cpc1

bleed solo de engine 1. x bleed selector auto. x bleed valve open auto. x bleed no open auto. Xbleed valve only operate automatically if apu bleed ON.

if bmc1 fail. prv1 no control auto. prv 1 y 2 auto.

fav is control by. seledoid thermostat. Bmc.

hpv opv prv. position swich. rotari position swich.

hpv control by v2500. eec. bmc.

Overheat bleed LH wing recibe information from: bmc1 loop A bmc 2 loop B. bmc1 loop A and loop B.

320 has: 2 BMC´S. 1 BMC.

which BMC control APU overheat?. bmc 1. bmc 2.

if bmc 1 fail.... bmc 2 can control all oposite side. bmc 2 only can monitor oposite side.

zone control ZC total failure. trim air pressure regulator valve close. trim air pressure regulator valve open.

pack controller has 2 lines. If pack controller line 1 fail. pack flow reain al the previous setting before the failure. go to high flow.

bypass valve. selenoid air motor. electrical motor.

classic. If compresor overheat (air clicle machine), what happend with flow control valve?. PC close valve. Flow control valve close automatically pneumatically.

how many motors have out flow valve?. 3 motors, 2 auto, 1 manually. 2 motors, 1 auto, 1 manually.

how many electronic actuator have in outflow valve?. 2. 1.

enhance. wich acsc comunicate with CFDS?. ACSC 1. ACSC 2.

How many zone controller we have?. 1, 2 channels. 2.

enhance. ACSC overheat fwd cabin.... pressure regulating valve and trim valve close. trim air valve open and pressure regulating valve close.

enhance. Which ACSC control cockpit temperature?. ACSC 1. ACSC 1 and 2.

enhance. Which ACSC control FWD and AFT cabin temperature?. ACSC 1. ACSC 2.

cooling air fan in Air clicle macnine: turbine move compressor and fan. compresor move fan.

funcion of emergency ram inlet: supply air if loose 2 packs and ventilate the cabin and cockpit. supply air if loose 1 pack.

ditching. outflow flow valve 1 and 2 close, avionic vent close, pack valve close, ram air inlet valve (if open) close. nothing happends.

which CPC normally controll pressurization?. swapp every flight. CPC 1.

push boton Cabin Pressurization fault light: if we loose boht computer. if we loose CPC1.

Water tank 320 in... FWD cargo. ATT cargo.

classic. toilet failure. Which computer control?. vaccum system controller. Cids.

enhance. toilet failure. Which computer control?. cids. Vaccum system controller.

waste tank 320 in.... aft cargo. fwd cargo.

vaccum generator recibe signal from. vaccum system controller. from cids.

classic. vacum system controller recibe signal from. altitud pressure swich. magic.

enhance. from wher cids recibe signal. from CPC througt SDAC. from magic.

wich computer control GLC?. GCU. IDG.

enhance. Which control APU generator?. GAPCU. GCU 1.

If GLC fail: gen P/B fault light come on. IDG P/B fault light come on.

emergency generatior is connected to: blue hyd from rat. green hyd from rat.

how many TR?. 3. 2.

ess TR get power from. EMER GEN or AC ESS BUS. AC ESS BUS or DC ESS BUS.

AC ESS BUS get power from. AC BUS 1. AC ESS BUS.

one FWC fail. no warnings are lost. we lost half warnings.

if we loose both sdacs. amber caution loose. no warnings loose.

if we loose one DMC. swich manually DMC3. swich automatically DMC3.

can primary fail affect other system?. yes. no.

DMC1 control. ND and PFD captain. SD and EWD.

if IDG oil outlet has overheat (avobe 200º). automatically disconect. manually disconect.

when appeare ADV indication. in ecam mono/single display. both screens opperative.

TR2 get power from. AC BUS 2. AC ESS BUS.

aural warning is generate from: SDAC. FWC.

FDR or SSDR get power from: AC ESS BUS. from interlock cirucuits.

linear acceleromenter send signal to FDIU. through SDAC. Directly.

IDG oil low pressure(140psi). IDG fault P/B light come on. GEN fault P/B light come on.

321 has. 8 frame on FWD section more than 320. 6 frame on FWD section more than 320.

panel 131 BR. lower fuselage right side. upper fuselage left side.

how many jacking points?. 3 jacking points. 4 jacking points.

which component block the movement of the outer handle??. handle gear box. lifting mechanism.

how many ways we do quick leveling?. alpha call up and attitud indicator. from FMGC1.

what is the material of windsheal sking?. tittanium. alluminium.

wich load is carried in FWD pylon to wing attachment?. vertical load. side load.

if you repacle DCM. software crossload from another DMC. software upload from DDU.

wher is the slide cylinder emergency exits?. In AFT cargo. In bulk cargo.

from where is replace sliding windows. from inside. from outside.

when move arm level to arm, gift bar stay. on the door. on the cabin.

function of dumper door. open door and dump door. open door.

indication of cargo doors in SD signal is from: LGCIU. SDAC.

indication of passanger doors in SD signal is from: SDAC. LGCIU.

when oxy mask deploid: after 30 sec selenoid cut of energy. nothing happend.

passanger oxy system use: chemical generator. chemical generator or cylinder.

pilot seat can be control. manually. manually or electrically.

ths fittins visual inspections: cracks and delamination. moisture and delamination.

PTU start automatic if. differencial pressure of 500psi between green and yellow. differencial pressure of 500psi between green and blue.

hydraulic shutoff valve activate from. fire P/B. engine master swicht.

pressure transducer green hyd fail. no indication. channel B indication.

2 condition RAT auto deploid. AC BUS1 AND AC BUS2 fault and more 100 knt. AC ESS BUS fault and more than 100 knt.

low air pressure hyd pump when.... 50 psi. 22 psi.

engines off. engine fuel low pressure valve is... open. close.

ground. slats extend. 1 minut after engine start.... center boost pump will stop. center boost pump will run.

how many fqic have (el de combustiblwe). 1 fqic, 2 channels. 2 fqic.

when you go to refuel panel and move refuel valve to open: selenoid energice and valve stay close. valve open.

during refuel if tank is in full level...the refuel valve... close. open.

how many boost pumps have a321 in center tank?. 0. 2.

T more than 85º in IGGS, ICU.... energice isolation valve selenoid and valve close. energice isolation valve selenoid and valve open.

how many FLSCU we have?. 2. 1.

purpuse of sequence valve. decrease presure from wing boost pump 5 psi than center. decrease presure from center boost pump 5 psi than wing.

elevator control by. ELAC 2. ELAC 1.

servo actuator if one acuator fail (both selenoid de-energice), ELEVATOR servoactuator in. damping mode. centering mode.

servo actuator if both acuator fail (all selenoid de-energice), ELEVATOR servoactuator in. centering mode. damping mode.

if we loose 1 hyd system in THS. half speed. medio recorido.

if 1 control valve in THS is jamp, THS. inmovilize. half speed.

if we loose 1 of 2 pcu hyd motor...slats. normal speed. half speed.

if we loose yellow hyd system. flap half speed. slats half speed.

if flap its disconection between outboard and inboard... wtb its applied. pob its applied.

which computer control alerons?. ELAC 1. ELAC 2.

trim THS move on ground manually: via trim wheel. via side stick.

spoilles get hydraulic from: 1 source. 2 source.

who can reset WTB?. on ground via CFDS. on ground via ELAC.

how many SFCC we have?. 2. 3.

flap disconection sensor send signal to. LGCIU. SFCC 1.

If we loose both ELACS, who control THS. SEC. SFCC.

if we loose green hyd how can roll?. ailerons and spoilers 2,3,4. half ailerons and spoiles 2,3,4.

rudder servocontrol have 2 servoconrol. if they are deenergize go to mode: by-pass. dumping.

wich speed close auto shutoff funcion of safety valve?. above 260knt. above 230knt.

close landing gear doors with. green. blue.

extension retraction main landing system, can we use yellow?. no. yes.

how can i prevend landing gear retraction on ground?. with control handle interlock selenoid. with safety pins.

before landing gear retracted LGCIU need to know. lg is extending before retraction. lg is contract before retraction.

to control LG ext o ret level handle send electrical signal to. LGCIU and then to selector valve. to selector valve directly.

enhance. Extension of LG in gravity. We have steering?. yes. no.

parking brake on. If pressure of brake pedal, and Pressure of the pedal is higer than parking brake.... extra brake. no more extra brake.

wich is the component that give priority to normal brake?. priority valve. BSCU.

how many BSCU we have?. 1 BSCU , 2 channels. 2 BSCU.

parking brake from. yellow. green.

engine anti ice P/B signal go: directly to the valve. via EEC.

engine fire detectors integrity need to be. open for fault. close for work.

how mani FDU we have. 3. 2.

for squib first. need to arm. push buttom.

when emerg will go on?. if we loose ess bus. if we loose ac bus 1 and ac bus 2.

we have signal of fire if: both loops detect fire. one loop detect fire.

windsheal low power or high power signal from. LGCIU. SDAC.

FDU test via. CFDS. Through the box.

lavatory smoke detector via in classic. SDCU. FDU.

Avionic smoke detector via. SDCU. AEVC.

ADR 1 FAIL. set ADR CAP ON 3. automatically.

IR provide to FMGEC position with. IR position plus gps plus hybrid. only IR position.

if we loose RA1..-. EGPWS is loose. EGPWS get signal from RA2.

RA has. 4 antennas. 2 antennas.

if IR 1 fail... set ATT HDG sich cap on 3. automatically.

ILS provide 2 signals. LOC and GLOW SLOP. LOC.

ILS 1 provide signal to. GPWS. EEC.

TCAS XDER recibe signals from. ATC. ADIRUS.

ATC TCAS panel selector swich selector to above. Signal go: to the ATC and the TCAS. directly to TCAS.

VOR ADF ILS....normally is. autotune from FMGEC. manually tune.

normal condition DME autotune thought. each fmgec tune radio through rmp. each fmgec tune radio directly.

how many VOR we have. 2. 1.

A/THR is dissengage and we have high AOA....What happend with A/THR. A/THR engage automatic to TOGA. A/THR not engage and go to TOGA.

alpha floor is detected b. FWC. FAC.

Whingsheal signal from FAC with clean configuration. We have protection of whindshiiel from FAC?. no. yes.

EGPWS has priority. stall over terrain tcas. terrarin tcas over stall.

priority. EGPWS over TCAS. TCAS over EGPWS.

A/P no engage yaw damper signal from. ELAC or FAC. SEC and FAC.

FMGEC set A/THR target to FADEC. throug FCU. directly.

Side stick move during A/P. no. yes.

FMGEC modes. normal independent and single. normal and single.

normal mode, wich FMGEC provide indication on the FMA (fligh mode anunciator). FMGEC 1 both FMA. FMGEC 1 or FMGEC 2.