3 Flashcards
(282 cards)
1
Q
If the BSCU fails most likely a BRAKES Sys 1 (2) FAULT may occur
A
The crew will be notfied with an ECAM message
2
Q
The APU bleed valve is automatically closed by the ECB above ….feet climbing
A
25000
3
Q
If there is an APU fire in flight the APU
A
must be shutdown manually and the agent manually discharged
4
Q
Although no busses are unpowered illumination of mergency exist lights in the cabin is desired. Which of the following answers are correct
A
Both answers are correct
5
Q
The fire extinguishing system for the cargo compartement discharges to eiter te FWD cargo of AFT/BULK cargo compartments depending on whether
A
The FWD or AFT Agent PB is pressed
6
Q
What does two amber lines across the last two digits of the fuel quantity mean?
A
The fuel quantity indication is inaccurate
7
Q
The pneumatic system supplies high pressure air for
A
all of the above
8
Q
When can managed vertical navigation be engaged
A
Only after managed lateral navigation has been engaged
9
Q
The audio managment system includes how many audio control panels
A
3
10
Q
The APU is supplying the electrical system. What is the order of priority for the different generators?
A
ENG EXT Power APU
11
Q
When both ENG1 and ENG2 pushbuttons are turned on each engine nacelle is anti iced by
A
Independent bleed air source from HP compressor
12
Q
The cabin pressure controllers receive signals from
A
All of the above
13
Q
In the event of low pressure heavy load users are isolated to give priority to
A
Rudder elevators ailerons spoilers and braiking
14
Q
In the event of low hydraulic pressure the priority valve and pressure maintaining valves give priority to primary flight controls and brakes. The pilots:
A
can neither control nor monitor the priority valve (automatic operation)
15
Q
How many HP ground units can be connected to the crossbleed duct?
A
One or two
16
Q
What happens when pressure and temperature are not sufficient to suplly the corresponding engine bleed valve (low engine speed)
A
HP valve opens IP stage remains open
17
Q
Cabin Interphone system permits you to speak to
A
The cabin attendants
18
Q
What is required for the FADEC to compute a reduced thrust setting?
A
A flex temperature must be entered on the TakeOFF PERF Page on the MCDU
19
Q
With nobody in the cockpit if you have an APU fire which statement is correct
A
On the ground, an APU EMER shutdown will occur and the APU fire bottle will be discharged automatically
20
Q
How are the FMAs displayed on the PFD
A
There are 5 colums and 3 rows
21
Q
At what power level does window heat operate while airborne
A
Normal power while inflight
22
Q
Autobrake if selected will only be activate by
A
The ground spoiler extension command
23
Q
If a flight attendand opens the door with escape slide armed
A
A white warning light warns that the slide is armed
24
Q
During engine start up, when is the BLUE hydraulic system pressurized
A
Automatically after first engine start (ENG1)
25
Ground position determing systems such as VOR DME ILS
cross check and refine the FMGS position computed by indepented systems such as ADIRS
26
Each passenger door has one CABIN PRESSURE warning light that
Warns of residual pressure in the cabin
27
What are the autopilot functions
All of the above
28
The FAULT light for the T.TANK MODE pushbutton switch on the fuel control panel comes on AMBER when
All of the above
29
Hot air from pneumatic system provides wing anti ice to
The four outboard slats
30
During normal flight the avionics ventilation sysytems controls the temperature by
All correct
31
Alpha floor protection is avaiable
From liftoff and down to 100ft RA alt in landing config
32
How is it determined that the cockpit sliding window is closed and locked ?
The red coloured indicator on the top of the handle should be completely flush and the red colour not be visible
33
Automatic transfer from the outer to the inner tanks occures when the center and trim tank have been emptied and either inner tank reaches ......kg
3500kg 7700lbs
34
Automatic control of CG
All of the above
35
When the door arming lever is in the ARM position opening the door from the outside will
Disarm the door
36
The electric standby horizon ISIS normally draws current from the DC ESS BUS. In case of total electrical failure the indicaiton remains usuable for .... minutes
Normal function in EMER ELEC CONFIG
37
What causes a DU to display a black screen with a white diagonal line?
DMC failure
38
Engine fire detection loops are installed in the
Pylon, nacelle, and engine core sections
39
For engine start HP air supplied from the ground air source
is not regulated
40
How does the FMGC derive Vapp
Vapp= Vls + 1/3 surface headwind component or VLS+5kts whichever is highest
41
The fire extinguishing system for the cargo compartment discharges through either the ..... in the FWD compartment or through ..... in the AFT/BULK cargo compartment
Two nozzles / one nozzle each
42
How many thrust lever positions are there and how are they labeled?
There are 4 TL positions; TOGA, FLX MCT, CL, IDLE
43
Which statement is correct regarding the illumination of the Amber BULK ISOL VALVE Fault light?
Either the inlet or outlet isolation valve is not in the selected position
44
The APU master SW FAULT light will illuminate
When an automatic shutdown of the APU occurs
45
You want to open the cabin doo, whilst lifting the control handle the white light illuminates,. What does it mean?
The slide is still armed
46
What are the correct positions of the PFD ND
PFD should be outboard and the ND should be inboard
47
How long does a normal IR alignment take?
approx. 10minutes
48
With the EMER EXIT LIT selector in the ARM position if partial loss of the normal AC power supply
The overhead emergency lights will illuminate automatically
49
The two center tank transfer pumps transfer fuel from the centre tank to the .....tanks
inner
50
The APU generator has priority over .... for AC BUS2
External Power B
51
What is the signification of an amber RAT indicator during Flight phases 1 and 2 (ECAM HYD page)
Pressure for stowing the RAT has been applied or the RAT pump is not avbl
52
Both indepentend cabin pressure controllers receive signals from
LGCIU, ADIRS, FMGEC, PSCU, EIU and flow control valves
53
If the thrust levers are set in the IDLE detent is Alpha floor protection still avbl?
Yes TL position is disregarded
54
There is / are ....HP ground air supply connector(s) located on the lower center fuselage
2
55
Opening a passenger door from outside disarms the door and escape slides
True
56
How can you get mechanics attention when he is outside the aircraft?
Use the EMCH pushbutton on the CALLS panel which sounds an external horn
57
What is required to arm the autobrake
Green hydraulic pressure
anti skid,
no failures in the braing system
58
Illumination of the SEL indicator on a Radio MAnagment PAnel indicates
A transceiver normalley assciated with one RMP is tuned by another
59
The override switch for the service interphone switch is located on the ..... and is used for maintenance purposes only
overhead panel
60
The green hydraulic circuit drives an emergency generator that automatically supplies emergency AC power to the aircraft electrical system in case of a main generators loss
TRUE
61
INFLIGHT a yellow IR FAULT light is steady ON. What does that mean?
The respective IR is lost
62
The APU air intake and an electrically operated flap allow air to reach the compressor inlet
TRUE
63
Which of the following statements is true
The APU is supplied by the trim tank transfer line
64
The APU is fed from the eninge 1 collector in the left inner tank through the APU FWD pump and the APU ISOL valve when
On ground, after two minutes when the trim tank is not refueled
65
Which situation will automatically illuminate the escape path lighting
Loss of power to the DC ESS BUS and the loss of normal electrical power
66
Which one of the following statements is true?
When the engine anti ice is operating continous ignition is autimatically activated
67
While operating on EMER ELEC POWER with the LDG Gear lowered which of the following control laws is in effect?
Direct
68
TAT probes are heated on the ground
FALSE
69
Which of the follwing have automatic fire ext systems?
APU and lavatory waste bins
70
You enter a dark cockpit what action is necessary before checking the main battery voltages
You have to verify that both batteries are off
71
After the engine shutdown, you observe a pulsing STS message. What does this mean?
It is a reminder that the status page holds a maintenance message
72
During a routine flight, which of the following would result after the loss of GEN2 and the subsequent start of the APU?
ENG GEN1 continues to power the AC BUS1 and downstream systems. The APU powers the AC BUS 2 and downstream systems
73
Air bleed from the engines is
cooled by an air to air heat exchanger using air bled from the engine fan
74
How many FADECs are installed in the aircraft?
2 - 1 each engine
75
If VHF3 transmission key illuminated amber showing the word CALL
Indicates SELCAL
76
Automatic cranking is provided
By the FADEC following an automatic start abort
77
What does the HORN shutoff on the EVAC panel do
Silences horn in the cockpit
78
When the thrust levers are moved to the takeoff postion and the FMGS updates its position at takeofff using
The navigation database and the takeoff runway entered into the MCDU by the pilot
79
The .... allows the pilot to select on the ECAM either warning and caution messages or the system and system status messages displayed
ECAM control panel
80
What happens to the cockpit door with electrical failure
it automartically unlocks
81
You are just about to takeoff. You have not inserted a FLEX temp. Can you still takeoff?
Yes but only using TOGA detent
82
On the hydraulic quantity indicator what does the amber level indicate?
The warning level
83
With the engines off if the AVAIL light is illumintated on both the APU START push button and the ECT power push button, what is the active source of electrical power for the ac busses?
The APU
84
APU bleed air supplies the pneumatic system if the APU speed is above
95%
85
After extenting the RAT is is possible to check its position and status?
Yes select the ECAM HYD page
86
With reference to the PROBE/WINDOW heat pb in normal position AUTO which of the following is true?
Window heating comes on automatically after first engine start
87
What does the Low accuracy message mean?
The estimated position uncertainty (EPU) exceeds the RNP
88
What does the LDG GEAR GRVTY EXTN selector handle initiate when selected to DOWN?
Closes HYD cutoff vlv, disengage doors and gear unlocks
89
What is the function of the APU GEN push button located on the overhead elec panel?
When selected to OFF the APU generator field is de-energized
90
What does the AMBER speed brakes mean on the lower ECAM?
Speed brakes are extended and engines not at idle
91
After a single DMC failure, how could a crew member recover the display units?
Rotate the EIS DMC switch on the switching panel to replace the failed DMC with DMC3
92
Which hyd sys supplies pressure to the LDG?
Green
93
When is the SRS active
Both are correct
94
If battery voltage is below minimum how do you charge them
I have to check that the BAT pb are on and switch the external power on
95
The LDG gear consists of
A Two inboard retracting main gears a forward retracting nose gear
96
When the APU fire pb is released out, an electrical signal is sent that
All of the above
97
The pack flow control valve are pneumatically operated and electrially controlled. They closes automatically in case of
All of the above
98
While flying the airplane with ATHR active the speed knob is pulled and turned to a selected speed that happens to be slower than Alpha prot. What speed will the aircraft slow to
VLS
99
What are the different types of flight guidance?
Managed and selected
100
Engine heat sensing is located pylon nacelle, engine core and fan section
True
101
With the EMER Exit LT in arm position which situation will activate the emergency lights and exit signs
DC ESS Bus failed or normal elec power failed
102
The IR FAULT and BAT lights are extinguished what does that mean?
The respective IR is operating normally
103
Leak measurement valve push buttons on the maintenance panel
are for maintenance purposes and ground ops only
104
Each engine bleed system is designed to
All of the above
105
If a BMC fails
The remaining BMC will automatically aussume most of the failed BMCs functions
106
If you have lost the Green system what is lost?
Gear retraction and nose wheel steering
107
A battery fault light will illuminate if
Battery charging current is outside limits
108
With the EMER EXIT LT selector in ARM position if partial loss of the normal AC power supply
The overhead emergency lights will illuminate automatically
109
The Rain RPLNT pb is inhibted on the GRD when the ENG are stopped
TRUE
110
An electric pump can also pressurize the yellow elec system. This pump runs automatically when
All of the above
111
In normal law all protections are active, which of the following is the most complete list
Protections, Load Factor, Pitch attitude, High AOA, Alpha Floor, bank angle, high speed
112
With the pressurization system in the automatic mode, which valves are closed when the ditching pb is seelected on
All valves below the waterline
113
How can the present position of the aircraft be initialized
Present position can be entered on the INIT page of the MCDU
114
The wing fuel transfer valves are
Are electrically held closed
115
During manual start how is the start valve opened
By depressing the ENG start pb on the overhead ppanel while the ENG MODE selector is out of the NORM position
116
In case of FWC1 fault
ECAM operation is not affected because there are two identical FWCs
117
With all fuel pump switches on are wing tank tanks running whie center tank is transferring to inner tanks?
Yes wing tanks are always running
118
The pack flow control valve are pneumatically operated and electrially coontrolled. They close automatically in case of
All of the above
119
What does Horn shutoff on the EVAC panel do?
Silences horn in cockpit
120
The basic element of an APU is a single shaft gas turbine which delivers.......power for driving the accessroy gear box (electrical generator) and produces bleed air (eng starting and pneumatic supply)
mechanical shaft
121
ADIRU 3 includes
ADR3 and IR3
122
With engines off the AVAIL light is illuminated on both the APU START push button and the EXT PWR push button, what is the active source of electrical power for the ac busses
The APU
123
The ac three hydraulic systems are normally pressurized by
At least one engine driven pump and one electric pump
124
The windshear detection function is provided in takeoff and approach phase
After Takeoff 3 s after liftoff up to 1300ft RA
125
Automatic cranking is provided
By the FADEC following an automatic start abort
126
The APU system page will appear on the ECAM
Both are correct
127
Holding the instinctive disconnect push button for more than fifteen seconds will
Disengage A/THR and alpha floor for the remainder of the flight
128
Although no busses are unpowered illumination of emergency exit lights in the cabin is desired. Which of the following answer are correct?
Both answers are correct
129
The APU master sw fault light will illuminate
When an automatic shutdown of the APU occurs
130
The purpose of the RESET position on the LDG gear grvty extn panel is to
Reset the system to the normal extension and retraction mode
131
A DISCH light on either the ENG or APU fire agent pb indicates
The extinguisher has lost pressure
132
One AP can be engaged on the GRD if the engines are not running
This AP will disengage when one engine is started
133
When both ENG1 and 2 pb are turned ON each engine nacelle is anti iced by
Independent bleed air source from HP compressor
134
With the APU running the APU bleed pb selected ON and the XBleed selector to AUTO the APU will:
Supply pneumatic air to both sides of the aircraft because the pneumatic crossbleed valve automatically opens
135
Which statements are true about the 3 PRIM computers
All of the above is correct
136
Can you tune the ILS receivers to different channels
No
137
Warm pre conditoned bleed air enters the cooling path via the ....... and is ducted to the primary heat exchanger
pack flow control valve
138
The Electronic Control Box ECB is primarily a full authority digital controller that performs the APU system logic for all modes of APU operations such as
All of the above is correct
139
Each passenger door has one CABIN PRESSURE warning light that
warns of residual pressure in the cabin
140
The RAT is capable of powering a pump which will pressurize
only the GREEN system
141
The green hydraulic circuit drives an emergency generator that automatically supplies emergency AC power to the aircraft electrical system in case of a main generator loss
True
142
The drain masts are heated after first engine start
False
143
Alpha floor protection is avbl
From liftoff and down to 100ft RA in landing config
144
When fling at cruise altitude the aircraft navigates using radio navaids only
False
145
What is the function os the system data acquisition concentrators SDAC
To supply warning calculators and data to the ECAM and DMC to be displayed
146
The APU will start provided the APU master switch is on the start pb is selected to ON and .....
the APU air intake flap is in the OPEN position
147
Which statement is correct regarding the cockpit voice recorder?
Is automatically energized after the first engine start or five minutes after AC electrical power is applied to the aircraft
148
WX radar can be displayed in what modes on the ND?
All modes except PLAN
149
If one engine anti system fails the second one takes over and provides anti icing for both engines
False
150
The Agent1 or Agent2 disch light comes on .......when the associated fire extinguishing bottle has lost pressure
Amber
151
The avionics OVBD extract valve opens when
All of the above
152
When the APU fire pb is released out an electrical signal is sent that
All of the above
153
There are ..... HP ground air suplly connectors located on the lower center fuselage
2
154
Both cockpit sliding windows can be opened from outside and inside
False
155
You enter a dark cockpit what action is necessary before checking the main battery voltage
You have to verify that both batteries are off
156
The engine bleed fault light illuminates when
All are correct
157
The ...... pb on the ECAM panel cancels an aural warning extinguishes the MASTER WARNING light but does not affect the ECAM msg display
EMER CANC
158
Ground dependent position determining systems such as VOR ILS DME
cross check and refine the FMGS position computed by idnependent systems such as ADIRS
159
When is TO inhibit and LANDING INHIBIT active
TO1500ft AGL and LANDING below 800ft AGL
160
During normal flight the avionics vent system controls the temperature by
All correct
161
In case of green hydraulic system loss what is the correct statement
Gear extension is done by gravity nose wheel steering may be lost and Autobrake is affected
162
The red UNLK indication on the LDG GEAR indicator illuminates
if the Gear is not locked in the selected position
163
When an engine and wing anti ice are in use and a BMC detects a leak
onyl the wing anti ice on the assciated side will be lost
164
The contactor of each TR opens automatically in case of
All above
165
The FWD and main cargo doors are hydraukically supplied by YELLOW system the bulk door is
mechanically locked and manually operated
166
Are there any limitations associated with disconnecting an IDG
Never disconnect an IDG unless the engine is running nor push the IDG disconnect pb for more than 3 seconds
167
High pressure air has....sources
3
168
Is there any inkage between TL and engines
no totally electrical
169
During TO phase
SRS mode will provide guidance to maintain V2+10kts as a speed reference
170
The temeprature of each ac zone is optimized by the zone controller by acting on the ....
trim air valves
171
With the EMER EXIT LT selector in the arm position, if partial loss of the normal AC power supply
the overhead emer lights will illuminate
172
An amber flashing IR fault light indicates that
ATT and HDG information may be recovered in ATT mode
173
If APU is operating in flight
You may use ELEC plus bleed air up to FL225
174
TAT probes are heated on the ground
FALSE
175
Both ECAM screens have failed is it possible to get E/WD indications?
Yes. it must be manually transferred toone of the NDs
176
When the aircraft is in the managed guidance mode, it is
following lateral, vertical and speed profiles as determined by the FMGC
177
When does the RAT deploy
Both engines fail, or G+B HYD LO LVL or G+Y HYD LO LVL
178
Following an Engine 1 Bleed fault why can you only use one pack if WAI is on
Only one ENG bleed sys cannot supply 2 packs and WAI
179
What is the function of the APU GEN pb located on the OVHD panel?
when selected to OFF the APU GEN field is deenergized
180
What is the Alpha Floor protection
It helps to prevent the ac from stalling and protects against WS encounters during TO and LDG
181
The APU BAT PB SW is selected OFF
Both are correct
182
In the event of an aborted TO with Autobrake armed automatic braking is initiated
At ground spoiler extension provided that the speed is above approx. 70kts
183
The wing fuel transfer valves are
all electrically held closed
184
With reference to the PROBE WINDOW HEAT pb in normal position AUTO which of the following is true?
Window heating comes on automatically after the first engine start
185
Rain protection is provided by
rain repellent and windshield wipers
186
The APU bleed valve is automatically closed by the ECB above..... feet climbing
25000
187
If the auto brake system automatically transitions to alternate brakes with the A/Skid & N/W strg switch in the ON position, which of the following will be avbl?
Anti Skid
188
VLS is the lowest speed that the autoflight system will fly the aircraft. This is a dynamic speed corresponding to an Angle of Attack
All of the above
189
Can the APU fire test be performed using battery power only?
yes
190
With the EMER EXIT LT selector in the ARM position which situation will activate the emergency lights and exit signs?
DC ESS BUS failed or normal electrical power failed
191
Each engine bleed system is designed to
All of the above
192
When APU is supplying the packs, the zone controller sends a demand signal to increase flow output when a zone temperature cannot be satisfied. This signal is sent to the
APU ECB
193
Where are the HF antennas located?
Leading edge of rudder
194
The Hydraulic System monitoring unit HSMU controls?
Automatic activation of electric pumps and RAM air turbine extension
195
Alpha floor protection is avbl
from liftoff and down 100ft RA in LDG config
196
The Audio switching rotary selector allows replacement of a failed 1 or 2 ACP with ACP3
True
197
The doors and slides control system DSCS consists of
All of the above
198
What causes a DU to blank
Both are correct
199
Which ACP switch config is correct for communication with other cockpit crew members while wearing a oxygen mask
Both are correct
200
The windshear detection is provided in TO and APP phase
after TO 3s after liftoff up to 1300ft RA
201
If you lost the GREEN system what equipment is lost
The emergency generator
202
The APU generator has priority over .....for AC BUS2
External power B
203
CI 0 corresponds to
Minimum fuel consumption
204
For eng start HP air supplied from the ground source
is not regulated
205
When selected APU bleed air
has priority over engine bleed air
206
What is the function of the black guarded EMER push button on the CALLS panel on the overhead panel
To alert all flight attendant of a pending urgent need to speak with them
207
What is the difference bertween eng and wing anti ice fault lights?
Both indicate valve in transit or valve position disagrees with selected position. Wing light also could indicate low pressure
208
During pushback you starz eng2 you observe the NW STRG DISC memo has changed to amber. Why?
Memo has become amber because one eng is running. This is normal
209
Aural alerts and voice msgs are transmitted
through the loudspeakers even if the speakers are switched off
210
If CP pitot heat has failed
Captain can recover his air data by using air data switching to 3
211
The thrust delivered by ATHR is already at MAX CLB. is it possible to obtain some additional thrust?
Yes by moving the TL FWD from the CL detent
212
Both independent cabin pressure controllers receive signals from
LGCIU ADIRS FMGEC EIU and flow ctrl valves
213
aft cargo indications may be found on which ECAM page
ECAM cruise page and COND page
214
What happens when a discrepancy between signal sent ot E/WD and the feedback signal is detected?
A "CHECK E/WD" msg appears on the upper ECAM and on the ND
215
When in alternate law all protections except Alpha floor will be lost
False
216
The master caution lights and the master caution indication on the ecam illuminate steady amber and are accompanied by a single chime at level .....caution
2
217
What is the signification of an amber RAT indicator during flight phases 1 and 2 (ECAM hyd page)
Pressure for stowing the RAT has been applied or the RAT pump is not avbl
218
When selecting the guarded RMP NAV key
FMGEC auto tuning is inhibted
219
Status page: inop sys indicates ENG1 Loop B
one fire detection loop for engine 1 has failed. fire detection for both engines is avbl
220
Can the crew depress the RMP NAV pb and use the RMP for navigaiotn simultanesouly with FMGC autotuning?
No RMP backup tuning supersedes the autotuning function of both FMGCs
221
The ECB also controls the APU fuel flow
True
222
One RMP gives the flight crew control of all radio comm systems and the other RMP provides backup to FMGCs for controlling rad nav
False
223
What does the RAT MAN ON switch do
Extends RAT pressurizes GREEN sys does NOT start emergency gen
224
While in flight operating normal law with the speed inside the alpha prot range
The side stick controller and flight controls revert to the AOA mode, and side stick defelction is proportional to AOA
225
The APU is fed from engine 1 collector in the left inner tank though the APU FWD pump and the APU ISOL vlv when
on ground after two minutes when the trim tank is not refueled
226
managed guidance is engaged by
pushing on the desired FCU selector knob
227
After an APU fire has been detected for how long will the chime continue to sound
Both are correct
228
The crossbleed valve is automatically controlled to
open when the APU bleed is selected ON and closed when a leak is detected
229
APU fire detection is accomplished by
Two parallel fire detection loops
230
During the ext preflight inspection in what pos would you expect to find the avionics OVBD extract vlv?
Open
231
What is the difference between -FD2 and 2FD2 on the FMA?
1 off 2 engaged / 1 inop 2 engaged
232
With the loss of pneumatic system pressure the engine bleed valve will
Assume the closed position
233
The hot air vlv push buttons controls
The hot air valve controlling pressure upstream of the packs
234
What are the mayor equipment losses with the loss of green system?
NW steering, Autobrakes
235
Insertion or deletion of a holding pattern or change of the SPD target during descend modifies also automatically the DES profile
FALSE
236
If LOW ACCURACY msg is displayed are there any approach restrictions?
Yes both LNAV VNAV app are not allowed
237
Which hyd sys supplies px to the nose wheel steering?
Green
238
Automatic control of CG
All of the above
239
Is it possible to parallel generators?
The elec sys will not allow paralleling of the gen
240
To control the nose wheel steering the BSCU receives inputs from
All of the above
241
When will normal operation of te blue system hydraulic pump begin
During the first eng start
242
Holding the instinctive disconnect button for more than 15sec
disengage the A/THR and Alpha Floor for te remainder of the flight
243
Inflight if both windshield wipers automatic heat has failed
Probe window heat pb should be set ON
244
When does the automatic depressurization sequence occur
on ldg touchdown to be complete latest 80s after landing
245
When is TO inhibit and LDG inhibit active
TO 1500 and LDG 800
246
What are the different air sources for ac and pressurization
ENG bleed air and recirculated air or if selected APU bleed and recirculated air
247
The FPV symbol illustrates the actual track and flight path angle being flown
correct as alt method of indicating FD commands
248
Which of the following is true
The APU is upplied by trim tank transfer line
249
RMP1 is dedicated to which VHF radios
All
250
There are three type of failures. Independent, primary and secondary - what is an indepentend?
a failure that affects an isolated system or item of equipment without degrading the performance of others in the aircraft
251
The avionic comp is accessible through an inward opening manually operated hinged door in the lower fuselage forward of the nose landing gear bay. The avionics compartment is also accesible from the cockpit via a hatch in the floor behind the cp seat a ladder is fixed in the avionics compartment for access to the cp ...
TRUE
252
The rain rplnt is inhibted on the ground when eng are stopped
True
253
In case of green hydraulic loss, what is correct statement
gear ext is done by gravity, nose wheel steering may be lost and antobrake is affected
254
hot air from the pneumatic system provides wing anti ice to
4 outboard slats
255
The LOC mode disengages when
Both are correct
256
What is true about the sideslip indicator beta target
all answers are correct
257
If the upper ecam du fails what will now be displayed at the lower unit?
E/WD
258
When additional pneumatic air is required for anti ice eng starting or aircond :
Add pneu air will be requested by BMC to the FADEC or the APU
259
The avionics compartment is the only are where there is no fire extinguishing system
True
260
If you depress the guarded NAV button the MCDU 'RAD NAV pages are inhibted and the RMP panel is used for navaid tuning
True
261
Takeoff can be performed using which power settings
Flex MCT and TOGA
262
What is the function of the Ram air valve
Cockpit and cabin ventilation in the event of a dual pack failure
263
With the loss of electrical power the WING anti ice valves
fail in closed pos
264
Which one of the following is true
When the engine anti ice is operating continous ignition is automatically activated
265
The ECB controls the APU fuel flow
True
266
How do you erase the CVR
press the erase pb when ac on ground and parking brake set
267
ADIRUS provide nav information
on an independent basis without referencing ground stations or satellites
268
With the EMER EXIT LT selector in the arm pos which situation will activate the emer lights and exit signs
DC ESS BUS failed or normal elec power failed
269
Temperature regulation is achieved b the precooler which regulates and limits the temperature at
200
270
The APU is fed from eng1 collector in left inner tank through the APU FWD pump and the APU isol valve when
On Ground after two minutes when the trim tank is not refueled
271
If the IR mode rotary selector is selected OFF
The ADIRU is not energized AD and IR information is lost
272
What is the max alt for APU
41000
273
What happens to RPM when either eng anti ice vlv is open
n1 limit is automatially reduced idle n1 increased
274
Where is information displayed provided by the DMC1 and DMC2
DMC1 supplies data to PFD1 ND1 and upper ECAM. DMC2 supplies data to PFD2 ND2 and lower ECAM
275
The APU may be started up to what ALT?
APU can be started at any altitude
276
Each engine bleed system is designed to
All of the above
277
Placing the ventilation Extract PB to override
insures the underfloor extract valve closes and the OVBD extract valve partially opens
278
If the APU is operating in flight
you may use elec plus bleed up to FL225
279
How many fire extinguising are there in the APU
1
280
What information is upplied by the IRs and displayed on the PFD
HDG ATT and VS
281
On an autoland approach with both autopilots on which fmgc is master
fmgc1
282
What is indicated by the autobrake DECEL lights
airplane decel is 80% of selected rate
