StrainTech EDV Support Glattfelden

CHAPTER 21 – AIR CONDITION
1 The temperature of each aircraft zone is optimized
by means of ….. ?
A A HOT AIR valve.
B A ZONE control valve.
lat
C A PACK FLOW valve.
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A320 Series - Technical Examination
2 Under what conditions should the pack flow
controller be set to LOW?
B With a low passenger load to increase
cabin temperature.
C With a high passenger load to reduce
cabin temperature.
Su
D In cold conditions to achieve a higher
cabin temperature range..
pp
A With a low passenger load to reduce bleed air
demand and improve fuel efficiency.
ort
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D A TRIM AIR valve
3 Under what conditions should the pack flow
DV
controller be set to HIGH?
A In cold conditions to achieve a higher
cabin temperature range.
hE
B With a low passenger load to increase
cabin temperature.
C With a high passenger load to reduce
cabin temperature.
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D With a high passenger load in hot
conditions in order to help reduce the
cabin temperature.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 1 of 57
No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
4 The PACK FLOW controller is set to NORM
and yet the ECAM display shows PACK
FLOW to be high. How is this possible ?
A As the engines are not running the PACK
FLOW indicators are at the position they
were selected to at the last shut down.
DV
Su
pp
D With cold outside air conditions the PACK
FLOW is automatically increased to help
increase the cabin temperature.
ort
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C HI flow is automatically selected regardless
of PACK FLOW selector position because air
is only being supplied by the APU.
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B As no bleed air is flowing the PACK FLOW
valves are spring loaded to the fully open
position.
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A320 Series - Technical Examination
CHAPTER 21 – PRESSURIZATION
against . . . .
hE
5 The safety valve protects the aircraft
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A Excessive cabin V/S in manual mode.
nT
B Water ingress in the event of ditching.
rai
C Excessive cabin altitude.
St
D Excessive differential pressure in the cabin.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 2 of 57
No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
6 Having manually set the LDG ELEV the cabin
altitude is . . .
A Only controllable manually through the MAN V/S CTL.
pp
ort
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C Still controlled normally through the safety valve.
D Only controllable manually through the LDG ELEV
selector.
MAN
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B Still controlled automatically through the outflow
valve.
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A320 Series - Technical Examination
7 In AUTO, the cabin differential pressure is
normally controlled by . . .
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A The SAFETY valve.
B The INLET valve.
??
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hE
D The OUTFLOW valve.
DV
C The EXTRACT valve.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
A320 Series - Technical Examination
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8 On the ground the cabin hould be . . . .
A Depressurized.
B At maximum differential pressure.
pp
ort
G
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C At sea level pressure..
A Controlled with the MAN V/S CTL.
B Controlled with the MODE SEL pb.
C Controlled with the DITCHING pb.
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9 The safety valve is….
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D Fully automatic and cannot be controlled manually.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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A320 Series - Technical Examination
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10 The MODE SEL pb sw in MAN mode allows
you to use the MAN V/S CTL in order to. . . .
A Manually alter the air inlet valve setting.
B Manually adjust the pack flow valve.
C Manually adjust the outflow valve.
ort
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11 The LDG ELEV has been set manually. What is
the value ?
lat
D Manually alter the pack outflow valve setting.
A 6 ft
B 60 ft
C 600 ft
pp
D 6’000 ft
Su
12 As you can see, cabin pressure control is
manual. You want to descend from FL350 to FL
310. What is your target CABIN ALT?
A 0 ft
DV
B 4’700 ft
C 5’300 ft
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D 6’000 ft
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
13 By moving the MAN V/S CTL to this position . . .
A The cabin altitude is raised by opening
the outflow valve.
B The cabin altitude is lowered by opening
the outflow valve.
C The cabin altitude raised by closing the
outflow valve.
ort
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D The cabin altitude is lowered by closing
the outflow valve.
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CHAPTER 21 – VENTILATION
A The aircraft must be on the ground with
the thrust levers not at T/O.
The aircraft must be in the air with the
thrust levers not at T/O and the skin
temperature below the ground threshold.
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DV
C
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B The aircraft must be on the ground with
the thrust levers at T/O and the skin
temperature above the ground threshold.
pp
14 For the aircraft to be in this normal operation,
open circuit configuration, what conditions must
be satisfied?
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
15 When can we have a closed circuit configuration
in normal operation?
A The aircraft must be on the ground with
the thrust levers not at T/O.
B The aircraft must be on the ground with
the thrust levers at T/O.
The aircraft must be in the air, or on the
ground with the thrust levers at T/O.
Su
pp
ort
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D
lat
C The aircraft must be in the air with the
thrust levers not at T/O.
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A320 Series - Technical Examination
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16 For the aircraft to be in this normal operation,
intermediate configuration, what conditions must
be satisfied?
A The aircraft must be on the ground with
the thrust levers not at T/O.
hE
B The aircraft must be in the air with the
thrust levers at T/O and the skin
temperature above the ground threshold.
The skin temperature must be below the
ground or in-flight threshold.
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D
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C The aircraft must be in the air, or on the
ground with the thrust levers at T/O.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
17 Which configuration of the ventilation system do
you expect with these flight conditions ?
A Open configuration.
B Closed configuration.
lat
C Intermediate configuration.
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A320 Series - Technical Examination
?
pp
ort
G
?
18 For the aircraft to be in this normal operation,
intermediate configuration, what conditions must
be satisfied?
Su
A The aircraft must be on the ground with
the thrust levers not at T/O.
DV
B The aircraft must be in the air with the
thrust levers at T/O and the skin
temperature above the ground threshold.
C The aircraft must be in the air, or on the
ground with the thrust levers at T/O.
hE
The skin temperature must be below the
ground or in-flight threshold.
St
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D
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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A BLEED Key
B ENG Key
C COND Key
D PRESS Key
B Intermediate Configuration on the ground
and open configuration in the air.
Su
C Open configuration on the ground and
smoke configuration in the air.
pp
A Closed configuration on the ground before
applying T/O power and open configuration
after applying T/O power and in the air.
ort
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20 With both the BLOWER and EXTRACT pb sw in
AUTO, what ventilation configurations do you
normally expect to see?
lat
19 Select the ECAM key to access the VENTilation
information.
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A320 Series - Technical Examination
?
?
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hE
DV
D Open configuration on the ground before
applying T/O power and closed configuration
after applying T/O power and in the air.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
21 With both the BLOWER and EXTRACT pb sw in
OVRD, what happens to the ventilation system?
A The system goes into open configuration and the
blower fan stops.
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B The system goes into closed configuration and the
blower fan stops.
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A320 Series - Technical Examination
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C The system goes into open configuration and the
extract fan stops.
?
?
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hE
DV
Su
pp
D The system goes into closed configuration and the
skin exchange outlet by-pass valve opens.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
CHAPTER 22 - AUTOFLIGHT
22 The dashes in some windows of this FCU
indicate that there is enough information to
provide Managed Guidance. What does this do?
A Guide the aircraft to target parameters
that the pilot selects on the FCU.
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B Guides the aircraft along a preplanned
route as computed by the FMGS. It has
priority over selected inputs.
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C Guides the aircraft in the vertical and
speed profiles only. It does not have
priority over selected inputs.
D Guides the aircraft in lateral, vertical and
speed profiles as computed by the FMGS
but selected inputs have priority.
23 ATC informs you of conflicting traffic and tells
Su
A Select FL100 immediately.
pp
you to level off immediately.
Do this now !
B Increase speed to break the climb rate
DV
C Push the EXPEED button immediately.
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hE
D Push the V//S – FPA knob immediately.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
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24 Have a look at the ND. What happens if the HDG
selector knob is pushed now?
A The aircraft reverts to the original F-PLN.
B The HDG/TRK target changes.
C The target changes from HDG to TRK.
DV
Su
pp
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D The aircraft will follow the selected HDG/TRK.
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A320 Series - Technical Examination
25 This aircraft is following a track of 140.
hE
A Thrue
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B False
26 Have a look at the FMA. Why are ALT and G/S on
nT
the same line but in different colors ?
A ALT is in active mode and G/S is in armed mode.
B ALT is in armed mode and G/S is in active mode.
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C ALT and G/S are in armed mode but ALT has a
constraint.
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D ALT and G/S are in armed mode but G/S has a
constraint.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
A320 Series - Technical Examination
27 Managed NAV is armed on an intercept heading.
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What happens if the HDG selector knob is
pulled?
A The aircraft will fly to the next waypoint
on the original F-PLN.
B The selection changes from HDG to TRK.
lat
C The aircraft follows the selected HDG/TRK.
Su
pp
ort
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D The aircraft continues on the heading until the
original F-PLN is intercepted.
DV
28 Selected NAV is active on an intercept heading.
What happens if the HDG selector knob is
pushed?
hE
A The aircraft will fly to the next waypoint on the original
F-PLN.
B The aircraft continues on the heading until the original
F-PLN is intercepted.
ec
C The aircraft follows the selected HDG/TRK
indefinitely.
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D The selection changes from HDG to TRK.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
29 Have a look at the FMA. The functions displayed
in green on the first line are ...
A All in armed mode as indicated by the
GREEN color.
B All in active mode as they are on the
first line and GREEN.
lat
C Either in armed or active mode
depending on the FMGC settings.
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30 Have a look at the FMA. The blue LOC is an
armed mode
A Yes.
pp
B No.
ort
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D The titles of the columns with ALT, G/S
and LOC as the active modes.
there a white box around it ?
Su
31 A/THR in blue means it is Armed. Why is
DV
A The A/THR has been disconnected and
the box means it has returned to the
armed mode.
B The A/THR has only become armed within
the last 10 seconds and the box is to draw
attention to the change.
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hE
C A box appears around any function which
is being controlled by the autopilot.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
A320 Series - Technical Examination
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32 A/THR in white means it is...
A Disconnected.
B Armed.
pp
ort
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C Activ.
33 Your next flight is from Paris-Orly to Cairo.
A With left Line Select Key 3.
DV
B With right Line Select Key 1
Su
The Company route has been entered in the
scratchpad. How you must insert the
selected route ORYCAI1?
C Pushing the F-PLN button twice.
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D With left Line Select Key 1.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
34 You notice that some waypoints have a small
triangle after the name. What does it mean?
A It means this point has to be overflown..
B It means these points are compulsory reporting points.
DV
Su
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ort
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C It indicates the flight plan has been changed at these
points.
D It indicates speed constraints at these points.
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A320 Series - Technical Examination
35 Why is the word DECELERATE on
the FMA ?.
hE
A It is a warning that you are over-ridding
a speed protection.
B TCAS discovered a possible conflict traffic and wants
to decelerate to keep the separation.
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C The aircraft missed a speed constraint while in
selected speed.
D The aircraft has passed the computed ideal descent
point.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
A The aircraft will stop the climb at FL 60, pass the
constraint and then continue to climb to FL 150.
B The aircraft will disregard the constraint and climb to
FL 150.
C As soon as the aircraft passes FL 60, the target
altitude on the PFD will change to FL 150 and the
aircraft continues to climb
pp
ort
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D The aircraft will level off at FL 60, the PF has to pull
the ALT selection knob a second time to climb to
FL 150.
lat
36 ATC cleared you to FL 150. The PF set the new
altitude on the FCU. What will happen if he pulls
the ALT selection knob?
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A320 Series - Technical Examination
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37 ATC cleared you to FL 150. The PF set the new
altitude on the FCU. What will happen if he pulls
the ALT selection knob?
DV
A The aircraft will stop the climb at FL 60, pass the
constraint and then continue to climb to FL 150.
hE
B The aircraft will disregard the constraint and climb to
FL 150.
C As soon as the aircraft passes FL 60, the target
altitude on the PFD will change to FL 150 and the
aircraft continues to climb
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D The aircraft will level off at FL 60, the PF has to pull
the ALT selection knob a second time to climb to
FL 150.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
A Dial in the new cleared level FL150 and push the
ALT control knob.raised by opening the outflow
valve.
B Dial in the new cleared level FL150 and pull the ALT
control knob.
ort
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C Pull the HDG control knob and then dial in the new
cleared level FL150 and pull the ALT control knob.
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38 ATC cleared you to FL 150. What selections
should you make to ensure that the aircraft
complies with the constraints?
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A320 Series - Technical Examination
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D Pull the HDG control knob and then dial in the new
cleared level FL150 and push the ALT control knob
Su
39 ATC tells you to turn onto a radar heading. Is it
still possible to comply with the climb constraint
at FL60?
A No. It is only possible to comply with the constraints
in managed NAV.
Yes. By selecting FL60 on the ALT knob until the
constraint point has beenpassed
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C
DV
B Yes. The constraint takes priority over any other FCU
selections.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
40 ATC cleared you to FL 150. The PF set the new
altitude on the FCU. What will happen if he
pushes the HDG/TRK selection knob now?
A The aircraft will continue on the present
heading, stop the climb at FL 60.
lat
B The aircraft will stay on the present
heading, disregard the constraint and
climb to FL 150.
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C The aircraft will continue in managed
NAV, stop the climb at FL 60 until the
constraint has been passed and then
climb to FL150.
The aircraft will follow the F-PLN,
disregard the constraint and climb to
FL 150.
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hE
DV
Su
pp
D
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© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
CHAPTER 23 – COMMUNICATION
41 How can you get the mechanics attention when
he is outside the aircraft?
A Use the Mech pb sw on the CALLS panel which
sounds an external horn.
lat
B Press the PA button and call him.
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Su
pp
ort
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C Select the MECH transmission key on the ACP
DV
42 During pre-flight, you have to check the CVR.
How you perform this test now?
A You don’t need any electrical power, the CVR is
battery powerded, just push the CVR test button
hE
B Apply electrical power, leave the park brake in the
OFF position and push the CVR test button.
ec
C Apply electrical power, set the park brake in the ON
position and push the CVR test button.
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D Apply electrical power, set the park brake in the ON
position, push the GND CTL button to energize the
CVR while on ground without engines running and
push the CVR test button.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
43 How do you erase the CVR?
A Press the CVR ERASE pb when the aircraft is on the
ground with the parking brake set.
B Press the CVR ERASE pb for 2 seconds when the
aircraft is airborne.
C It is not possible to erase the CVR.
mean?
ort
G
44 In this example what does the white SEL light
lat
D Press the CVR ERASE and CVR TEST pbs
simultaneously.
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A It is an indication that somebody is transmitting on
VHF 2.
B It is an indication that both RMP 1 and RMP 2 are
being used to tune VHF1.
pp
C It is an indication of a SELCAL.
RMP 1
RMP 2
ec
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DV
Su
D It is an indication that both RMP 1 and RMP2 are
being used to tune VHF2.
45 In case of RMP 2 failure, VHF 2 is lost
nT
A Yes
St
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B No
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A Select VHF2, turn the freyuency selecter until 125.05
is displayed in the STBY window, now push the
transfer button to select 125.05 as the active
frequency.
B The Captain hs to change the frequency because your
RMP is on VHF2.
47 You want to check the ATIS. The correct
ort
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C Hold down the transfer button and adjust the
frequency selector untill 125.05 is displayed, release
the transfer button now.
RMP 2
lat
46 How you select 125.05 as the active frequency
on VHF 2 on RMP 2?
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pp
frequency has been set on VOR 1. The
loudspeaker is switched on but you can’t
hear the information. How you do the right
settings on the ACP?
Su
A Open the VOR1 lever (CW) the ATIS will be audible
over the speaker.
B Push the RESET button twice and turn the VOR1
knob fully CW.
DV
C Open the VOR1 lever (CW) and select VOICE to
listen to the ATIS on VOR 1
48 With the AUDIO SWITCHING knob in the
hE
CAPT 3 position, the Captain uses his own
acoustic equipment on ACP 3.
A Yes
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B No.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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CHAPTER 24 – ELECTRICAL
49 You enter a dark cockpit, what actionsare
necessary before checking the battery voltages?
A You have to check that the external power is on.
B You have to ensure that at least one battery is on.
lat
C You have to ensure that both batteries are on.
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D You have to verify that both batteries are off.
50 According to these indications, which statement
is true ?
A Both battery voltages are below the minimum
of 30 V.
pp
B Both battery voltages are above the minimum
of 25.5 V.
Su
C I can only check the battery voltages on the ECAM
ELEC page.
D I am unable to check the battery voltages with
external power available.
do you charge them?
DV
51 If the battery voltages are below minimum how
hE
A I have to call a mechanic because the batteries can
only be charged by maintenance.
B I have to switch the external power on
and check the BAT pbs are on.
C I have to switch the external power to ON and switch
the batteries off.
nT
ec
D I have to start the APU as the batteries can only be
charged by the APU generator.
52 What is the meaning of the green AVAIL light?
rai
A External power is plugged in, you must push the EXT
PWR pb to connect it
B External power is available to the batteries only.
C The external power panel door has been opened.
St
D External power is supplying the aircraft systems.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
52 After having switched the external power to ON,
you get the following indications. What do they
mean?
A Battery voltage is too low to allow external power
connection.
B There is a fault as the external power supply has
priority over the generators.
lat
C You have to switch the generators on.
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Su
pp
ort
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D On ground these indications are normal when the
engines are not running
DV
54 Both batteries are now charged by the external
power unit. Approximately how long does the
charging process take?
B 60 minutes
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C 4 hours
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D 20 minutes
hE
A 10 minutes
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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55 Having started the APU, how can you get the
APU generator to power the electrical system?
A The APU generator must be switched on.
B By pushing the EXT PWR pb thus disconnecting the
external power.
lat
C By pushing the BUS TIE pb.
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A320 Series - Technical Examination
pp
ort
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D You are unable to as The APU power output is
outside normal parameters.
56 Now you want the APU generator to supply the
electrical system. How you proceed?
Su
A When the APU is running, the power is automatically
transferred from External PWR to the APU generator.
DV
B After the APU has started, switch the batteries off
befor you ask the maintenance to disconnect the
External PWR.
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hE
C Simply de-select the Extrenal PWR by psuhing the
External PWR switch and then allow the maintenance
to remove the External PWR from the aircraft-
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 25 of 57
No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
57 Now the APU generator is supplying the electrical
system. Do you know the order of priority for the
different generators?
A Engines, external power, APU.
B APU, engines, external power.
lat
C External power, engines, APU.
tfe
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A320 Series - Technical Examination
Su
pp
ort
G
D APU, external power, engines.
DV
58 An ECAM Warning appears. How you proceed?
A To push the IDG2 pb until the GEN FAULT light
comes on and then for at least 3 more seconds.
hE
B To push the IDG 2 pb for a maximum of 10
seconds.
C To push the IDG2 pb for at least 10 seconds to
ensure the disconnection.
St
rai
nT
ec
D To push the IDG2 pb until the GEN FAULT
light comes on, but only for a
maximum of 3 seconds.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 26 of 57
No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
A It is a reminder to push the GALLEY pb to manually
shed the main galley.
B It is a reminder to get the flight attendants to switch off
galley equipment to decrease the load on the
remaining generator.
pp
ort
G
C It is a reminder that the main galley has been shed
automatically following the loss of one generator.
lat
59 After IDG disconnection why do you get a
GALLEY SHED indication on the SD ?
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A320 Series - Technical Examination
Su
60 Immediately after the fault occurred, you notice
the red FAULT light on the RAT & EMER GEN
pushbutton. How do you interpret this indication?
DV
A The EMER GEN is not yet supplying the system.
B The EMER GEN has failed. You will have to lower the
landing gear to reactivate it
hE
C The RAT has failed. You will have to turn the
batteries to OFF.
St
rai
nT
ec
D The FAULT light is always on when you
are in ELEC EMER CONFIG.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 27 of 57
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written permission of the authors!
With the EMER GEN on line, how would you
expect the ELEC page to look ?
B
pp
ort
G
A
lat
61
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A320 Series - Technical Examination
St
rai
nT
ec
hE
DV
Su
C
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
62
The ECAM requires you to reset the
generators.
But the reset was un-successful. Why must
you push the BUS TIE pb sw OFF?
To isolate both sides of the electrical
system.
To connect the APU generator to the
electrical system.
C
To re-connect both sides of the electrical
system.
D
To shed the AC ESS BUSS.
lat
B
St
rai
nT
ec
hE
DV
Su
pp
ort
G
A
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A320 Series - Technical Examination
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
63 You want to open the cabin door, whilst lifting the
control handle the white light illuminates. What
does this mean?
A There is residual pressure in the cabin.
B The ramp is not correctly positioned.
C The slide is still armed.
ort
G
D Somebody is trying to open the door from outside.
lat
CHAPTER 25 – CABIN
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A320 Series - Technical Examination
64 There is no other way of deploying the overwing
pp
escape slide if it fails to deploy automatically on
opening the emergency exit.
A Yes
St
rai
nT
ec
hE
DV
Su
B No
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
A They can be deployed by the flight attendants using
the CIDS panel.
C They cannot be deployed if the automatic system
fails.
ort
G
B They can be deployed by pressing the MASK MAN
ON pb on the Overhead Panel.
lat
65 If the oxygen masks fail to deploy automatically
how else can they be deployed?
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A320 Series - Technical Examination
Su
pp
D They can be deployed by pressing the PASSENGER
SYS ON pb on the Overhead Panel.
DV
66 Make the necessary switch selections so that the
EVAC alarm can be activated from either the
cockpit or the cabin.
hE
A Press the HORN SHUT OFF switch twice
nT
ec
B Push the COMMAND button
St
rai
C Select CAPT & PURS
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
A320 Series - Technical Examination
A Three long buzzers and a red EVAC light.
B Three long buzzers and a steady amber EMER call
light.
ort
G
C Three long buzzers, flashing EMER CALL, EMER
ON and ACP ATT lights.
lat
pressed the Emergency Call button. What
indications will you get in the flight deck?
tfe
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n
67 In the cabin one of the flight attendants has
St
rai
nT
ec
hE
DV
Su
pp
D Flashing EMER CALL, EMER ON and EVAC lights.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 32 of 57
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written permission of the authors!
68 It is the first flight of the day. Are you able to
carry out the APU fire test?
A No, the SQUIB and DISCH light should be
illuminated.
C Yes, the APU FIRE pb is in and guarded and the
AGENT light is extinguished.
69 Can the APU FIRE test be performed using
battery power only ?
pp
A Yes
ort
G
B No, you have to raise the guard before you can carry
out the test.
lat
CHAPTER 26 – FIRE
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A320 Series - Technical Examination
Su
B No
DV
70 Can you declare the APU FIRE test as
successful?
hE
A Yes
St
rai
nT
ec
B No
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
71 Would you get additional indications if AC power
was available ?
A No.
?
?
lat
B Yes, the MASTER CAUTION and CRC.
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A320 Series - Technical Examination
ort
G
C Yes, the APU FIRE procedure on the
ECAM, the CRC and the MASTER WARN.
?
?
pp
72 According to these indications...
Su
A One fire detection loop has failed. Fire detection for
both engines is not available.
?
INOP SYS
ENG 1 LOOP B
B One fire detection loop has failed. Fire detection for
both engines is still available.
DV
C One fire detection loop of engine 1 has failed. Fire
detection for engine 1 is inoperative.
St
rai
nT
ec
hE
D Both fire detection loops of engine 1 have failed. Fire
detection for engine 1 is inoperative.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 34 of 57
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written permission of the authors!
73 With reference to cargo compartment fire
extinguishing, which statement is true?
A There are two fire bottles, one for the FWD
compartment and one for the AFT.
B There is only one fire bottle, pressing either DISCH
pb discharges it into both compartments.
C There is only one fire bottle, when it is discharged
both amber DISCH lights come on.
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A320 Series - Technical Examination
SMOKE FWD CARGO SMOKE LAND ASAP
St
rai
nT
ec
hE
DV
Su
pp
ort
G
lat
D There are two fire bottles, when the DISCH pb is
pressed they are both discharged into the
appropriate compartment.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 35 of 57
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written permission of the authors!
A320 Series - Technical Examination
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CHAPTER 27 – FLIGHT CONTROLS
74 How many actuators are provided to control the
ailerons and how many hydraulic sources supply
these actuators?
A 2 hydraulic sources with 4 actuators.
ort
G
lat
B 1 hydraulic source with 2 actuators.
C 4 hydraulic sources with 4 actuators.
pp
D 3 hydraulic sources with 4 actuators.
Su
75 The message WING TIP BRK ON appears on the
E/WD. What does it mean?
FLAP
S
DV
A A hydraulic device locks the flaps in their present
position.
B To reduce structural stress, the slats movement is
being slowed down through the wing tip brakes.
F
F LOCKED
F/CTL FLAPS LOCKED
- WING TIP BRK ON
MAX SPEED . . . . . . . . . . . . . . 215
hE
C To avoid asymmetry, the outer slats are locked in
their present position.
St
rai
nT
ec
D Because of the locked flaps, the wing tip brakes also
lock the slats.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
A320 Series - Technical Examination
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76 Are there any control surfaces with a mechanical
backup?
A Yes, the ailerons.
lat
B Yes, the spoilers.
ort
G
C Yes, the THS and the rudder.
77 You have the following message.
What happened?
pp
D No, there aren’t any control surfaces with mechanical
backup.
F/TTL SPLR FAULT
B The right SPLR 3 failed to extend.
DV
C The left SPLR 3 failed to retract.
Su
A The left SPLR 3 failed to extend.
St
rai
nT
ec
hE
D The right SPLR 3 failed to retract.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 37 of 57
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written permission of the authors!
78 What will happen next?
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A320 Series - Technical Examination
F/TTL SPLR FAULT
A The left SPLR 3 will be retracted, the right SPLR 3
will be inhibited to prevent asymmetry.
ort
G
lat
B The right SPLR 3 will be extended to prevent
asymmetry.
DV
Su
pp
C Left SPLR 3 remains extended, spoiler operation is
not possible anymore.
hE
79 What does the white cross indicate?
ec
A It is an indicator for the sidestick deflections during
the flight control check.
nT
B It is an indicator for the control surface deflections
during the flight control check.
St
rai
C It is an indication for the rudder pedal deflections
during the flight control check.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 38 of 57
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written permission of the authors!
80 What will happen if the speed reaches VFE Speed
( red barber pole )?
A There will be an automatic flap retraction.
B There will be an automatic slat and flap retraction.
ort
G
St
rai
nT
ec
hE
DV
Su
pp
D High Speed protection will become active, the
autothrust will reduce thrust.
lat
C High Speed protection will become active, the
autopilot will increase the pitch.
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A320 Series - Technical Examination
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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written permission of the authors!
A320 Series - Technical Examination
tfe
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n
81 In Normal Law, if one sidestick is rapidly pulled
fully back, can the aircraft’s maximum allowable
“G” load be exceeded ?
A Yes. Rapid sidestick deflection must never be made.
lat
B Yes, until maximum pitch attitude is reached.
D No. The load factor limitation overrides sidestick
commands to avoid excessive “G” loads.
ort
G
C No. At maximum “G” load, the sidesticks are deactivated for 5 seconds.
Su
pp
82 In this situation, which indications do you expect,
if one sidestick is deflected fully forward ?
B
hE
DV
A
D
St
rai
nT
ec
C
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 40 of 57
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written permission of the authors!
A The bank angle will automatically return to 33º.
B The bank angle will not change.
ort
G
C The bank angle will return to wings level, because
the bank protection is active.
lat
83 According to these indications, if you release the
sidestick now...
tfe
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A320 Series - Technical Examination
Su
pp
D The bank angle will return to 20º
.
DV
84 In Normal Law, what is the maximum bank angle you
can reach with the sidestick fully deflected ?
A 33º
hE
B There is no bank limitation.
C 80 º
?
St
rai
nT
ec
D 67 º
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 41 of 57
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written permission of the authors!
A320 Series - Technical Examination
tfe
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85 According to these indications, which flight
control law is active ?
A Normal Law.
B Alternate Law.
lat
C Direct Law.
pp
ort
G
D Mechanical Back Up.
Su
86 According to these indications, which flight control
law is active ?
DV
A Normal Law.
C Direct Law.
hE
B Alternate Law.
St
rai
nT
ec
D Mechanical Back Up.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 42 of 57
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written permission of the authors!
A320 Series - Technical Examination
tfe
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87 According to these indications, which flight
control law is active ?
A Normal Law.
lat
B Alternate Law
ort
G
C Direct Law.
pp
D Mechanical Back Up.
88 According to these indications, which flight control
law is active ?
Su
A Normal Law.
DV
B Alternate Law
hE
C Direct Law.
St
rai
nT
ec
D Mechanical Back Up.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 43 of 57
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written permission of the authors!
A320 Series - Technical Examination
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89 Observe the PFD.
Without any sidestick inputs...
A The aircraft’s attitude will stay constant.
lat
B The pitch will stay constant, the bank angle will
slowly decrease.
ort
G
C The bank angle will stay constant, the pitch will
slowly decrease.
pp
D The aircraft’s attitude will slowly tend towards “wings
level” and “pitch 0”.
Su
90 According to the following indications...
DV
A The High Angle Of Attack protection is active.
hE
B The Alpha Floor protection is active.
C The Load Factor Limitation is active.
St
rai
nT
ec
D No protection is active.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 44 of 57
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written permission of the authors!
91 Let’s assume, you have set idle power and pulled
the sidestick back to maintain altitude. Observe
the PFD. If you release the sidestick now...
A The aircraft will descend with 135 kts.
lat
B The aircraft will descend with 150 kts.
tfe
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A320 Series - Technical Examination
ort
G
C The aircraft will maintain altitude until 120 kts are
reached.
Su
92 According to these indications...
pp
D The aircraft will maintain altitude until a stall occurs.
DV
A The High Angle Of Attack protection is active.
hE
B The Alpha Floor protection is active.
ec
C The Load Factor Limitation is active.
St
rai
nT
D No protection is active.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 45 of 57
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written permission of the authors!
A The speed will fall below 120 kts. The aircraft might
stall.
B The speed will fall below 120 kts. To avoid a stall,
climb power will be automatically set.
C The High Angle Of Attack protection will override the
sidestick input. The pitch will be lowered to maintain
120 kts.
pp
ort
G
D The speed will fall further. At 114 kts the pitch will be
lowered to maintain 114 kts.
lat
93 According to these indications, if the sidestick is
held at full back position...
tfe
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A320 Series - Technical Examination
Su
94 Observe the PFD. Which statement is true ?
A FLOOR
DV
A The Alpha Floor protection has automatically set CLB
power.
B The Alpha Floor protection has automatically set
TO/GA power.
hE
C The Alpha Floor protection will override sidestick
inputs. The nose will be lowered.
St
rai
nT
ec
D A stall is detected.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 46 of 57
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written permission of the authors!
tfe
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A320 Series - Technical Examination
95 To fly a coordinated turn...
A No rudder inputs are required.
lat
B You have to center the sideslip indicator with the
rudder pedals.
Su
pp
ort
G
C Only little rudder inputs are required.
DV
96 In Normal Law, is there a maximum pitch
attitude?
A
hE
A Yes, indicated by the green dashes (A).
B
nT
C No.
ec
B Yes, indicated by the green dashes (B).
St
rai
D Yes, pitch is limited to 20º nose up.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 47 of 57
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written permission of the authors!
A320 Series - Technical Examination
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97 In Normal Law, is there a maximum bank angle?
A No.
B
B Yes, indicated by the green dashes (A).
A
lat
C Yes, indicated by the white dashes (B).
pp
ort
G
D Yes, bank is limited to 80º.
98 How do you interpret the amber crosses on
the PFD?
Su
A The autotrim is lost. You have to use manual pitch
trim.
DV
B The ailerons are controlled directly by the sidesticks.
X
X
hE
C The bank angle protection is lost.
St
rai
nT
ec
D The bank angle protection is active.
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 48 of 57
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A320 Series - Technical Examination
B
pp
ort
G
lat
A
tfe
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99 The Capt’s sidestick is deflected fully left and the FO’s sidestick is simultaneously deflected fully
right. Which indications do you expect ?
D
St
rai
nT
ec
hE
DV
Su
C
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 49 of 57
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A320 Series - Technical Examination
B
The FO’s sidestick is also deflected. Both
inputs are added.
C
The FO’s sidestick is also deflected. The green light
indicates that his input is suppressed because you
have priority.
D
The FO’s sidestick is also deflected. The green light
indicates that your input is suppressed because he
has priority.
?
lat
The green light flashes because your sidestick is out
of neutral position.
ort
G
A
tfe
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100 Let’s assume you, as Capt, deflect your sidestick
to the left in order to fly a turn. Observe the
indications. How do you interpret them
pp
101 If both pilots deflect their sidesticks fully back...
The “pitch up” order is twice as high as with only one
stick deflected.
B
The “pitch up” order is 1.5 times higher than with
only one stick deflected.
C
No inputs are send to the flight control computers
unless one pilot presses the take over pb on his
stick.
D
The “pitch up” order is equal to a single stick
deflection.
Su
A
hE
DV
?
ec
102 If the FO presses the take over pb constantly...
The Capt is unable to re-activate his sidestick.
B
The Capt’s sidestick is still active. It will be deactivated after 40 secs.
C
The Capt can re-activate his sidestick by pressing
the take over pb for more than 40 secs.
rai
nT
A
The Capt can re-activate his sidestick immediately
by pressing his take over pb.
St
D
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
CAPT
F/O
Page 50 of 57
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written permission of the authors!
A320 Series - Technical Examination
B
The Capt is unable to re-activate his sidestick for the
rest of the flight.
C
The Capt is unable to re-activate his sidestick for the
rest of the flight.
D
Both sidesticks are active.
lat
The Capt’s sidestick is de-activated unless he
presses his take over pb.
> 40 sec
ort
G
A
tfe
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103 Let’s assume the FO presses his take over pb
and releases it after more than 40 secs...
CAPT
F/O
pp
104 With either AP engaged, which statement is true?
Both sidesticks are locked in neutral position. The
lock can not be overridden.
B
Both sidesticks are de-activated until the AP is
disengaged.
C
Both sidesticks are locked in neutral position. By
applying a certain force, the lock can be overridden
but the AP remains engaged.
D
Both sidesticks are locked in neutral position. By
applying a certain force, the lock can be overridden
and the AP is disengaged.
St
rai
nT
ec
hE
DV
Su
A
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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A320 Series - Technical Examination
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CHAPTER 28 – FUEL
Yes.
B
No.
pp
ort
G
A
lat
105 According to this indication, only the Center
Tank Pumps are feeding the engines.
Su
106 According to the FUEL page, which statement is
correct?
All the pumps are on but only the APU is receiving
fuel.
B
All the pumps are off and the APU is receiving fuel
by gravity.
C
All the pumps are on but no fuel is being used.
St
rai
nT
ec
hE
DV
A
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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A320 Series - Technical Examination
A
The center tank fuel mode selector is OFF.
B
The center tank pumps are OFF.
C
At least one center tank pump is running.
tfe
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107 The message CTR TK FEEDG appears in the
MEMO. What does it mean?
A reminder to switch the center tank pumps OFF.
pp
108 What does an amber line across the last two
digits of the fuel quantity mean?
ort
G
D
lat
CTR TK FEEDG
Not all the fuel aboard is useable.
B
The Fuel Quantity Indication is inaccurate.
C
A disagreement between fuel measured and fuel
entered on the MCDU has been detected.
=
=
St
rai
nT
ec
hE
DV
Su
A
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
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109 What does this indication for a Center Tank
Pump mean?
It is switched on with the Mode SEL pb in AUTO but
not supplying fuel.
B
It is switched on with the Mode SEL pb in AUTO and
supplying fuel.
C
The center tank is using gravity to supply fuel.
D
It is switched on with the Mode SEL pb in MAN but
not supplying fuel.
ort
G
lat
A
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A320 Series - Technical Examination
pp
110 After engine shutdown, what are your actions to
close the fuel transfer valves?
You have to switch the inner tank pumps off.
B
You have to call maintenance to close the valves.
C
No action is required. The valves will close
automatically during the next refueling.
St
rai
nT
ec
hE
DV
Su
A
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 54 of 57
No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
111 The message OUTER TK FUEL XFRD appears in
the MEMO. What does it mean?
A
Fuel is transferred from the inner tank to the outer
tank.
B
Fuel is transferred from the outer tank to the inner
tank.
C
Fuel is transferred from the inner tank to the center
tank .
D
Fuel is transferred from the center tank to the inner
tank.
tfe
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A320 Series - Technical Examination
St
rai
nT
ec
hE
DV
Su
pp
ort
G
lat
OUTER TK FUEL XFRD
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 55 of 57
No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
112 How has the fuel been transferred from the outer
to the inner tanks?
A
By setting the MODE SEL pb to MAN.
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A320 Series - Technical Examination
The transfer valve has been opened automatically
by the low level sensor in the center tanks.
C
By setting the MODE SEL pb to AUTO.
D
The transfer valve has been opened automatically
by the low level sensor in the inner tank.
St
rai
nT
ec
hE
DV
Su
pp
ort
G
B
lat
OUTER TK FUEL XFRD
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 56 of 57
No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!
113 Why do the center tank pumps switch off
automatically when the slats are extended for
take-off?
To keep the center of gravity as low as possible.
B
During take-off, the center tank fuel is pumped to the
rear to trim the aircraft.
C
To ensure the wing tanks are used for take-off.
D
During take-off, the center tank fuel is gravity fed
only.
pp
ort
G
lat
A
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A320 Series - Technical Examination
2400 lbs
B
3300 lbs
C
4700 lbs.
D
5300 lbs.
St
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Su
114 What is the minimum fuel quantity for take-off?
© 2006 ­ 2011 by StrainTech EDV Support CH ­ 8192 Glattfelden
Page 57 of 57
No part of this paper may be used or reproduced in any form or by any means, or stored in a databse or retrievial sytem, without prior
written permission of the authors!