cabina

The supply functions in the Full Face Quick Donning (crew) masks are: Normal and Emergency. Normal, 100 % and Emergency. Normal and 100% with overpressure.

The operation of the Bulk Cargo door is?. Hydraulically. Only Manually. Electro hydraulically.

The air compressor of the water tank: It will run when 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 Fwd Entry Door can be open either manual or electrically. The Damper actuator also open the door in emergency operation. The Outer lever follows the inner control lever movement.

The Crew Oxygen System has two overpressure safety outlets located at... Pressure Regulator and Low Press. Manifold. Oxygen Cylinder Valve and Pressure Regulator. Low Press. Manifold and Fill Port.

Where is the STA. "0" located?. 100 mm. forward the radome. On the first frame. 2540 mm. forward the radome.

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

Regarding the passenger oxygen system: The masks deploy automatically if the cabin altitude is higher than 14000 feet. The masks deploy automatically only. The masks will deploy automatically when the cabin altitude is higher than 8000 feet.

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.

To open the cargo door is necessary... To watch if the green light on control panel is ON when the Hyd Press is available. To pressurize the yellow Hyd system. To presurize the Blue Hyd Sys. in maintenace overhead panel at the cockpitt.

The pilot seat movement is controlled... Only manually. Electrically and or manually. Manually and hydraulically.

In wich modes can the ELT be activated?. The ELT is always in active mode transmiting signal to satellites. Only manually from the overhead panel, during the first 5 minutes of the hour. Auto activation is not posible. Automatically by the G. switch and manually placing the switch in the ON position.

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?. The position is the same for armed or disarmed. Fix in the door. Fix to the cabin floor.

Without power on the Aircraft how can you see the Oxy pressure?. On the forward attendant panel PTP. There's no way to see the Oxy press. On the bottle indicator.

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

With the "LOW OIL LEVEL" Msg. on ECAM display, APU Page, the APU: A Manual Stop Procedure must be followed to avoid an overtemperature. Althought a corrective action is required, the APU still can run by another 60 hours in this condition. 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.

Which Component controls and monitors the APU?. The Fuel Control Unit (FCU). The Inlet Guide Vane Controlactuator (IGV). The Electronic Control Box (ECВ).

The Water heater in the potable water supply is: Pneumatically heated by bleed air. The water is warmed by action of the oil/water heat exchanger. Electrically powered.

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.

The Ecam Message "Low Fuel Pressure" means? Elegir una única respuesta. Low fuel press at the FCU inlet. Low fuel press detected by the APU fuel pump. Low fuel pressure delivered by the FCU.

APS 3200: 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 135 C.

What should be do if some emergency oxy panel on PSIU do not open after Oxy Sys activation?. Press the Oxygen Reset switch on the overhead panel. Pull down the cover from the test door stop. Unlatch de door with the manual release tool.

With the airplane on ground and service toillet panel open. What happen?. The toillets system is inoperative and in the FAP appears the Waste Quantity. Is possible one operation more only. The toillets System works normally.

The Waste Water system drain to: One wasted tank on the Aft. cargo compartmen. The air condition Ram Air system. The overboard through the drain masts.

About A320: Which of this statements concern to the Emergency Exit Hatches is true?. There are one overwing emergency door each side of the fuselage. Removal of the cover flap in the hatches will deploy the overwing slide. Pulling down the cover flap will turn ON the Slide Armed light between the hatches.

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.

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

The purpose of the de-oiling valve solenoid is: Reduces the pressure pump load during starting. It vents the oil sump (gearbox) to the exhaust. It separetes de air from the oil.

APS 3200: The ignition system consists of: 1 Ignition Unit and 2 Ignitor Plugs. 2 Ignition Units and 1 Ignitor Plug. 1 Ignition Unit and 1 Ignitor Plug.

Where are the overwing slide cylinders located?. Behind the belly fairing. Behind the sidewall panels of the forward cargo compartment. Behind the sidewall panels of 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.

APS 3200: The APU Bleed Control Valve is operated by: Electrical signal. Fuel pressure from the FCU. Pneumatic pressure.

The purpose of the Inlet Guide Vane Actuator (IGVA) is: Allow the operation of IGV's by air pressure. Send signals to the ECB for the open/close cycle of the Surge Valve. Regulate the load compressor inlet air flow by positioning the IGV's.

The signal for the automatic deploy of the passenger oxygen masks comes from: The Air Data Sensors. A dedicated altitude pressure switch located in the avionic compartement. Any of the ADIRUs.

CLASSIC: The unit that is connected to the CFDS system, and gives faults information of the toilet system is: The Vaccum Generator. The Vaccum System Controller. The Flush Control Unit.

Which of these zones are not pressurized?. The forward cargo compartment. Only the Bulk cardo compartment. The rear fuselage after of frame 70.

The APU fuel boost pump supplies fuel, when.... The tank fuel boost pumps are operating and the fuel pressure is high. Everytime the APU is in the startcycle. The tank fuel boost pumps are not operating and the fuel pressure is low.