manually by a pushbutton or physically by a tool
b)
manually, by pushbutton only
c)
electrically only
77.
If the crew supply pushbutton is off, the word OXY will display ________ on the DOOR/OXY ECAM PAGE.
a)
amber
b)
green
c)
blue
d)
white
78.
The cabin oxygen system is a ___________ system.
a)
demand
b)
continuous- flow
79.
Cabin oxygen masks are automatically presented to persons in the cabin when the cabin altitude exceeds ___________.
a)
12,000 feet
b)
15,000 feet
c)
12,500 feet
d)
14,000 feet
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