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Get Premier Features
Terms Definitions
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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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
What are the autothrust active zones for 1engine operations
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
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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
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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
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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
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1032015 ORAL QUESTIONS Flashcards shy Course Hero
httpswwwcourseherocomflashcards497121ORALshyQUESTIONS 219
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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
What are the autothrust active zones for 1engine operations
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
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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
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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
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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
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1032015 ORAL QUESTIONS Flashcards shy Course Hero
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
What are the autothrust active zones for 1engine operations
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
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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
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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
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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
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1032015 ORAL QUESTIONS Flashcards shy Course Hero
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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
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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
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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
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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
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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
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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
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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
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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
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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
What are the autothrust active zones for 1engine operations
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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
What are the autothrust active zones for 1engine operations
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
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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
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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
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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
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1032015 ORAL QUESTIONS Flashcards shy Course Hero
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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
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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
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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
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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
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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
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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
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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
What are the autothrust active zones for 1engine operations
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
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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
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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
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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
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Fall 2009
BY 411 Advanced HumanAnatomy BY 411 AdvancedHuman Anatomy Potential
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GES 405
Spring 2015
Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
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Spring 2010
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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
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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
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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
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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
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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
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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
What are the autothrust active zones for 1engine operations
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
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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
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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
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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
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NO OF TERMS
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UPLOAD DATE
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Assignment 1UC Davis
HIN 2
Winter 2015
1 pages
Oral QuestionsAzusa Pacific
SOCL 358
Spring 2013
5 pages
Moliere Oral QuestionsThomas S Wootton High
FRENCH AP Lang
Fall 2010
2 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
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कछ 耂न ी (use व) इन को कछनह ीचाहहए Oral questions1 ȅया तझ नय जतचा耂हय닼 2ककसको 耂य ककताब चा耂हय
SOC358HUMANDIVERSITYStudyGuideforOralExamPleaserememberyouwillbesubmittingyourstudyguidenotesimmediatelyfollo
Generated by CamScannerGenerated by CamScanner
Questions Examen OralFall 2013Ole Miss
FR 111
Fall 2013
FR 111 Questions exemplespour lexamen oral Preacuteparez(agrave loral) les questionssuivantes 1 Comment tu
4 pages
BY 411- Oral QuizQuestions for LowerExtremity final (2)UAB
BY 411
Fall 2009
BY 411 Advanced HumanAnatomy BY 411 AdvancedHuman Anatomy Potential
11 pages
Oral Final Exam_PracticesheetColorado
JPNS 1010
Fall 2014
Oral Final Exam Practicesheet Tested speakingability 1 Able to answersimple questions about
2 pages
An Oral History InterviewQuestionsRutgers
ABNORMALIT 920
Fall 2013
An Oral History InterviewQuestions so Im going toask you some questionsabout your Grandma To
5 pages
Oral MechanismUCM
CD 1401
Fall 2014
Aspiration Researchquestion As seen in the titleof the research article themain question to this is canan oral mechanism
2 pages
L11 STUDY QUESTIONSAuburn
BIOL 2560
Summer 2011
Lecture 18 Questions 1 Theoral mucosa produces _____(antimicrobial peptides) 2The tongue mixes
4 pages
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Potential Oral QuizQuestions forAbdominopelvic CavitySpring 2011UAB
BY 411
Fall 2009
BY 411611 AdvancedHuman Anatomy Potential
14 pages
16_March4_Fluvial6OralBuffalo State
GES 405
Spring 2015
Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
14 pages
discussion1University of Illinois Urbanhellip
ASTR 330
Spring 2010
Group up earlyhttpwwwpublicasueduatjlb Oral PresentationQuestions Thesequestions are rated 1-10 out
6 pages
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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
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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
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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
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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
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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
What are the autothrust active zones for 1engine operations
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
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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
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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
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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
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14 pages
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GES 405
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Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
14 pages
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ASTR 330
Spring 2010
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1032015 ORAL QUESTIONS Flashcards shy Course Hero
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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
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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
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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
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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
What are the autothrust active zones for 1engine operations
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
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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
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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
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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
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NO OF TERMS
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UPLOAD DATE
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Assignment 1UC Davis
HIN 2
Winter 2015
1 pages
Oral QuestionsAzusa Pacific
SOCL 358
Spring 2013
5 pages
Moliere Oral QuestionsThomas S Wootton High
FRENCH AP Lang
Fall 2010
2 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
httpswwwcourseherocomflashcards497121ORALshyQUESTIONS 1719
कछ 耂न ी (use व) इन को कछनह ीचाहहए Oral questions1 ȅया तझ नय जतचा耂हय닼 2ककसको 耂य ककताब चा耂हय
SOC358HUMANDIVERSITYStudyGuideforOralExamPleaserememberyouwillbesubmittingyourstudyguidenotesimmediatelyfollo
Generated by CamScannerGenerated by CamScanner
Questions Examen OralFall 2013Ole Miss
FR 111
Fall 2013
FR 111 Questions exemplespour lexamen oral Preacuteparez(agrave loral) les questionssuivantes 1 Comment tu
4 pages
BY 411- Oral QuizQuestions for LowerExtremity final (2)UAB
BY 411
Fall 2009
BY 411 Advanced HumanAnatomy BY 411 AdvancedHuman Anatomy Potential
11 pages
Oral Final Exam_PracticesheetColorado
JPNS 1010
Fall 2014
Oral Final Exam Practicesheet Tested speakingability 1 Able to answersimple questions about
2 pages
An Oral History InterviewQuestionsRutgers
ABNORMALIT 920
Fall 2013
An Oral History InterviewQuestions so Im going toask you some questionsabout your Grandma To
5 pages
Oral MechanismUCM
CD 1401
Fall 2014
Aspiration Researchquestion As seen in the titleof the research article themain question to this is canan oral mechanism
2 pages
L11 STUDY QUESTIONSAuburn
BIOL 2560
Summer 2011
Lecture 18 Questions 1 Theoral mucosa produces _____(antimicrobial peptides) 2The tongue mixes
4 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
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Potential Oral QuizQuestions forAbdominopelvic CavitySpring 2011UAB
BY 411
Fall 2009
BY 411611 AdvancedHuman Anatomy Potential
14 pages
16_March4_Fluvial6OralBuffalo State
GES 405
Spring 2015
Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
14 pages
discussion1University of Illinois Urbanhellip
ASTR 330
Spring 2010
Group up earlyhttpwwwpublicasueduatjlb Oral PresentationQuestions Thesequestions are rated 1-10 out
6 pages
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1032015 ORAL QUESTIONS Flashcards shy Course Hero
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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
1032015 ORAL QUESTIONS Flashcards shy Course Hero
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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
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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
What are the autothrust active zones for 1engine operations
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
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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
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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
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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
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Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
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1032015 ORAL QUESTIONS Flashcards shy Course Hero
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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
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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
What are the autothrust active zones for 1engine operations
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
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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
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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
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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
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Assignment 1UC Davis
HIN 2
Winter 2015
1 pages
Oral QuestionsAzusa Pacific
SOCL 358
Spring 2013
5 pages
Moliere Oral QuestionsThomas S Wootton High
FRENCH AP Lang
Fall 2010
2 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
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कछ 耂न ी (use व) इन को कछनह ीचाहहए Oral questions1 ȅया तझ नय जतचा耂हय닼 2ककसको 耂य ककताब चा耂हय
SOC358HUMANDIVERSITYStudyGuideforOralExamPleaserememberyouwillbesubmittingyourstudyguidenotesimmediatelyfollo
Generated by CamScannerGenerated by CamScanner
Questions Examen OralFall 2013Ole Miss
FR 111
Fall 2013
FR 111 Questions exemplespour lexamen oral Preacuteparez(agrave loral) les questionssuivantes 1 Comment tu
4 pages
BY 411- Oral QuizQuestions for LowerExtremity final (2)UAB
BY 411
Fall 2009
BY 411 Advanced HumanAnatomy BY 411 AdvancedHuman Anatomy Potential
11 pages
Oral Final Exam_PracticesheetColorado
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Aspiration Researchquestion As seen in the titleof the research article themain question to this is canan oral mechanism
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BIOL 2560
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Lecture 18 Questions 1 Theoral mucosa produces _____(antimicrobial peptides) 2The tongue mixes
4 pages
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Potential Oral QuizQuestions forAbdominopelvic CavitySpring 2011UAB
BY 411
Fall 2009
BY 411611 AdvancedHuman Anatomy Potential
14 pages
16_March4_Fluvial6OralBuffalo State
GES 405
Spring 2015
Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
14 pages
discussion1University of Illinois Urbanhellip
ASTR 330
Spring 2010
Group up earlyhttpwwwpublicasueduatjlb Oral PresentationQuestions Thesequestions are rated 1-10 out
6 pages
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1032015 ORAL QUESTIONS Flashcards shy Course Hero
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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
What are the autothrust active zones for 1engine operations
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
1032015 ORAL QUESTIONS Flashcards shy Course Hero
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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
1032015 ORAL QUESTIONS Flashcards shy Course Hero
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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
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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
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NO OF TERMS
212
UPLOAD DATE
March 15th 2013
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Related Documents
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Related Flashcards
Assignment 1UC Davis
HIN 2
Winter 2015
1 pages
Oral QuestionsAzusa Pacific
SOCL 358
Spring 2013
5 pages
Moliere Oral QuestionsThomas S Wootton High
FRENCH AP Lang
Fall 2010
2 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
httpswwwcourseherocomflashcards497121ORALshyQUESTIONS 1719
कछ 耂न ी (use व) इन को कछनह ीचाहहए Oral questions1 ȅया तझ नय जतचा耂हय닼 2ककसको 耂य ककताब चा耂हय
SOC358HUMANDIVERSITYStudyGuideforOralExamPleaserememberyouwillbesubmittingyourstudyguidenotesimmediatelyfollo
Generated by CamScannerGenerated by CamScanner
Questions Examen OralFall 2013Ole Miss
FR 111
Fall 2013
FR 111 Questions exemplespour lexamen oral Preacuteparez(agrave loral) les questionssuivantes 1 Comment tu
4 pages
BY 411- Oral QuizQuestions for LowerExtremity final (2)UAB
BY 411
Fall 2009
BY 411 Advanced HumanAnatomy BY 411 AdvancedHuman Anatomy Potential
11 pages
Oral Final Exam_PracticesheetColorado
JPNS 1010
Fall 2014
Oral Final Exam Practicesheet Tested speakingability 1 Able to answersimple questions about
2 pages
An Oral History InterviewQuestionsRutgers
ABNORMALIT 920
Fall 2013
An Oral History InterviewQuestions so Im going toask you some questionsabout your Grandma To
5 pages
Oral MechanismUCM
CD 1401
Fall 2014
Aspiration Researchquestion As seen in the titleof the research article themain question to this is canan oral mechanism
2 pages
L11 STUDY QUESTIONSAuburn
BIOL 2560
Summer 2011
Lecture 18 Questions 1 Theoral mucosa produces _____(antimicrobial peptides) 2The tongue mixes
4 pages
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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
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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
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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
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Potential Oral QuizQuestions forAbdominopelvic CavitySpring 2011UAB
BY 411
Fall 2009
BY 411611 AdvancedHuman Anatomy Potential
14 pages
16_March4_Fluvial6OralBuffalo State
GES 405
Spring 2015
Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
14 pages
discussion1University of Illinois Urbanhellip
ASTR 330
Spring 2010
Group up earlyhttpwwwpublicasueduatjlb Oral PresentationQuestions Thesequestions are rated 1-10 out
6 pages
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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
1032015 ORAL QUESTIONS Flashcards shy Course Hero
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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
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Assignment 1UC Davis
HIN 2
Winter 2015
1 pages
Oral QuestionsAzusa Pacific
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Spring 2013
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Fall 2010
2 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
httpswwwcourseherocomflashcards497121ORALshyQUESTIONS 1719
कछ 耂न ी (use व) इन को कछनह ीचाहहए Oral questions1 ȅया तझ नय जतचा耂हय닼 2ककसको 耂य ककताब चा耂हय
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Fall 2013
FR 111 Questions exemplespour lexamen oral Preacuteparez(agrave loral) les questionssuivantes 1 Comment tu
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Summer 2011
Lecture 18 Questions 1 Theoral mucosa produces _____(antimicrobial peptides) 2The tongue mixes
4 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
httpswwwcourseherocomflashcards497121ORALshyQUESTIONS 1819
Cant find what you need
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Potential Oral QuizQuestions forAbdominopelvic CavitySpring 2011UAB
BY 411
Fall 2009
BY 411611 AdvancedHuman Anatomy Potential
14 pages
16_March4_Fluvial6OralBuffalo State
GES 405
Spring 2015
Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
14 pages
discussion1University of Illinois Urbanhellip
ASTR 330
Spring 2010
Group up earlyhttpwwwpublicasueduatjlb Oral PresentationQuestions Thesequestions are rated 1-10 out
6 pages
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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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1032015 ORAL QUESTIONS Flashcards shy Course Hero
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NO OF TERMS
212
UPLOAD DATE
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Assignment 1UC Davis
HIN 2
Winter 2015
1 pages
Oral QuestionsAzusa Pacific
SOCL 358
Spring 2013
5 pages
Moliere Oral QuestionsThomas S Wootton High
FRENCH AP Lang
Fall 2010
2 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
httpswwwcourseherocomflashcards497121ORALshyQUESTIONS 1719
कछ 耂न ी (use व) इन को कछनह ीचाहहए Oral questions1 ȅया तझ नय जतचा耂हय닼 2ककसको 耂य ककताब चा耂हय
SOC358HUMANDIVERSITYStudyGuideforOralExamPleaserememberyouwillbesubmittingyourstudyguidenotesimmediatelyfollo
Generated by CamScannerGenerated by CamScanner
Questions Examen OralFall 2013Ole Miss
FR 111
Fall 2013
FR 111 Questions exemplespour lexamen oral Preacuteparez(agrave loral) les questionssuivantes 1 Comment tu
4 pages
BY 411- Oral QuizQuestions for LowerExtremity final (2)UAB
BY 411
Fall 2009
BY 411 Advanced HumanAnatomy BY 411 AdvancedHuman Anatomy Potential
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BIOL 2560
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Lecture 18 Questions 1 Theoral mucosa produces _____(antimicrobial peptides) 2The tongue mixes
4 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
httpswwwcourseherocomflashcards497121ORALshyQUESTIONS 1819
Cant find what you need
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Potential Oral QuizQuestions forAbdominopelvic CavitySpring 2011UAB
BY 411
Fall 2009
BY 411611 AdvancedHuman Anatomy Potential
14 pages
16_March4_Fluvial6OralBuffalo State
GES 405
Spring 2015
Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
14 pages
discussion1University of Illinois Urbanhellip
ASTR 330
Spring 2010
Group up earlyhttpwwwpublicasueduatjlb Oral PresentationQuestions Thesequestions are rated 1-10 out
6 pages
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NO OF TERMS
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Assignment 1UC Davis
HIN 2
Winter 2015
1 pages
Oral QuestionsAzusa Pacific
SOCL 358
Spring 2013
5 pages
Moliere Oral QuestionsThomas S Wootton High
FRENCH AP Lang
Fall 2010
2 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
httpswwwcourseherocomflashcards497121ORALshyQUESTIONS 1719
कछ 耂न ी (use व) इन को कछनह ीचाहहए Oral questions1 ȅया तझ नय जतचा耂हय닼 2ककसको 耂य ककताब चा耂हय
SOC358HUMANDIVERSITYStudyGuideforOralExamPleaserememberyouwillbesubmittingyourstudyguidenotesimmediatelyfollo
Generated by CamScannerGenerated by CamScanner
Questions Examen OralFall 2013Ole Miss
FR 111
Fall 2013
FR 111 Questions exemplespour lexamen oral Preacuteparez(agrave loral) les questionssuivantes 1 Comment tu
4 pages
BY 411- Oral QuizQuestions for LowerExtremity final (2)UAB
BY 411
Fall 2009
BY 411 Advanced HumanAnatomy BY 411 AdvancedHuman Anatomy Potential
11 pages
Oral Final Exam_PracticesheetColorado
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Fall 2014
Oral Final Exam Practicesheet Tested speakingability 1 Able to answersimple questions about
2 pages
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Fall 2013
An Oral History InterviewQuestions so Im going toask you some questionsabout your Grandma To
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CD 1401
Fall 2014
Aspiration Researchquestion As seen in the titleof the research article themain question to this is canan oral mechanism
2 pages
L11 STUDY QUESTIONSAuburn
BIOL 2560
Summer 2011
Lecture 18 Questions 1 Theoral mucosa produces _____(antimicrobial peptides) 2The tongue mixes
4 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
httpswwwcourseherocomflashcards497121ORALshyQUESTIONS 1819
Cant find what you need
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Potential Oral QuizQuestions forAbdominopelvic CavitySpring 2011UAB
BY 411
Fall 2009
BY 411611 AdvancedHuman Anatomy Potential
14 pages
16_March4_Fluvial6OralBuffalo State
GES 405
Spring 2015
Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
14 pages
discussion1University of Illinois Urbanhellip
ASTR 330
Spring 2010
Group up earlyhttpwwwpublicasueduatjlb Oral PresentationQuestions Thesequestions are rated 1-10 out
6 pages
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कछ 耂न ी (use व) इन को कछनह ीचाहहए Oral questions1 ȅया तझ नय जतचा耂हय닼 2ककसको 耂य ककताब चा耂हय
SOC358HUMANDIVERSITYStudyGuideforOralExamPleaserememberyouwillbesubmittingyourstudyguidenotesimmediatelyfollo
Generated by CamScannerGenerated by CamScanner
Questions Examen OralFall 2013Ole Miss
FR 111
Fall 2013
FR 111 Questions exemplespour lexamen oral Preacuteparez(agrave loral) les questionssuivantes 1 Comment tu
4 pages
BY 411- Oral QuizQuestions for LowerExtremity final (2)UAB
BY 411
Fall 2009
BY 411 Advanced HumanAnatomy BY 411 AdvancedHuman Anatomy Potential
11 pages
Oral Final Exam_PracticesheetColorado
JPNS 1010
Fall 2014
Oral Final Exam Practicesheet Tested speakingability 1 Able to answersimple questions about
2 pages
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Fall 2013
An Oral History InterviewQuestions so Im going toask you some questionsabout your Grandma To
5 pages
Oral MechanismUCM
CD 1401
Fall 2014
Aspiration Researchquestion As seen in the titleof the research article themain question to this is canan oral mechanism
2 pages
L11 STUDY QUESTIONSAuburn
BIOL 2560
Summer 2011
Lecture 18 Questions 1 Theoral mucosa produces _____(antimicrobial peptides) 2The tongue mixes
4 pages
1032015 ORAL QUESTIONS Flashcards shy Course Hero
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Potential Oral QuizQuestions forAbdominopelvic CavitySpring 2011UAB
BY 411
Fall 2009
BY 411611 AdvancedHuman Anatomy Potential
14 pages
16_March4_Fluvial6OralBuffalo State
GES 405
Spring 2015
Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
14 pages
discussion1University of Illinois Urbanhellip
ASTR 330
Spring 2010
Group up earlyhttpwwwpublicasueduatjlb Oral PresentationQuestions Thesequestions are rated 1-10 out
6 pages
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Potential Oral QuizQuestions forAbdominopelvic CavitySpring 2011UAB
BY 411
Fall 2009
BY 411611 AdvancedHuman Anatomy Potential
14 pages
16_March4_Fluvial6OralBuffalo State
GES 405
Spring 2015
Today Oral Communicationassignment Go over anyquestions about Lab 3(Due on Friday) Briefstreams Start Karst Exam 1
14 pages
discussion1University of Illinois Urbanhellip
ASTR 330
Spring 2010
Group up earlyhttpwwwpublicasueduatjlb Oral PresentationQuestions Thesequestions are rated 1-10 out
6 pages
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