ORAL QUESTIONS Flashcards - Course Hero

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What is the difference between the green andblack circuit breakers

The green circuit breakers will show on ECAMthe black ones will not

Why do some of the circuit breakers have redcollars

These are for the wing tip brakes and cannot bereset if pulled

When would you use AUDIO SWITCHING In the case of an individual ACP failure Theselector enables the CA or FO to utilize theoverhead ACP3

What are the ADIRS Combined ADR (external probes) and IR(position amp nav) computer which supplies datato many users

What are some of the parameters the ADRprovides

Altitude airspeed (IASMach) AOA temperatureand overspeed warnings

What are some of the parameters the IRprovides

Heading position attitude ground speed FPVtrack and accelerations

If the IR 1 fault light illuminated what are someprimary ECAM actions you might see

Select IR1 to OFF and the ATTHDG selector toCAPT 3 on EIS switching panel

If the ADR of 1 ADIRU failed what are some ofthe ECAM procedures you would expect to see

Select AIR DATA (switching panel) to CAPT 3 toallow ADR3 to replace ADR1 Then ADR 1 off

Talk through the ADIRS power up procedure andinitialization

Switch each IR to NAV Look for the ON BAT lightillumination Then observe a steady white ALIGNlight Enter PPOS by inserting the starting airportinto the MCDU and select ALIGN IRS prompt

ORAL QUESTIONSA320

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Quiz



Why is it important to observe the ON BAT lightduring IR initialization

To ensure that a good test has been completedA good test will confirm that at least one IR canbe powered by the aircraft batteries in the eventof power loss

Does the ON BAT light illuminate during a fastalign

No

What could cause the flashing white ALIGN lightto illuminate on the ground

No PPOS entered after 10 minutes 1 degree ofdifference in the last known LATLONG or theaircraft was moved during the initial alignment(Not in Rev 1A)

What are some external indications that theADIRS have reverted to battery power on theground

The ADIRU amp AVNCS light will illuminate on theexternal power panel and an external horn willsound

What does a steady FAULT light on the IRindicate

The IR has failed

What does a flashing FAULT light on the IRindicate

The IR has failed but heading and attitude maystill be recovered (turn the selector to ATT)

Can the ADR be turned off without losing the IRfunctions

Yes Select the ADR switch to OFF

Can an IR be turned off without losing the ADRfunctions

No Turning off the IR will also turn off the ADR

What would a flight control consequence be ifyou lost two IRs

You would be in Alternate Law with someprotections lost Also the autopilot andautothrust may be unavailable

What kind of flight control system does theAirbus A320 have

Fly by wire

How are the flight controls controlled andactivated

The flight surfaces are electrically commandedand hydraulically actuated

How is NORMAL LAW indicated on the PFD You will see green equals marks at 67 degrees ofbank 30 degrees pitch up 15 degrees pitchdown and on the speed tape at VMO + 6kts

How is ALTERNATE LAW indicated on the PFD The normal green equals marks will be replacedwith amber xs at pitch and bank limits Atraditional barber pole shows on the speed tape

How is DIRECT LAW indicated on the PFD USE MANUAL PITCH TRIM

How is MECHANICAL BACKUP indicated on the MAN PITCH TRIM ONLY shows in red on the PFD



PFD plus the amber xs associated with alternate law

When operating in NORMAL LAW what does theside stick command for pitch and roll

The sidestick commands a load factor for pitchand a roll rate for roll

What does a RED ARROW light on the glareshieldindicate

A priority takeover has been made by the otherpilot You have lost priority

Name the flight control computers on board theAirbus A320

ELAC 12 (Elevator Aileron Computer) SEC 123(Spoiler Elevator Computer) FAC 12 (FlightAugmentation Computer)

What are some of the ELAC functions Normal elevator THS (trimmable horizontalstabilizer) and aileron control

What are some of the SEC functions Normal spoiler control The SEC also providesstandby elevator and THS control

What does SEC 3 control Number 1 (nearest fuselage) spoilers on theground and number 2 spoilers for roll control ampspeedbrakes in flight

What are some of the FAC functions Rudder movementtrimlimiter yaw dampingspeed protections and windshear protection

What should happen to the THS after landing It will return to the zero position 5 seconds aftertouchdown

Explain the spoiler extension logic on landing fora full extension to occur

Both MLG on the ground and both thrust leversat idle will immediately extend spoilers if armed(if not armed they will deploy after reverse isselected)

Explain the spoiler extension logic on landing fora partial extension to occur

If one MLG is on the ground and at least onereverser is selected partial spoiler deploymentwill occur (10 degrees)

Explain the spoiler extension logic in the eventof a rejected takeoff

If speed is above 72kts the spoilers will deploy(if armed)if the thrust levers are moved to idle Ifnot armed the spoilers will deploy with reversethrust selected

In normal law when descending through 50ftthe pitch is memorized What happens at 30ft

You enter FLARE mode The pitch is reduced to25 degrees down over 8 seconds requiring aflare from the pilot

With the AP on what speed brake lever positionresults in the max available spoiler surfaceextension (A320)

Half speedbrake selected



From takeoff to touchdown in normal law whenis alpha floor protection available

From liftoff to 100ft RA on landing

What does the red FAULT light on the RAT ampEMER GEN switch mean

The emergency generator is not producingpower with AC BUS 1 amp 2 unpowered in flight

When would the red FAULT light on the RAT ampEMER GEN normally illuminate

During the dropping and initial spool up of theRAT (8 seconds) and then below 100 kts

How can the emergency RAT be deployed Push the guarded RAT switch on the EMER ELECpanel or HYD (for blue system power only)

What does the emergency RAT supply It powers the hydraulic blue system which drivesthe emergency generator to supply the AC ESSbus (and DC ESS through the ESS TR)

What electrical buses are powered by theemergency electrical generator

AC ESS BUS (plus the DC ESS BUS through theESS TR)

What is different between selecting theemergency genrator using the HYD button andan automatic RAT drop

Pushing the HYD RAT button will only allow theRAT to power the blue hydraulic system An autoextension will power the electrical system aswell

After deploying the RAT using the HYD panelhow could you then extract electrical power

Push the guarded MAN ON switch on the EMERELEC panel However if the auto system triggerselectrical power will be supplied automaticallywithout pushing the MAN ON switch

What would cause the GEN 1 LINE SMOKE lightto illuminate

Avionics smoke detected (also blower andextract FAULT lights would be illuminated)

An ECAM procedure directs you to turn the GEN1 LINE PB to OFF What is accomplished

The GEN 1 contactor opens and directs GEN 1 topower a fuel pump in each wing

With the GEN 1 LINE PB selected OFF would youexpect the ECAMQRH to direct a landing in theEmergency Electrical Configuration

No On landing gear extension the GEN 1 LINE isrestored enabling normal electricalconfiguration for landing

Which RMPs work during an EmergencyElectrical Configuration

RMP 1 only

Why is the GND CTRL button selected on duringthe pre-flight flow

To ensure that the checklist and briefings arecaptured before flight

If the GND CTL button was not selected on howwould the system work in automatic mode

The CVR is on for 5 minutes after electricalpower is first applied then off until the firstengine starts It stays on until 5 minutes afterthe last engine is shutdown



How do we capture the ITL PA recording on theCVR

The ACP 3 PA intercom is selected on and thevolume is set to 1 oclock position

What does the SYS ON light on the oxygen panelindicate

An electronic signal has been sent to the maskscommanding them to drop

The SYS ON light is on (oxygen panel) Does thismean that the masks have all deployed

Not necessarily The SYS ON only confirms thatthe signal to drop the masks has been sent

What will cause an automatic deployment of thecabin oxygen masks

When the cabin pressure exceeds 14000ft(+250ft to -750ft range)

How does the passenger oxygen system work A chemical generator supplies oxygen when themasks are pulled towards the user Approx 15minutes of oxygen is available per mask

What happens when the CREW SUPPLY button ispushed on the oxygen panel

This opens the oxygen supply valve to suppliesoxygen to the cockpit mask distributionmanifold

Where are the engine fire loops installed In the fan pylon and core

What happens if both fire loops failsimultaneously

A fire warning is triggered if this occurs within 5seconds

What does the amber DISCH light indicate onthe fire button

After arming a low pressure is sensed in the firebottle

How many fire bottles per engine are there Two halon extinguishers per engine

What happens when the engine fire button ispushed

Silences warnings and arms the squibs The fuelSOV hyd SOV engine bleed valve and pack flowvalves close The FADEC is disconnected and theGEN is de-energized

What happens when the ENG FIRE test button ispressed

The CRC sounds master warning lights flashFIRE PB amp DISCH lights illuminate thrust firelight illuminates and the ECAM fire warningshows

What will happen if the APU is operating and anAPU fire is detected

On the ground the APU will auto shutdown after3 seconds and an external horn will sound Inflight a normal fire warning will sound

Name the three hydraulic systems Green Yellow Blue

How is each hydraulic system powered GREEN = Engine and PTU BLUE = Electric andemergency RAT YELLOW = Engine electric PTUand hand pump



When does the blue hydraulic system normallyoperate

After the first engine start

The emergency RAT supplies the blue hydraulicsystem Does the RAT automatically drop if bluepressure is lost

No

What can be done to correct low brakeaccumulator pressure

Turn on the yellow electric pump to recharge thesystem (after checking with the ground crew)

Can the green hydraulic system be powered onthe ground with both engines off

Yes via the yellow electric pump and the PTU

With no hydraulic system power available howcan the cargo door be opened

Using the yellow system hand pump

When will the PTU automatically operate When a difference of gt500psi between the greenand yellow systems is detected The PTU isinhibited during the first engine start testedduring the second start and is inhibited for 40seconds after cargo door operation

What are some of the users of the greenhydraulic system

Landing gear slatsflaps normal brakes 1reverser and flight controls

What are some of the users of the bluehydraulic system

Emergency generator slats and flight controls

What are some of the users of the yellowhydraulic system

NWS alternate brakes parking brake 2reverser cargo door and flight controls

What do the hydraulic priority valves do They shut off big hydraulic users to protect theflight controls in a low pressure situation

What would cause a FAULT light in the hydraulicENG 1 pump

Low reservoir fluid level low reservoir pressurelow pump pressure or reservoir overheat

The FAULT light on the yellow electric pump willilluminate for one item that does not illuminatethe engine hydraulic FAULT light What is it

A pump overheat

How do you know which fault has occurred if theFAULT light is illuminated on the ENG 1 hydraulicpump

The ECAM will display the fault details

Describe the layout of the fuel tanks in theA320

Two wing tanks divided into an inner outer andvent tank One center tank

Generally speaking what is the total fuel Our general maximum fuel total is 42000lbs



capacity (N521-524 amp 621-632 amp 639 = 42300lbs) (N525-530 amp 633-onwards = 42900lbs)

How can the fuel total read 42200lbs on ECAMwhen fueled to maximum capacity

There is a 2 provision for heat expansion up to20 degrees C

Where are the fuel pumps located There are 2 center tank pumps and 2 wing tankpumps per wing The APU has its own pumpwhich runs when the center tank pumps are off

Is there any difference between the center andwing tank pumps

They are identical pumps but the center pumpshave a greater output flow

Explain the flow of fuel from after engine start toslats retracted (assume full tanks)

The center tanks feed the engines for 2 minutesafter engine start After takeoff with slatsretracted and 1100lbs burned from the wingtanks the center tanks will run

What does a FAULT light in one of the enginefuel pumps indicate

Low pump pressure

How are the IDGs cooled Using fuel which is returned to the outer wingtank If the outer tank is full it will spill into theinner tank

What does a FAULT light in the fuel modeselector indicate

Auto logic mode has failed The center tank hasmore than 550lbs of fuel with either wing tankhaving less than 11000lbs

How is fueling progress indicated to the pilots REFUELG is shown in green on the upper ECAM

Where does the IDG cooling fuel return to The outer wing tanks via the fuel return valve Ifthe outer wing tank is full the fuel will transferto the inner tank using a spill pipe

What if the return IDG cooling fuel fills the wingtanks with the center tanks feeding

The center pumps will shut off until 1100lbs isburned from the wing tanks Then the centertanks will run again

What is the minimum battery voltage 255 volts

What should be done of the battery voltagedrops below 255V on the ground

Connect external power and turn the batteryswitches to ON

Explain how to conduct the battery check duringthe first flight cockpit set-up

Select the ELEC page Turn BAT 1amp2 off thenback on Check to see that the charge currentdrops below 60 amps in 10 seconds

Is the main electrical power system AC or DC AC



If all AC is lost what electrical busses will bepowered without the RAT on-line

Battery 1 supplies the AC static inverter andpowers the AC ESS BUS Battery 2 supplies theDC ESS BUS

The engine GEN FAULT is illuminated beforeengine start Is this normal

Yes

What is an IDG Integrated Drive Generator An engine drivenconstant speed drive unit for electricalgeneration

How does an IDG operate Variable engine RPM is converted to a constantspeed to supply electrical generators

What precaution should be observed ifdisconnecting the IDG

Do not hold the switch for more than 3 secondsto avoid damage Do not push when the engineis not running

Can the IDG be reconnected in flight if it hasbeen disconnected

No the ground crew must reconnect it afterlanding

Describe the function of the BUS TIE in auto It will open or close ties to connect AC busses toavailable generators using a priority system(engines -gt APU -gt external)

If GEN 1 fails to supply AC BUS 1 what happens The bus ties close to connect an availablegenerator to AC BUS 1

How is the AC ESS bus normally powered AC BUS 1

If AC BUS 1 fails how is the AC ESS buspowered

AC BUS 2 will supply AC ESS

What indication will you get to show that AC BUS2 is feeding AC ESS

The ALTN light on the AC ESS FEED switch willilluminate if selected on

What does the GALY amp CAB FAULT light indicateon the electrical panel

A generator is operating at more than 100

Explain the auto function of the GALY amp CABpushbutton

The main galley in-seat power and IFE is shedduring single generator operations However itis powered with APU GEN or EXT PWR on theground

How is the DC BAT bus normally powered DC BUS 1

How does the emergency generator connect tothe electrical system

The RAT powers the blue hydraulic system whichdrives the emergency generator by means of ahydraulic motor The generator feeds AC ESSbus The ESS TR then powers DC ESS bus



What does the BAT FAULT light indicate The charging current is too excessive and thebattery contactor opens

Pack flow is selected to NORM Only the APU isproviding bleed air or one pack is selected offWhat is the pack flow rate

High (120 flow)

If the HOT AIR valve faults what will happen tothe temperature control system

You lose zone control All zones receive directpack air at the same temperature

Explain the XBLEED function in its differentpositions

In AUTO the xbleed valve opens if the APUbleed is on or during engine start With theengines running the xbleed valve closes toisolate the two sides OPENCLOSE = obvious

How are the air conditioning packs controlledand operated

Selecting the pack switch on opens the packcontrol valve which takes bleed air to the packThis air is cooled by ram air directed into theACM and the water is removed The conditionedair is sent to the mixing chamber fordistribution

What are some potential causes for the airconditioning pack FAULT light

The pack flow valve is not in the commandedposition or compressorpack outlet overheat

What are some potential causes for an enginebleed FAULT light

There is a bleed leak overpressure overheat orthe valve is open during engine start or with theAPU bleed on

What does the APU bleed FAULT illuminationindicate

APU bleed leak

What does selecting the RAM AIR pushbuttonaccomplish

An emergency ram air inlet ventilates thecabincockpit to remove smoke or in the caseboth packs fail The outflow valve will generallyopen 50

What is accomplished if the wing anti-ice buttonis selected on the ground

A 30 second test is carried out

What does the wing FAULT light indicate The wing anti-ice valve is not in the commandedposition or there is low bleed pressure

What does the ENG 1(2) FAULT light on the anti-ice panel indicate

An engine anti-ice valve is not in thecommanded position

If electrical power fails what position do thewing and engine anti-ice valves default to

The wing valve fails in the closed position Theengine valves fail to open



Describe the probe and window heat logic The window and probe heating is on with atleast one engine running The probes are all onlow while on the ground (except TAT which isnot heated on the ground)

What does selecting the MODE SEL from AUTOto MAN to AUTO achieve

It swaps the cabin pressure controllers

How is the landing field elevation entered intothe system in normal and abnormal modes

In auto the field elevation is set by the FMGC Insemi-automatic the crew dials the landingelevation using the rotary dial In manual thecrew uses the toggle switches to select cabinVS

What does pushing the DITCHING buttonaccomplish

Closes all valves and opening below the waterline (assuming the outflow valve is in automode)

What does the APU master switch FAULT lightindicate

The APU has automatically shutdown

What does the APU AVAIL light indicate The APU speed is above 95 (after 2 secs) and isavailable for electrical supply Bleed air is alsoavailable

What condition in the APU system would causean external horn to sound

An APU fire is detected

In the emergency electrical configuration willthe APU start immediately

No If you attempt an APU start it is inhibited for45 seconds to prevent interference withgenerator coupling

What does the illumination of the cargo hot airFAULT mean

A duct overheat has been detected

What does the illumination of an AFT ISOLVALVE FAULT light mean

The valve is not in the commanded position

Describe the cargo smoke test Press the test button for 3 seconds to illuminateSQUIBDISCH lights Look for the masterwarnings lights SMOKE light ECAM warning andlisten for the CRC

Following a cargo smoke indication anddischarge of the cargo bottle what would be theexpected indication on the cargo smoke panel

The DISCH light will be on (low bottle pressure)and then possibly a SMOKE light due to gasestrapped in the cargo compartment

How many fire extinguishing bottles are in thecargo system

One



What are some potential causes for theillumination of an avionics blower FAULT light

Low blower pressure computer power failuresmoke warning or duct overheat

What are some potential causes for theillumination of an avionics extract FAULT light

Low extract pressure computer power failure orsmoke warning

Describe the avionics ventilation system Avionics air is directed around the skin to cool inflight This is the same on the ground if the skintemp is lt12c If gt12c the inlet and outlet opento push cooling air through If an overheat orblower fan fault occurs the air condition valveopens to add cooling air If smoke is alsodetected a small flap opens to extract thesmoke

What condition would cause an external horn tosound regarding the avionics cooling system

If on the ground with the engines stopped a lowblowerextract pressure or a duct overheat isdetected

What are some of the causes for autoland redlight

If below 200ft RA both autopilots fail or there isa loss of the LOCGS signal or an excessive ILSdeviation occurs or the RA1amp2 difference isgt15ft

What action should the pilot take if the redautoland light illuminates below 200 RA

Immediate go-around

What should be selected on the glareshield EFIScontrol panel during the cockpit preparation

ARC or ROSE NAV (if the heading after takeoff isgt70 degrees) and RANGE as required (40NM forTCASWX radar)

if a HDG is pre-selected (not pulled) prior totakeoff what lateral mode will be active afterliftoff

RWY TRACK

If a managed lateral dot is displayed next to theFCU HDG window prior to takeoff what lateralmode will be active after liftoff

NAV

What are some ways to disconnect theautopilot

Push the takeover PB or glareshield PB oroverpower the controls

Describe the preflight actions performed usingthe ECAM control panel

Recall all warnings check O2 pressure on theDOOR page check HYD quantity check OILquantity STS check and PRESS page to showAUTO landing elevation

Should the ECAM control panel fail whichfunctions are still available

CLR STS RCL ALL and EMER CNCL



What does pressing the EMER CANC accomplishfor both warnings and cautions

Warnings it cancels the aural and master lightsbut the ECAM message still shows Cautions itcancels the caution for the rest of the flight andthe status page shows CANCELLED CAUTION(push RCL for 3 seconds to review)

What is the purpose of having the EMER CANCbutton

To cancel nuisance aural warnings

If an RMP 1 failure occurs how can you use VHF1

Use RMP 2

How is autothrust normally armed Move the thrust levers beyond CL on takeoff

What would be the normal FMA indicationsduring takeoff with FLX thrust and a runway witha LOC

MAN FLX SRS RWY autothrust blue

What would be the FMA indications duringtakeoff with TOGA selected

MAN TOGA SRS autothrust blue

How should autothrust be turned off Match the donuts in the N1 indicator and pushthe disconnect buttons on the thrust levers

What should the pilot do to get out of TOGAlock

(After an Alpha Floor event) Press the disconnectbutton put the levers to CL and press theglareshield ATHR on button

What should the pilot do to get out of thrustlock

(After disconnecting autothrust using theglareshield ATHR button) Move the thrustlevers out of climb and then re-engage

How can a pilot turn off autothrust for theremainder of a flight

Press the disconnect buttons for more than 15seconds

If the pilot has disconnected the autothrust isalpha floor protection available

No

What are the autothrust active zones for 2engine operations

Idle to CL


Idle to MCT

What is Virgin Americas SOP for reverse thrustuse

Use as required down to 70 kts then idlereverse only Do not use in flight or topowerback

When selecting the flap lever to 1 after the flapshave been at CONF 2 or higher what flap setting

Flaps 1+F



will the flapslats go to

What is the normal flap setting for the go-around

Retract the flaps one step

Maximum demonstrated crosswind for takeoffand landing

38 knots (including gusts)

Maximum tailwind for takeoff and landing 10 knots

Maximum wind for passenger door operations 65 knots

Maximum wind for cargo door operations 40 knots (must be closed before 65 knots)

VLE 280 knots or M 067

VLO Extension 250 knots

VLO Retraction 220 knots

Maximum gear extend altitude 25000 feet

Maximum tire speed 195 knots (groundspeed)

Maximum brake temperature for takeoff 300 degrees C

With brakes set N1 limit is 75 N1

Maximum windshield wiper speed 230 knots

Maximum speed with flight deck window open 200 knots

Do not use LP ground airhellip With the packs operating (to avoid valve chatter)

Do not use HP ground airhellip With the APU bleed selected on (to avoiddamage)

Minimum height for AP use after takeoff (SRSmode)

100 feet AGL (internal logic prevents use until 5secs after liftoff)

Minimum height for AP use for non-precisionapproach

MDA

Minimum height for AP use for circlingapproach

MDA less 100 feet

Minimum height for AP use with CAT1displayed

160 feet AGL



Minimum height for AP use for go-around 100 feet AGL

Minimum height for AP in all other phases offlight

500 feet AGL

With one engine inoperative do not use thesemodes

FINAL APP NAV VS NAV FPA

Autothrust is approved for usehellip With or without the APFD in selected andmanaged modes

Maximum altitude with the flapsslats extended FL200

Maximum outer fuel tank imbalance 1521 lbs

Maximum inner fuel tank imbalance 3306 lbs

True or false Center tank can be used fortakeoff

False (the center tank must not be used fortakeoff)

When must you not use the ISIS bugs function After both PFDs are lost

Maximum APU altitude for dual packoperations

15000 feet

Maximum APU altitude for engine start usingbleed air

20000 feet

Maximum APU altitude for single packoperations

22500 feet

After 3 APU starter cycles how long must youwait before trying again

60 minutes

True or false APU bleed air can be used for winganti-icing

False (APU bleed air must not be used for winganti-ice)

Minimum oil temperature for starting -40 degrees C

Minimum oil temperature for takeoff -10 degrees C

Minimum oil quantity for departure 95 quarts + 05 quarts for each planned flighthour

Maximum engine starter cycles 4 cycles

Minimum engine starter cooling after 4attempts

15 minutes



Maximum duration of an engine starter cycle 2 minutes

Minimum pause between engine start attempts 20 seconds

Maximum N2 for re-engagement of the starter 20 N2

Do not use maximum reverse thrust below 70 knots IAS

True or false Reverse thrust cannot be used inflight

True (reverse thrust cannot be used in flight)

True or false Reverse thrust can be used to backup an airplane

False (do not back up an airplane with reversethrust)

EMERGENCY DESCENT Crew 02 Mask ON Signs ON ALT Turn amp PullHDG Turn amp Pull SPDMACH Adjust (ThrustLever if ATHR off IDLE) Speedbrake FULL

LOSS OF BRAKING If autobrake on - Brake Pedals PUSH If nobraking - Thrust Reverse MAX Brake PedalsRELEASE ASkid amp NWS OFF Brake PedalsPRESS (Max 1000psi) If still no braking - ParkingBrake USE

UNRELIABLE SPEED INDICATION APFD Off ATHR Off PITCHTHRUST BelowThrust Reduction Altitude 15degTOGAAbove ThrRed Alt and below 10000 ft 10degCLBAbv 10000ft 5degCLBFLAPS If 0123 MAINTAIN CURRENTCONFIGIf FLAPS FULL Select and MaintainCONFIG 3Check Spdbrks retractedLdg GearUPAt or Above MSA or Circuit Alt Level Off fortroubleshooting

1 4803 ~

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Why is it important to observe the ON BAT lightduring IR initialization

To ensure that a good test has been completedA good test will confirm that at least one IR canbe powered by the aircraft batteries in the eventof power loss

Does the ON BAT light illuminate during a fastalign

No

What could cause the flashing white ALIGN lightto illuminate on the ground

No PPOS entered after 10 minutes 1 degree ofdifference in the last known LATLONG or theaircraft was moved during the initial alignment(Not in Rev 1A)

What are some external indications that theADIRS have reverted to battery power on theground

The ADIRU amp AVNCS light will illuminate on theexternal power panel and an external horn willsound

What does a steady FAULT light on the IRindicate

The IR has failed

What does a flashing FAULT light on the IRindicate

The IR has failed but heading and attitude maystill be recovered (turn the selector to ATT)

Can the ADR be turned off without losing the IRfunctions

Yes Select the ADR switch to OFF

Can an IR be turned off without losing the ADRfunctions

No Turning off the IR will also turn off the ADR

What would a flight control consequence be ifyou lost two IRs

You would be in Alternate Law with someprotections lost Also the autopilot andautothrust may be unavailable

What kind of flight control system does theAirbus A320 have

Fly by wire

How are the flight controls controlled andactivated

The flight surfaces are electrically commandedand hydraulically actuated

How is NORMAL LAW indicated on the PFD You will see green equals marks at 67 degrees ofbank 30 degrees pitch up 15 degrees pitchdown and on the speed tape at VMO + 6kts

How is ALTERNATE LAW indicated on the PFD The normal green equals marks will be replacedwith amber xs at pitch and bank limits Atraditional barber pole shows on the speed tape

How is DIRECT LAW indicated on the PFD USE MANUAL PITCH TRIM

How is MECHANICAL BACKUP indicated on the MAN PITCH TRIM ONLY shows in red on the PFD
















































RMP 1 only





































No


















A pump overheat

















Low pump pressure



















Yes

























High (120 flow)












APU bleed leak


































One













Immediate go-around




RWY TRACK


NAV














Use RMP 2














No


Idle to CL


Idle to MCT




Flaps 1+F

























MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














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RMP 1 only





































No


















A pump overheat

















Low pump pressure



















Yes

























High (120 flow)












APU bleed leak


































One













Immediate go-around




RWY TRACK


NAV














Use RMP 2














No


Idle to CL


Idle to MCT




Flaps 1+F

























MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














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SOCL 358

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5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


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Summer 2011


4 pages






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Fall 2009


14 pages


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Spring 2015


14 pages


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RMP 1 only





































No


















A pump overheat

















Low pump pressure



















Yes

























High (120 flow)












APU bleed leak


































One













Immediate go-around




RWY TRACK


NAV














Use RMP 2














No


Idle to CL


Idle to MCT




Flaps 1+F

























MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














1 4803 ~


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Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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No


















A pump overheat

















Low pump pressure



















Yes

























High (120 flow)












APU bleed leak


































One













Immediate go-around




RWY TRACK


NAV














Use RMP 2














No


Idle to CL


Idle to MCT




Flaps 1+F

























MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














1 4803 ~


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Winter 2015

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SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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No


















A pump overheat

















Low pump pressure



















Yes

























High (120 flow)












APU bleed leak


































One













Immediate go-around




RWY TRACK


NAV














Use RMP 2














No


Idle to CL


Idle to MCT




Flaps 1+F

























MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














1 4803 ~


Follow




NO OF TERMS

212

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HIN 2

Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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Terms of Use














Low pump pressure



















Yes

























High (120 flow)












APU bleed leak


































One













Immediate go-around




RWY TRACK


NAV














Use RMP 2














No


Idle to CL


Idle to MCT




Flaps 1+F

























MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














1 4803 ~


Follow




NO OF TERMS

212

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March 15th 2013

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HIN 2

Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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Yes

























High (120 flow)












APU bleed leak


































One













Immediate go-around




RWY TRACK


NAV














Use RMP 2














No


Idle to CL


Idle to MCT




Flaps 1+F

























MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














1 4803 ~


Follow




NO OF TERMS

212

UPLOAD DATE

March 15th 2013

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Related Documents

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HIN 2

Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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Terms of Use







High (120 flow)












APU bleed leak


































One













Immediate go-around




RWY TRACK


NAV














Use RMP 2














No


Idle to CL


Idle to MCT




Flaps 1+F

























MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














1 4803 ~


Follow




NO OF TERMS

212

UPLOAD DATE

March 15th 2013

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Related Documents

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HIN 2

Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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Terms of Use



























One













Immediate go-around




RWY TRACK


NAV














Use RMP 2














No


Idle to CL


Idle to MCT




Flaps 1+F

























MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














1 4803 ~


Follow




NO OF TERMS

212

UPLOAD DATE

March 15th 2013

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HIN 2

Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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Terms of Use















Immediate go-around




RWY TRACK


NAV














Use RMP 2














No


Idle to CL


Idle to MCT




Flaps 1+F

























MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














1 4803 ~


Follow




NO OF TERMS

212

UPLOAD DATE

March 15th 2013

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Related Documents

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HIN 2

Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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Use RMP 2














No


Idle to CL


Idle to MCT




Flaps 1+F

























MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














1 4803 ~


Follow




NO OF TERMS

212

UPLOAD DATE

March 15th 2013

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Related Documents

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HIN 2

Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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MDA


MDA less 100 feet


160 feet AGL





500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














1 4803 ~


Follow




NO OF TERMS

212

UPLOAD DATE

March 15th 2013

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Related Documents

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HIN 2

Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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500 feet AGL











15000 feet


20000 feet


22500 feet


60 minutes








15 minutes














1 4803 ~


Follow




NO OF TERMS

212

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Related Documents

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HIN 2

Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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1 4803 ~


Follow




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HIN 2

Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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NO OF TERMS

212

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HIN 2

Winter 2015

1 pages


SOCL 358

Spring 2013

5 pages


FRENCH AP Lang

Fall 2010

2 pages







FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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FR 111

Fall 2013


4 pages


BY 411

Fall 2009


11 pages


JPNS 1010

Fall 2014


2 pages


ABNORMALIT 920

Fall 2013


5 pages

Oral MechanismUCM

CD 1401

Fall 2014


2 pages


BIOL 2560

Summer 2011


4 pages






BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


ASTR 330

Spring 2010


6 pages



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BY 411

Fall 2009


14 pages


GES 405

Spring 2015


14 pages


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Spring 2010


6 pages



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