revision Flashcards by Izzy Lane

when does the pack ram air inlet flap open automatically

after lift off

How well did you know this?

Not at all

Perfectly

what happens when a duct overheat occurs

hot air pressure regulating valve and all trim air valves close

How well did you know this?

Not at all

Perfectly

redundancy in the operation of the pressurisation outflow valves is provided by

two automatic and one manual meaning 3

How well did you know this?

Not at all

Perfectly

what happens when the extract pb is selected to override

system goes to the closed config, air conditioning is added, blower and extract fan keeps running

How well did you know this?

Not at all

Perfectly

the battery is ventilated and cooled by

air drawn from a Venturi in the skin of the ac

How well did you know this?

Not at all

Perfectly

cost index 999 corresponds to

minimum time

How well did you know this?

Not at all

Perfectly

on the FCU you have selected a heading prior to TO with hdg/vs mode after getting airborne the lateral FMA will

ray trk will be engaged at 30ft

How well did you know this?

Not at all

Perfectly

following failure of one FMGC in order to regain the ND you must

select the same range and mode as the other nd

How well did you know this?

Not at all

Perfectly

incorrect statement for annunciators on the MCDU

FAIL amber light indicates the onside FMGC has failed

How well did you know this?

Not at all

Perfectly

the APU has been switched off but the avail lights remains illuminated why could this happen

the apu bleed air was in use

How well did you know this?

Not at all

Perfectly

during apu start the fault light

illuminates amber with an exam caution when an apu auto shut down occurs

How well did you know this?

Not at all

Perfectly

fuel for apu operation is normally supplied from

the left fuel feed line only

How well did you know this?

Not at all

Perfectly

at what point does the CVR stop automatically

5 mins after the 2nd engine shutdown

How well did you know this?

Not at all

Perfectly

what are the emer evac indication in the cabin when evacuation initiated from the cockpit

evac lights flash at fwd and aft attendant panels. evac tone sounds

How well did you know this?

Not at all

Perfectly

regarding the batteries what’s true

during PCP the battery voltage check must be done with the BATT switches off

How well did you know this?

Not at all

Perfectly

regarding flight with batt power only which of the following busbars are powered

hot bus 1 and 2 ac and dc ess bus

How well did you know this?

Not at all

Perfectly

in the event of ac bus 1 and 2 failure in flight, if the RAT fails to auto extend what means are available to deploy the RAT

press MAN ON guarded pb on emer elec pwr panel

How well did you know this?

Not at all

Perfectly

select correct statement concerning OEBS

Red oebs have a significant impact on the safe operation of the ac

How well did you know this?

Not at all

Perfectly

Roxy masks automatically drop if the cabin pressure alt exceeds

14000ft

How well did you know this?

Not at all

Perfectly

how do the crew escape from the cockpit if cockpit door is jammed

escape panel can only be removed from the cockpit side by pulling the quick release pins towards the centre of the flap and kicking the panel open

How well did you know this?

Not at all

Perfectly

what happens when the extract and blower are selected to override

extract fan keeps running
blower fan stops
smoke config
air conditioning air added

How well did you know this?

Not at all

Perfectly

the eng1 (2) fire light remains illuminated until

the fire is extinguished

How well did you know this?

Not at all

Perfectly

what is the function of the gen 1 line pb

when selected off gen 1 is removed from all busses but continues to power one fuel pump in each wing

How well did you know this?

Not at all

Perfectly

following election of flap 1 what’s true

during acceleration following a go around config 1 + f will be result

How well did you know this?

Not at all

Perfectly

when will speed brakes retract auto in flight

config full is selected

what can be overridden by the side stick

low speed stability

in norm law what protections are available

pitch attitude load factor high speed high angle of attach bank angle

what causes reversion to mechanical back up what ac pitch and lateral control is available

loss of all ELACs and SECs: use of THR and rudder

the side stick priority red arrow will illuminate

in front of the pilot losing authority

which flight control computers computes alpha prot, max, VSW based on aerodynamic data and the activation of the protection is computed by which computer

computed by FAC activated by ELAC

regarding max bank angles what's true

in high speed protection the max is 40º (full side stick deflection) and 0º (when side stick neutral)

the alpha lock function inhibits

slat retraction at low speed

which protection is available in alternate law

load factor protection

for what reason would you use the emer cancel pb

used to cancel master cautions (aural, lights and ecam procedures)

false statement on yaw bar

the yaw bar is displayed only during take off roll

what is the function of the system data acquisition concentrators (SDACs)

to generate display of system pages and engine parameters. also to supply info to the FWC for warning messages and alerts

the normal fuel feed sequence is

centre tanks, inner tanks to 750kg each tank, then outer tanks via the inner tanks

with fuel in the centre tank, auto mode is selected and the slats extended in flight the centre tank pumps will

stop

how may a fuel leak be discovered/detected un the flight

by comparing the sum of FOB and fuel used is significantly less than FOB at eng start

what precaution should be taken when you apply gravity fuel feeding

avoid negative g factor

if both transfuse valves in one side fail

the outer cell quantity is boxed amber on the ecam fuel page display

prior to engine start us it possible to pressurise the green system by

using the yellow elec pump and the ptu

whilst on the ground the blue elec pump

will run after first eng start

the air gap above the fluid in the hydraulic reservoir is pressurised by

no1 engine bleed air or the pneumatic system

when is the PTU self tested

during second eng start

the window heat computer provides two heating levels for the windshield

lo level on the ground, normal level in flight

what happens if wing anti nice is selected on when taxying for take off

the wing anti ice valves open for 30 sec only and on lift off they reopen

following landing in heavy rain what is the first actions to protect the avionics vent system from water entry

extract valve to ovrd

following the use of oxygen mask how is the boom mic reestablished

by closing the left door of the storage box and then pressing the TEST slide

above what cabin altitude will the crew oxygen mask auto supply over pressure regardless of the emer pressure selector position

cabin alt exceeds 30000ft

after impact during ditching the lowest point of the passenger exits (aft door) remains above the waterline for more than

7 mins

the red light on an entry/ service door will flash if

the cabin is still pressurised and both engines are shut down with slides disarmed

what actions are required if a windshield crack is detected

diagnosis of the affected ply is required as per qnh procedure before making descent decision

which computer is responsible for the controls all datalink comms and auto select the best available communication media (VHR, HF or SATCOM)

ATSU

controls of the water and waste systems are located on

forward attendant panel

how is a TA intruder (surrounding air traffic) indicated on the nd

amber circle

the landing gear indicator panel on the instrument panel is

connected to LGCIU 1

after landing a flashing green auto brk in the wheel sd page indicated

auto brake has disengaged

the landing gear indicator panel UNLK light will illuminate red if

the gear is not locked in the selected position

at 100kts on take off what is the situation regarding nose wheel steering

rudder steering is available hand wheel steering is not

LG CTL indication appears in amber on the wheel sd with ECAM caution when

there is a disagreement between LG lever and LG position

what is the sequence of events when gravity extension of the gear is performed

safety valve closes then the doors unlock then the gear unlocks

which info is used in order to produce the EGPWS display

a FMGS database and FM1 position

the compass card on the DDRM1 is supplied from

ADIRU 1 or 3

for FM position which of the following statements is incorrect

each FMGC computes a bias vector from its own IRS position to the radio portion or GPIRS position

when the ac is on the ground and if one ADIRU is powered by ac batteries what external warnings are activated

an external horn sounds and the ADIRU and AVNCS light comes on amber on the external power panel

selection of the NAV key on RMP engages the radio navigation back up mode, this action

removes the NAVAIDS tuning capability from both FMGCsw

what is meant by check ATT (amber) on the PFDs

both PFDs show different attitudes: check ISIS in order to identify failed system

which of the following correctly completes the statement switching the apu air bleed on will cause

the crossbleed valve to open and the eng bleed valves to close

regarding operation with high eng thrust the

HP valve closes and the IP stage supplies bleed air

on the eng panel on the centre console the fault light will illuminate

when there is an automatic start abort

after eng master level set to off during parking phase the eng does not shut down as expected due to LP fuel valve remained open which procedure will you follow

eng fire pb sw (affected engine) press

in the event of a hot start during auto engine start the FADEC will

aborts the start, attempts restart, auto cranks and advices shutdown if unsuccessful

LVR ASYM is displayed on FMA if

ATHR active, one THR LVR is in the clb detent and the other one out of the clb detent

how to carry out dry cranking

mode sel crank - eng man start pb ơn

during a relight of engine in flight

FADEC will open the start valve is ac is outside stabilised wind milling envelope

which of the following APU limitations is correct

in emer elec config apu start is limited to 25000ft or below

what is the minimum height for the use of autopilot during take off with SRS mode

100ft

how many times can you reset a cb

once if authorised by the procedure

what is the maximum continuous eng oil temp

140º (155º if for 15mins)

what is the max operating speed VMO/MMO

350 /0.82

what precautions should you take if LP ground air unit is connected

do not use conditioned air simultaneously from PACKS

what is the maximum tyre ground speed

195

what is the max permitted wind speed for passenger door operation

what is the max permitted speed for use of windscreen wipers

230

the ram air inlet should only be used if differential pressure is less than

1 PSI

what is the max speed for landing gear retraction

220

if an inoperative component is not listed specifically in the Mel can the item be deferred for safe operation

according to the ecam handling procedure what must be carried out from memory, without referring to the ecam or qrh procedure

dont sink warning

what are the correct initial actions following a windshear warning on final approach

TOGA thrust - ap if engaged keep on - SRS follow

what are the combined initial actions of the crew in event of a rejected take off at >100kts below V1

call stop - select idle thrust - reverse thrust max

what is the correct immediate pitch attitude and thrust guidance in the event of unreliable IAS indications just after take off

TOGA 15º

which of the following cockpit lights are available when only on batteries

right hand dome light

during a TCAS RA climb procedure if descend descend now audio command is triggered twice what could be happening

the intruders trajectory has changed

in the event of sudden depressurisation at fl300 due to structural failure what are initial actions

emer descent initiate if ATHR is off thr levers idle

during landing with auto brakes selected you realise ac is not slowing down what re correct initial actions

rev max - brake pedals release - asked and nw steering off

if dual SDAC fault

some amber cautions are lost but red warnings are available

which page on the sd can the crew confirm the ldg elev auto info during cockpit prep SOP

press SD

loss of both ecam Du's what is initial actions

rotate the ecam/nd tsfr switch left or right as appropriate

an excessive ils deviation is indicated by

loc and gs scale indications flashing continuously

weather radar images can be displayed on the ND

in all modes except plan

when will the sideslip index change to blue

eng failure at take off or go around

if only one ECAM DU is operative how is advisory shown

ADV is displayed on the EWD the associated ECP button flashes

how is Econ SPEED RANGE SHOW ON SPEED SCALE

magenta bars on the speed tape +/-20

during managed descent pull hdg modes go to

speed / vs / hdg

in the event of both FMGCs failing NAV backup tuning

available one either RMP 1 or 2

if one ap is engaged

the related fmgc is the master

when both CDs are off and AP pb is switched on

the ap engages in VS or FPA depending on FCU selection

the SRS mode disengages auto at

acceleration alt

each fmgc computes a bias vector from its

MIX IRS and radio or GPIRS position

what vertical mode will AP revert to when alt is changed with alt* captured

VS or FPA

ac below 200ft RA LAND mode active with AP on under which conditions will auto land warning not flash

one engine fail

revision Flashcards

(112 cards)