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Screening > 3 > Flashcards

3 Flashcards

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

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2
Q

The APU bleed valve is automatically closed by the ECB above ….feet climbing

A

25000

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3
Q

If there is an APU fire in flight the APU

A

must be shutdown manually and the agent manually discharged

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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

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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

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6
Q

What does two amber lines across the last two digits of the fuel quantity mean?

A

The fuel quantity indication is inaccurate

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7
Q

The pneumatic system supplies high pressure air for

A

all of the above

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8
Q

When can managed vertical navigation be engaged

A

Only after managed lateral navigation has been engaged

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9
Q

The audio managment system includes how many audio control panels

A

3

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10
Q

The APU is supplying the electrical system. What is the order of priority for the different generators?

A

ENG EXT Power APU

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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

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12
Q

The cabin pressure controllers receive signals from

A

All of the above

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13
Q

In the event of low pressure heavy load users are isolated to give priority to

A

Rudder elevators ailerons spoilers and braiking

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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)

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15
Q

How many HP ground units can be connected to the crossbleed duct?

A

One or two

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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

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17
Q

Cabin Interphone system permits you to speak to

A

The cabin attendants

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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

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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

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20
Q

How are the FMAs displayed on the PFD

A

There are 5 colums and 3 rows

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21
Q

At what power level does window heat operate while airborne

A

Normal power while inflight

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22
Q

Autobrake if selected will only be activate by

A

The ground spoiler extension command

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23
Q

If a flight attendand opens the door with escape slide armed

A

A white warning light warns that the slide is armed

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24
Q

During engine start up, when is the BLUE hydraulic system pressurized

A

Automatically after first engine start (ENG1)

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25
Q

Ground position determing systems such as VOR DME ILS

A

cross check and refine the FMGS position computed by indepented systems such as ADIRS

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26
Q

Each passenger door has one CABIN PRESSURE warning light that

A

Warns of residual pressure in the cabin

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27
Q

What are the autopilot functions

A

All of the above

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28
Q

The FAULT light for the T.TANK MODE pushbutton switch on the fuel control panel comes on AMBER when

A

All of the above

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29
Q

Hot air from pneumatic system provides wing anti ice to

A

The four outboard slats

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30
Q

During normal flight the avionics ventilation sysytems controls the temperature by

A

All correct

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31
Q

Alpha floor protection is avaiable

A

From liftoff and down to 100ft RA alt in landing config

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32
Q

How is it determined that the cockpit sliding window is closed and locked ?

A

The red coloured indicator on the top of the handle should be completely flush and the red colour not be visible

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33
Q

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

A

3500kg 7700lbs

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34
Q

Automatic control of CG

A

All of the above

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35
Q

When the door arming lever is in the ARM position opening the door from the outside will

A

Disarm the door

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36
Q

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

A

Normal function in EMER ELEC CONFIG

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37
Q

What causes a DU to display a black screen with a white diagonal line?

A

DMC failure

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38
Q

Engine fire detection loops are installed in the

A

Pylon, nacelle, and engine core sections

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39
Q

For engine start HP air supplied from the ground air source

A

is not regulated

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40
Q

How does the FMGC derive Vapp

A

Vapp= Vls + 1/3 surface headwind component or VLS+5kts whichever is highest

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41
Q

The fire extinguishing system for the cargo compartment discharges through either the ….. in the FWD compartment or through ….. in the AFT/BULK cargo compartment

A

Two nozzles / one nozzle each

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42
Q

How many thrust lever positions are there and how are they labeled?

A

There are 4 TL positions; TOGA, FLX MCT, CL, IDLE

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43
Q

Which statement is correct regarding the illumination of the Amber BULK ISOL VALVE Fault light?

A

Either the inlet or outlet isolation valve is not in the selected position

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44
Q

The APU master SW FAULT light will illuminate

A

When an automatic shutdown of the APU occurs

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45
Q

You want to open the cabin doo, whilst lifting the control handle the white light illuminates,. What does it mean?

A

The slide is still armed

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46
Q

What are the correct positions of the PFD ND

A

PFD should be outboard and the ND should be inboard

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47
Q

How long does a normal IR alignment take?

A

approx. 10minutes

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48
Q

With the EMER EXIT LIT selector in the ARM position if partial loss of the normal AC power supply

A

The overhead emergency lights will illuminate automatically

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49
Q

The two center tank transfer pumps transfer fuel from the centre tank to the …..tanks

A

inner

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50
Q

The APU generator has priority over …. for AC BUS2

A

External Power B

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51
Q

What is the signification of an amber RAT indicator during Flight phases 1 and 2 (ECAM HYD page)

A

Pressure for stowing the RAT has been applied or the RAT pump is not avbl

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52
Q

Both indepentend cabin pressure controllers receive signals from

A

LGCIU, ADIRS, FMGEC, PSCU, EIU and flow control valves

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53
Q

If the thrust levers are set in the IDLE detent is Alpha floor protection still avbl?

A

Yes TL position is disregarded

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54
Q

There is / are ….HP ground air supply connector(s) located on the lower center fuselage

A

2

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55
Q

Opening a passenger door from outside disarms the door and escape slides

A

True

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56
Q

How can you get mechanics attention when he is outside the aircraft?

A

Use the EMCH pushbutton on the CALLS panel which sounds an external horn

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57
Q

What is required to arm the autobrake

A

Green hydraulic pressure
anti skid,
no failures in the braing system

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58
Q

Illumination of the SEL indicator on a Radio MAnagment PAnel indicates

A

A transceiver normalley assciated with one RMP is tuned by another

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59
Q

The override switch for the service interphone switch is located on the ….. and is used for maintenance purposes only

A

overhead panel

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60
Q

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

A

TRUE

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61
Q

INFLIGHT a yellow IR FAULT light is steady ON. What does that mean?

A

The respective IR is lost

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62
Q

The APU air intake and an electrically operated flap allow air to reach the compressor inlet

A

TRUE

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63
Q

Which of the following statements is true

A

The APU is supplied by the trim tank transfer line

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64
Q

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

A

On ground, after two minutes when the trim tank is not refueled

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65
Q

Which situation will automatically illuminate the escape path lighting

A

Loss of power to the DC ESS BUS and the loss of normal electrical power

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66
Q

Which one of the following statements is true?

A

When the engine anti ice is operating continous ignition is autimatically activated

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67
Q

While operating on EMER ELEC POWER with the LDG Gear lowered which of the following control laws is in effect?

A

Direct

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68
Q

TAT probes are heated on the ground

A

FALSE

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69
Q

Which of the follwing have automatic fire ext systems?

A

APU and lavatory waste bins

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70
Q

You enter a dark cockpit what action is necessary before checking the main battery voltages

A

You have to verify that both batteries are off

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71
Q

After the engine shutdown, you observe a pulsing STS message. What does this mean?

A

It is a reminder that the status page holds a maintenance message

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72
Q

During a routine flight, which of the following would result after the loss of GEN2 and the subsequent start of the APU?

A

ENG GEN1 continues to power the AC BUS1 and downstream systems. The APU powers the AC BUS 2 and downstream systems

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73
Q

Air bleed from the engines is

A

cooled by an air to air heat exchanger using air bled from the engine fan

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74
Q

How many FADECs are installed in the aircraft?

A

2 - 1 each engine

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75
Q

If VHF3 transmission key illuminated amber showing the word CALL

A

Indicates SELCAL

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76
Q

Automatic cranking is provided

A

By the FADEC following an automatic start abort

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77
Q

What does the HORN shutoff on the EVAC panel do

A

Silences horn in the cockpit

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78
Q

When the thrust levers are moved to the takeoff postion and the FMGS updates its position at takeofff using

A

The navigation database and the takeoff runway entered into the MCDU by the pilot

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79
Q

The …. allows the pilot to select on the ECAM either warning and caution messages or the system and system status messages displayed

A

ECAM control panel

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80
Q

What happens to the cockpit door with electrical failure

A

it automartically unlocks

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81
Q

You are just about to takeoff. You have not inserted a FLEX temp. Can you still takeoff?

A

Yes but only using TOGA detent

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82
Q

On the hydraulic quantity indicator what does the amber level indicate?

A

The warning level

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83
Q

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?

A

The APU

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84
Q

APU bleed air supplies the pneumatic system if the APU speed is above

A

95%

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85
Q

After extenting the RAT is is possible to check its position and status?

A

Yes select the ECAM HYD page

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86
Q

With reference to the PROBE/WINDOW heat pb in normal position AUTO which of the following is true?

A

Window heating comes on automatically after first engine start

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87
Q

What does the Low accuracy message mean?

A

The estimated position uncertainty (EPU) exceeds the RNP

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88
Q

What does the LDG GEAR GRVTY EXTN selector handle initiate when selected to DOWN?

A

Closes HYD cutoff vlv, disengage doors and gear unlocks

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89
Q

What is the function of the APU GEN push button located on the overhead elec panel?

A

When selected to OFF the APU generator field is de-energized

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90
Q

What does the AMBER speed brakes mean on the lower ECAM?

A

Speed brakes are extended and engines not at idle

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91
Q

After a single DMC failure, how could a crew member recover the display units?

A

Rotate the EIS DMC switch on the switching panel to replace the failed DMC with DMC3

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92
Q

Which hyd sys supplies pressure to the LDG?

A

Green

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93
Q

When is the SRS active

A

Both are correct

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94
Q

If battery voltage is below minimum how do you charge them

A

I have to check that the BAT pb are on and switch the external power on

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95
Q

The LDG gear consists of

A

A Two inboard retracting main gears a forward retracting nose gear

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96
Q

When the APU fire pb is released out, an electrical signal is sent that

A

All of the above

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97
Q

The pack flow control valve are pneumatically operated and electrially controlled. They closes automatically in case of

A

All of the above

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98
Q

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

A

VLS

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99
Q

What are the different types of flight guidance?

A

Managed and selected

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100
Q

Engine heat sensing is located pylon nacelle, engine core and fan section

A

True

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101
Q

With the EMER Exit LT in arm position which situation will activate the emergency lights and exit signs

A

DC ESS Bus failed or normal elec power failed

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102
Q

The IR FAULT and BAT lights are extinguished what does that mean?

A

The respective IR is operating normally

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103
Q

Leak measurement valve push buttons on the maintenance panel

A

are for maintenance purposes and ground ops only

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104
Q

Each engine bleed system is designed to

A

All of the above

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105
Q

If a BMC fails

A

The remaining BMC will automatically aussume most of the failed BMCs functions

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106
Q

If you have lost the Green system what is lost?

A

Gear retraction and nose wheel steering

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107
Q

A battery fault light will illuminate if

A

Battery charging current is outside limits

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108
Q

With the EMER EXIT LT selector in ARM position if partial loss of the normal AC power supply

A

The overhead emergency lights will illuminate automatically

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109
Q

The Rain RPLNT pb is inhibted on the GRD when the ENG are stopped

A

TRUE

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110
Q

An electric pump can also pressurize the yellow elec system. This pump runs automatically when

A

All of the above

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111
Q

In normal law all protections are active, which of the following is the most complete list

A

Protections, Load Factor, Pitch attitude, High AOA, Alpha Floor, bank angle, high speed

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112
Q

With the pressurization system in the automatic mode, which valves are closed when the ditching pb is seelected on

A

All valves below the waterline

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113
Q

How can the present position of the aircraft be initialized

A

Present position can be entered on the INIT page of the MCDU

114
Q

The wing fuel transfer valves are

A

Are electrically held closed

115
Q

During manual start how is the start valve opened

A

By depressing the ENG start pb on the overhead ppanel while the ENG MODE selector is out of the NORM position

116
Q

In case of FWC1 fault

A

ECAM operation is not affected because there are two identical FWCs

117
Q

With all fuel pump switches on are wing tank tanks running whie center tank is transferring to inner tanks?

A

Yes wing tanks are always running

118
Q

The pack flow control valve are pneumatically operated and electrially coontrolled. They close automatically in case of

A

All of the above

119
Q

What does Horn shutoff on the EVAC panel do?

A

Silences horn in cockpit

120
Q

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)

A

mechanical shaft

121
Q

ADIRU 3 includes

A

ADR3 and IR3

122
Q

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

A

The APU

123
Q

The ac three hydraulic systems are normally pressurized by

A

At least one engine driven pump and one electric pump

124
Q

The windshear detection function is provided in takeoff and approach phase

A

After Takeoff 3 s after liftoff up to 1300ft RA

125
Q

Automatic cranking is provided

A

By the FADEC following an automatic start abort

126
Q

The APU system page will appear on the ECAM

A

Both are correct

127
Q

Holding the instinctive disconnect push button for more than fifteen seconds will

A

Disengage A/THR and alpha floor for the remainder of the flight

128
Q

Although no busses are unpowered illumination of emergency exit lights in the cabin is desired. Which of the following answer are correct?

A

Both answers are correct

129
Q

The APU master sw fault light will illuminate

A

When an automatic shutdown of the APU occurs

130
Q

The purpose of the RESET position on the LDG gear grvty extn panel is to

A

Reset the system to the normal extension and retraction mode

131
Q

A DISCH light on either the ENG or APU fire agent pb indicates

A

The extinguisher has lost pressure

132
Q

One AP can be engaged on the GRD if the engines are not running

A

This AP will disengage when one engine is started

133
Q

When both ENG1 and 2 pb are turned ON each engine nacelle is anti iced by

A

Independent bleed air source from HP compressor

134
Q

With the APU running the APU bleed pb selected ON and the XBleed selector to AUTO the APU will:

A

Supply pneumatic air to both sides of the aircraft because the pneumatic crossbleed valve automatically opens

135
Q

Which statements are true about the 3 PRIM computers

A

All of the above is correct

136
Q

Can you tune the ILS receivers to different channels

A

No

137
Q

Warm pre conditoned bleed air enters the cooling path via the ……. and is ducted to the primary heat exchanger

A

pack flow control valve

138
Q

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

A

All of the above is correct

139
Q

Each passenger door has one CABIN PRESSURE warning light that

A

warns of residual pressure in the cabin

140
Q

The RAT is capable of powering a pump which will pressurize

A

only the GREEN system

141
Q

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

A

True

142
Q

The drain masts are heated after first engine start

A

False

143
Q

Alpha floor protection is avbl

A

From liftoff and down to 100ft RA in landing config

144
Q

When fling at cruise altitude the aircraft navigates using radio navaids only

A

False

145
Q

What is the function os the system data acquisition concentrators SDAC

A

To supply warning calculators and data to the ECAM and DMC to be displayed

146
Q

The APU will start provided the APU master switch is on the start pb is selected to ON and …..

A

the APU air intake flap is in the OPEN position

147
Q

Which statement is correct regarding the cockpit voice recorder?

A

Is automatically energized after the first engine start or five minutes after AC electrical power is applied to the aircraft

148
Q

WX radar can be displayed in what modes on the ND?

A

All modes except PLAN

149
Q

If one engine anti system fails the second one takes over and provides anti icing for both engines

A

False

150
Q

The Agent1 or Agent2 disch light comes on …….when the associated fire extinguishing bottle has lost pressure

A

Amber

151
Q

The avionics OVBD extract valve opens when

A

All of the above

152
Q

When the APU fire pb is released out an electrical signal is sent that

A

All of the above

153
Q

There are ….. HP ground air suplly connectors located on the lower center fuselage

A

2

154
Q

Both cockpit sliding windows can be opened from outside and inside

A

False

155
Q

You enter a dark cockpit what action is necessary before checking the main battery voltage

A

You have to verify that both batteries are off

156
Q

The engine bleed fault light illuminates when

A

All are correct

157
Q

The …… pb on the ECAM panel cancels an aural warning extinguishes the MASTER WARNING light but does not affect the ECAM msg display

A

EMER CANC

158
Q

Ground dependent position determining systems such as VOR ILS DME

A

cross check and refine the FMGS position computed by idnependent systems such as ADIRS

159
Q

When is TO inhibit and LANDING INHIBIT active

A

TO1500ft AGL and LANDING below 800ft AGL

160
Q

During normal flight the avionics vent system controls the temperature by

A

All correct

161
Q

In case of green hydraulic system loss what is the correct statement

A

Gear extension is done by gravity nose wheel steering may be lost and Autobrake is affected

162
Q

The red UNLK indication on the LDG GEAR indicator illuminates

A

if the Gear is not locked in the selected position

163
Q

When an engine and wing anti ice are in use and a BMC detects a leak

A

onyl the wing anti ice on the assciated side will be lost

164
Q

The contactor of each TR opens automatically in case of

A

All above

165
Q

The FWD and main cargo doors are hydraukically supplied by YELLOW system the bulk door is

A

mechanically locked and manually operated

166
Q

Are there any limitations associated with disconnecting an IDG

A

Never disconnect an IDG unless the engine is running nor push the IDG disconnect pb for more than 3 seconds

167
Q

High pressure air has….sources

A

3

168
Q

Is there any inkage between TL and engines

A

no totally electrical

169
Q

During TO phase

A

SRS mode will provide guidance to maintain V2+10kts as a speed reference

170
Q

The temeprature of each ac zone is optimized by the zone controller by acting on the ….

A

trim air valves

171
Q

With the EMER EXIT LT selector in the arm position, if partial loss of the normal AC power supply

A

the overhead emer lights will illuminate

172
Q

An amber flashing IR fault light indicates that

A

ATT and HDG information may be recovered in ATT mode

173
Q

If APU is operating in flight

A

You may use ELEC plus bleed air up to FL225

174
Q

TAT probes are heated on the ground

A

FALSE

175
Q

Both ECAM screens have failed is it possible to get E/WD indications?

A

Yes. it must be manually transferred toone of the NDs

176
Q

When the aircraft is in the managed guidance mode, it is

A

following lateral, vertical and speed profiles as determined by the FMGC

177
Q

When does the RAT deploy

A

Both engines fail, or G+B HYD LO LVL or G+Y HYD LO LVL

178
Q

Following an Engine 1 Bleed fault why can you only use one pack if WAI is on

A

Only one ENG bleed sys cannot supply 2 packs and WAI

179
Q

What is the function of the APU GEN pb located on the OVHD panel?

A

when selected to OFF the APU GEN field is deenergized

180
Q

What is the Alpha Floor protection

A

It helps to prevent the ac from stalling and protects against WS encounters during TO and LDG

181
Q

The APU BAT PB SW is selected OFF

A

Both are correct

182
Q

In the event of an aborted TO with Autobrake armed automatic braking is initiated

A

At ground spoiler extension provided that the speed is above approx. 70kts

183
Q

The wing fuel transfer valves are

A

all electrically held closed

184
Q

With reference to the PROBE WINDOW HEAT pb in normal position AUTO which of the following is true?

A

Window heating comes on automatically after the first engine start

185
Q

Rain protection is provided by

A

rain repellent and windshield wipers

186
Q

The APU bleed valve is automatically closed by the ECB above….. feet climbing

A

25000

187
Q

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?

A

Anti Skid

188
Q

VLS is the lowest speed that the autoflight system will fly the aircraft. This is a dynamic speed corresponding to an Angle of Attack

A

All of the above

189
Q

Can the APU fire test be performed using battery power only?

A

yes

190
Q

With the EMER EXIT LT selector in the ARM position which situation will activate the emergency lights and exit signs?

A

DC ESS BUS failed or normal electrical power failed

191
Q

Each engine bleed system is designed to

A

All of the above

192
Q

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

A

APU ECB

193
Q

Where are the HF antennas located?

A

Leading edge of rudder

194
Q

The Hydraulic System monitoring unit HSMU controls?

A

Automatic activation of electric pumps and RAM air turbine extension

195
Q

Alpha floor protection is avbl

A

from liftoff and down 100ft RA in LDG config

196
Q

The Audio switching rotary selector allows replacement of a failed 1 or 2 ACP with ACP3

A

True

197
Q

The doors and slides control system DSCS consists of

A

All of the above

198
Q

What causes a DU to blank

A

Both are correct

199
Q

Which ACP switch config is correct for communication with other cockpit crew members while wearing a oxygen mask

A

Both are correct

200
Q

The windshear detection is provided in TO and APP phase

A

after TO 3s after liftoff up to 1300ft RA

201
Q

If you lost the GREEN system what equipment is lost

A

The emergency generator

202
Q

The APU generator has priority over …..for AC BUS2

A

External power B

203
Q

CI 0 corresponds to

A

Minimum fuel consumption

204
Q

For eng start HP air supplied from the ground source

A

is not regulated

205
Q

When selected APU bleed air

A

has priority over engine bleed air

206
Q

What is the function of the black guarded EMER push button on the CALLS panel on the overhead panel

A

To alert all flight attendant of a pending urgent need to speak with them

207
Q

What is the difference bertween eng and wing anti ice fault lights?

A

Both indicate valve in transit or valve position disagrees with selected position. Wing light also could indicate low pressure

208
Q

During pushback you starz eng2 you observe the NW STRG DISC memo has changed to amber. Why?

A

Memo has become amber because one eng is running. This is normal

209
Q

Aural alerts and voice msgs are transmitted

A

through the loudspeakers even if the speakers are switched off

210
Q

If CP pitot heat has failed

A

Captain can recover his air data by using air data switching to 3

211
Q

The thrust delivered by ATHR is already at MAX CLB. is it possible to obtain some additional thrust?

A

Yes by moving the TL FWD from the CL detent

212
Q

Both independent cabin pressure controllers receive signals from

A

LGCIU ADIRS FMGEC EIU and flow ctrl valves

213
Q

aft cargo indications may be found on which ECAM page

A

ECAM cruise page and COND page

214
Q

What happens when a discrepancy between signal sent ot E/WD and the feedback signal is detected?

A

A “CHECK E/WD” msg appears on the upper ECAM and on the ND

215
Q

When in alternate law all protections except Alpha floor will be lost

A

False

216
Q

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

A

2

217
Q

What is the signification of an amber RAT indicator during flight phases 1 and 2 (ECAM hyd page)

A

Pressure for stowing the RAT has been applied or the RAT pump is not avbl

218
Q

When selecting the guarded RMP NAV key

A

FMGEC auto tuning is inhibted

219
Q

Status page: inop sys indicates ENG1 Loop B

A

one fire detection loop for engine 1 has failed. fire detection for both engines is avbl

220
Q

Can the crew depress the RMP NAV pb and use the RMP for navigaiotn simultanesouly with FMGC autotuning?

A

No RMP backup tuning supersedes the autotuning function of both FMGCs

221
Q

The ECB also controls the APU fuel flow

A

True

222
Q

One RMP gives the flight crew control of all radio comm systems and the other RMP provides backup to FMGCs for controlling rad nav

A

False

223
Q

What does the RAT MAN ON switch do

A

Extends RAT pressurizes GREEN sys does NOT start emergency gen

224
Q

While in flight operating normal law with the speed inside the alpha prot range

A

The side stick controller and flight controls revert to the AOA mode, and side stick defelction is proportional to AOA

225
Q

The APU is fed from engine 1 collector in the left inner tank though the APU FWD pump and the APU ISOL vlv when

A

on ground after two minutes when the trim tank is not refueled

226
Q

managed guidance is engaged by

A

pushing on the desired FCU selector knob

227
Q

After an APU fire has been detected for how long will the chime continue to sound

A

Both are correct

228
Q

The crossbleed valve is automatically controlled to

A

open when the APU bleed is selected ON and closed when a leak is detected

229
Q

APU fire detection is accomplished by

A

Two parallel fire detection loops

230
Q

During the ext preflight inspection in what pos would you expect to find the avionics OVBD extract vlv?

A

Open

231
Q

What is the difference between -FD2 and 2FD2 on the FMA?

A

1 off 2 engaged / 1 inop 2 engaged

232
Q

With the loss of pneumatic system pressure the engine bleed valve will

A

Assume the closed position

233
Q

The hot air vlv push buttons controls

A

The hot air valve controlling pressure upstream of the packs

234
Q

What are the mayor equipment losses with the loss of green system?

A

NW steering, Autobrakes

235
Q

Insertion or deletion of a holding pattern or change of the SPD target during descend modifies also automatically the DES profile

A

FALSE

236
Q

If LOW ACCURACY msg is displayed are there any approach restrictions?

A

Yes both LNAV VNAV app are not allowed

237
Q

Which hyd sys supplies px to the nose wheel steering?

A

Green

238
Q

Automatic control of CG

A

All of the above

239
Q

Is it possible to parallel generators?

A

The elec sys will not allow paralleling of the gen

240
Q

To control the nose wheel steering the BSCU receives inputs from

A

All of the above

241
Q

When will normal operation of te blue system hydraulic pump begin

A

During the first eng start

242
Q

Holding the instinctive disconnect button for more than 15sec

A

disengage the A/THR and Alpha Floor for te remainder of the flight

243
Q

Inflight if both windshield wipers automatic heat has failed

A

Probe window heat pb should be set ON

244
Q

When does the automatic depressurization sequence occur

A

on ldg touchdown to be complete latest 80s after landing

245
Q

When is TO inhibit and LDG inhibit active

A

TO 1500 and LDG 800

246
Q

What are the different air sources for ac and pressurization

A

ENG bleed air and recirculated air or if selected APU bleed and recirculated air

247
Q

The FPV symbol illustrates the actual track and flight path angle being flown

A

correct as alt method of indicating FD commands

248
Q

Which of the following is true

A

The APU is upplied by trim tank transfer line

249
Q

RMP1 is dedicated to which VHF radios

A

All

250
Q

There are three type of failures. Independent, primary and secondary - what is an indepentend?

A

a failure that affects an isolated system or item of equipment without degrading the performance of others in the aircraft

251
Q

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 …

A

TRUE

252
Q

The rain rplnt is inhibted on the ground when eng are stopped

A

True

253
Q

In case of green hydraulic loss, what is correct statement

A

gear ext is done by gravity, nose wheel steering may be lost and antobrake is affected

254
Q

hot air from the pneumatic system provides wing anti ice to

A

4 outboard slats

255
Q

The LOC mode disengages when

A

Both are correct

256
Q

What is true about the sideslip indicator beta target

A

all answers are correct

257
Q

If the upper ecam du fails what will now be displayed at the lower unit?

A

E/WD

258
Q

When additional pneumatic air is required for anti ice eng starting or aircond :

A

Add pneu air will be requested by BMC to the FADEC or the APU

259
Q

The avionics compartment is the only are where there is no fire extinguishing system

A

True

260
Q

If you depress the guarded NAV button the MCDU ‘RAD NAV pages are inhibted and the RMP panel is used for navaid tuning

A

True

261
Q

Takeoff can be performed using which power settings

A

Flex MCT and TOGA

262
Q

What is the function of the Ram air valve

A

Cockpit and cabin ventilation in the event of a dual pack failure

263
Q

With the loss of electrical power the WING anti ice valves

A

fail in closed pos

264
Q

Which one of the following is true

A

When the engine anti ice is operating continous ignition is automatically activated

265
Q

The ECB controls the APU fuel flow

A

True

266
Q

How do you erase the CVR

A

press the erase pb when ac on ground and parking brake set

267
Q

ADIRUS provide nav information

A

on an independent basis without referencing ground stations or satellites

268
Q

With the EMER EXIT LT selector in the arm pos which situation will activate the emer lights and exit signs

A

DC ESS BUS failed or normal elec power failed

269
Q

Temperature regulation is achieved b the precooler which regulates and limits the temperature at

A

200

270
Q

The APU is fed from eng1 collector in left inner tank through the APU FWD pump and the APU isol valve when

A

On Ground after two minutes when the trim tank is not refueled

271
Q

If the IR mode rotary selector is selected OFF

A

The ADIRU is not energized AD and IR information is lost

272
Q

What is the max alt for APU

A

41000

273
Q

What happens to RPM when either eng anti ice vlv is open

A

n1 limit is automatially reduced idle n1 increased

274
Q

Where is information displayed provided by the DMC1 and DMC2

A

DMC1 supplies data to PFD1 ND1 and upper ECAM. DMC2 supplies data to PFD2 ND2 and lower ECAM

275
Q

The APU may be started up to what ALT?

A

APU can be started at any altitude

276
Q

Each engine bleed system is designed to

A

All of the above

277
Q

Placing the ventilation Extract PB to override

A

insures the underfloor extract valve closes and the OVBD extract valve partially opens

278
Q

If the APU is operating in flight

A

you may use elec plus bleed up to FL225

279
Q

How many fire extinguising are there in the APU

A

1

280
Q

What information is upplied by the IRs and displayed on the PFD

A

HDG ATT and VS

281
Q

On an autoland approach with both autopilots on which fmgc is master

A

fmgc1

282
Q

What is indicated by the autobrake DECEL lights

A

airplane decel is 80% of selected rate

Screening (6 decks)

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