repaso

the supply functions in the full face quick donning (crew) masks are;. Normal, and 100% with overpressure. normal and emergency. normal and 100% and emergency.

the ecam message “low fuel pressure” means: Low fuel pressure delivered by the FCU. Low fuel press detected by the APU fuel pump. low fuel press at the FCU inlet.

the operation of the bulkl cargo door is: only manually. hydraulically. electro hydraulically.

APU:when is the drain tank drained: When the aircraft speed is above 200KTS. when the aircraft altitude is above 2000 feet. when aircraft is in approach for landing.

the air compressor of the wáter tank: it will run the pressure in the tank is lower than 22 psi. it will have priority over the pneumatic system. it is used only on ground operations.

the ambar door name on the lower ECAM display means: the door is unlocked. the cabin diff press is more than an specific value. the door is close and the slide is in flight.

-.what about the door system is right: the damper actuator also open the door in emergency operation. the fwd entry door can be open either manual or electrically. the outer lever follows the inner control lever movement.

APS3200 :an APU LOP auto-shutdown will occur when. when RPM are above 95%,and the oil pressure is lower than 35 PSI. the LOP SW has failed and APU speed is below 7%. when APU RPM are lower than 95% and oil temp is 135C.

.the crew oxygen system has two overpressure safety outlets at: oxygen cylinder valve and pressure regulator. pressire regulator and low press manifold. low press manifols and fill port.

.where is the STA. “0” located: 2540mm forward the radome. 100mm forward the radome. on the first frame.

.the purpose of the de-oiling valve solenoid is: reduces the pressure pump load durind starting. it vents the oil sump (gearbox) to the exhaust. it separetes de air from the oil.

what should happen if the door emergency control handle is in disarmed and somebody try to open the door from outside : the door will open normally. the door emergency control handle will be moved to the armed position. the slide will deploy.

regarding the Passenger oxygen system: the masks deploy automatically if the cabin altitude is higher than 14000 feet. the mask deploy automatically only. the mask will deploy automatically whe the cabin altitude is higher than 8000 feet.

APS 3200 the ignition system consists of: 1 ignition unit and 2 ignitor plugs. 2 ignition unit and 1 ignitor plugs. 1 ignition unit and 1 ignitor plugs.

what should be do if some emergency oxy panel on PSIU do not open after oxy sys activation: unlatch de door with the manual release tool. pull down the cover from the test door stop. press the oxygen reset switch on the overheat panel.

.to accomplish a potable water system service: it can be done with electrical power available or not. it is necessary to have electrical power available,ground service at least. it must be done without electrical power.

with the airplane on ground and service toillet panel open.What happen: the toillets system is inoperative and in the FAP appears the waste quantily. is possible one operation more only. the toillets system works normally.

to open the cargo door is necessary: to pressurize the yellow hyd system. to watch if the green light on control panel is ON when the hyd press is available. to prezurize the blue hyd sys in maintenace overhead panel at the cockpit.

.where are the overwing slide cylinders located: behind the sidewall panels of the aft cargo compartment. behind the sidewall panels of the forward cargo compartment. behind the belly fairing.

the waste water system drain to: the overboard through the drain masts. the air condition Ram air system. one wasted tank on the aft cargo compartment.

.the green lights installed on the potable water system panel: they are ON when any Drain/Overflow valve is open or the water tank is full. they are On when the Water Tank is full and the valves are in the Closed position. they are On when the Control Handle is on Neutral position.

the pilot seat movement is controlled. electrically and or manually. only manually. manually and hydraulically.

in wich modes can the ELT be activated: automatically by the G switch and manually placing the switch in the ON position. the ELT is always in active mode transmiting signal to satellites. only manually from the overhead panel,during the first 5 minutes for the hour auto activation is not posible.

.APS 3200:the APU bleed control valve is operated by. pneumatic pressure. fuel pressure from the FCU. electrical signal.

.CLASSIC :The drain mast heating control unit can be tested from: the PTP and by the test button on it panel. the MCDU. the ECAM test page.

when the slide in the Passenger door is armed,the girt bar is: fix to the cabin floor. fic in the door. the position is the same for armed or disarmed.

the purpose of the inlet guide vane actuator (IGVA) is: regulate the load compressor inlet air Flow by positioning the IGV’s. allow the operation of IGV´s by air pressure. send signals to the ECB for the open/close cycle of the surge valve.

.About A320: which of this statements concern to the emergency exit hatches is true: pulling down the cover flap will turn ON the slide armed light between the hatches. removal of the cover flap in the hatches will deploy the overwing slide. there are one overwing emergency door each side of the fuselage.

.without power on the aircraft how can you see the oxy pressure: On the forward attendant panel PTP. On the bottle indicator. there´s no way to see the oxy press.

.regarding the vaccum generator: it Works either in flight or on ground,depending on the aircraft altitude. it is used to presurize the waste holding tank. it works only when the aircraft is on ground condition.

the signal for the automatic deploy of the Passenger oxygen masks comes from: a dedicated altitude pressure switch located in the avionic compartment. the air data sensors. any of the ADIRUs.

.with the “LOW OIL LEVEL” msg on ECAM display APU page,the APU: Althought a corrective action is required, the APU still can run by another 60 hours in this condition. a manual stop procedure must be followed to avoid an overtemperature. will have a protective shutdown to avoid an overtemperature condition.

.which of these definitions about structure is correct: The ailerons,elevator and rudder are made of composite material. the radome is built with aluminiun alloy. the leading edge devices are made of aramid reinforced plastic.

.CLASSIC:the unit that is connected to the CFDS system,and gives faults information of the toilet system is: the vaccum system controlled. the vaccum generator. the flush control unit.

.which component controls and monitors the APU. the electronic control box (ECB). the inlet guide vane controlactuator (IGV). the fuel control unit (FCU).

the water heater in the potable water supply is: electrically powered. the water is warmed by action of the oil/water heat exchanger. pneumatically heated by bleed air.

APS 3200 what will happens if one thermocouple fails: nothing,the APU keeps running (or stays available). the EGT is lost. the APU goes to shut down.

which of these zones are not pressurized. the rear fuselage after of frame 70. only the bulk cargo compartment. the forward cargo compartment.

the APU fuel boost pump supplies fuel,when: the tank fuel boost pums are notoperating and the fuel pressure is LOW. every time the APU is in the startcycle. the tank fuel boost pumps areoperating and the fuel pressure is high.

releasing the master SW to OFF,with the APU bleed valve open: the APU will shutdown,after a cooldown period. the APU will shutdown inmediately. the APU will shutdown,only if the start P/B sw is released.