Fam A320 Línea y base

When pressing the TEST PB in fire protection panel (overhead), which light is ON only as a lamp test?. FIRE PB (RED). SQUIB (WHITE). DISCH (AMBER). MASTER WARNING (RED).

In the event of a fire in any engine or APU, how is the extinguisher bottle discharged in the corresponding engine or APU. Releasing the FIRE PB after pressing the AGENT PB. Pressing the AGENT PB after releasing the FIRE PB. Just by pressing the corresponding FIRE PB. Just by pressing the corresponding AGENT PB.

What is indicated if the SQUIB white light in the fire protection panel (FIRE PB released out) is ON. . Automatic discharge of the corresponding extinguisher bottle. The arming and continuity of the bottle explosive charge circuit. Manual discharge of the corresponding extinguisher bottle. None of the above.

In the event of a fire in any engine or APU, how is the extinguisher bottle discharged in the corresponding engine or APU. Pressing the AGENT PB after releasing the FIRE PB. Releasing the FIRE PB after pressing the AGENT PB. Just by pressing the corresponding AGENT PB. Just by pressing the corresponding FIRE PB.

During a smoke condition in the avionics compartment, what happens when the EXTRACT FAN PB (ventilation panel) is set in OVRD (override) position. The blower fan continues to run and the air conditioning system is used as air source to ventilate the avionics compartment. The blower fan is stopped and the air conditioning is used as air source to ventilate avionics compartment. The extract fan is stopped and the air in the avionics compartment is dumped through the extract valve. The extract fan continues to run and the air in avionics compartment is dumped through the extract valve.

Which component monitors the smoke detectors installed in the lavatories air extraction duct. SDCU (smoke detection control unit). FDU (fire detection unit). AEVC (avionics equipment ventilation computer). All of the above.

Which component from the fire extinguishing system detects when any of the fire extinguisher bottles has been manually or thermally discharged (amber DISCH light ON). Pressure switch. Loop A/Loop B. FDU. Squib.

In the event of an APU fire in flight, the autoextinguishing system will initiate the emergency shutdown In the event of an APU fire in flight, the autoextinguishing system will initiate the emergency shutdown. False. True.

What kind of test is performed when the TEST PB in the fire protection panel is pressed. Explosive charge circuits integrity in the fire extinguisher bottles. Fire detection system loop circuits continuity and FDU integrity. Fire warnings and indications in the cockpit. All of the above.

Which one of the responder switches in the fire loop detectors (normally closed) has the function of sensing an internal pressure loss in the sensor and trigger a fault condition for the loop in the cockpit. Alarm switch. Integrity switch.

What result is obtained if any of the FDU (engines or APU) senses a Loop A & Loop B FAULT condition (failure of both loops) with the failures of the loops occurring within a time frame of less than 5 seconds. Fire warnings (Fire PB ON, Master warning, Continuos repetitive chime, ECAM warning, Etc. Loop fault (only ECAM amber message). Fire Det fault (ECAM amber message, Master caution, single chime, etc.). There is no consequences in the cockpit.

Which is the main function of the FDU (fire detection unit) for the engines and APU: To control the fire extinguishing system. To control the fire detection system. To control the fire detection and fire extinguishing system. None of the above.

In a cold aircraft configuration (completely de-energized), how is it possible to determine if the APU fire extinguisher bottle has a low pressure condition caused by thermal discharge. By means of the amber DISCH light (fire panel). By means of the white SQUIB light (fire panel). By the absence of the red disc in the fuselage. By means of CFDS.

Que sucede cuando el FQIS (fuel quantity indicating system) detecta una condición de high level en cualquiera de los tanques durante la operación de refueling. Se activa un warning en el fuel system por exceso de combustible. Se detiene completamente de manera automática la operación del refueling. Se cierra la Refuel valve correspondiente para evitar sobrellenado del tanque. Se abre la transfer valve para llenar el inner cell.

Cual es el estado de las fuel boost pumps de los wing tanks cuando las boost pumps del center tank alimentan a los motores: Encendidas, ya que funcionan todo el tiempo. Encendidas, ya que ellas tambien alimentan a los motores mientras el center tank lo hace. Apagadas, ya que las boost pumps del center tank tienen prioridad. Apagadas, ya que solo funcionan cuando el center tank está vacío.

En la página de Fuel de ECAM cuando se inicializa la indicación de FUEL USED de los motores nuevamente a Cero: Al apagar completamente el sistema. Después del apagado de los motores (engine shutdown). Al siguiente arranque de motores (engine start). Al siguiente Refueling del avión.

Con la siguiente configuración: avión en tierra, slats extendidos, MODE SEL PB en fuel control panel en AUTO mode; que fuente alimenta los motores 3 minutos después del engine start?. Los wing tank inner cells. Los wing tanks outer cells. Todos los anteriores. El center tank.

Cual es la función de las intercell transfer valves cuando éstas se accionan: Permitir el flujo de combustible del center tank hacia los inner cells. Permitir el flujo de combustible de los inner cells hacia los outer cells. Permitir el flujo de combustible de los outer cells hacia los inner cells. Permitir el flujo de combustible de los outer cells hacia los vent surge tanks.

Hacia donde libera normalmente el overpressure protector del sistema de venteo de los fuel tanks una sobrepresión dentro del outer cell de los wing tanks: Hacia el inner cell. Hacia el center tank. Hacia la atmósfera (overboard). Hacia el vent surge tank.

Cual es la función de los pressure switches de las boost pumps de los wing tanks y center tank. Determinar cuando existe una diferencia de presión suficiente para abrir las transfer valves. Controlar el encendido y apagado automático de las boost pumps. Determinar cuando existe una diferencia de presión suficiente para abrir las transfer valves. Enviar la señal de LOW PRESSURE Warning a ECAM cuando la boost pump falla.

Que componente del sistema de Refuel/Defuel permite interconectar las salidas de presión de las boost pumps del sistema (feed system) a la refueling gallery cuando se llevan a cabo operaciones de defueling o transferencia de combustible entre tanques en tierra. Refuel valve. Defuel/Transfer valve. Diffusers. Air inlet valve. Drain valve.

Cuando los wing tanks se encuentran alimentando los motores, que sucede cuando el low level sensor detecta que se han alcanzado 1650 lbs de combustible en alguno de los Inner cells de los wing tanks. Se abre la transfer valve del wing tank que tiene bajo nivel. Se cierra la transfer valve del wing tank que tiene bajo nivel. Se cierran simultáneamente las transfer valves de ambos wing tanks. Se abren simultáneamente las transfer valves de ambos wing tanks.

Que componente del sistema de combustible permite alimentar los motores por gravedad cuando no tenemos fuentes de presión (boost pumps) disponibles: LP Valve. Sequence valves. By-pass suction valves. Crossfeed valve.

How is the TLA (thrust lever angle) transmitted to the EEC, when the engine thrust levers are moved in the cockpit. By means of mechanical movement supplied by the thrust lever resolvers. By means of cables and pushrods between the thrust levers and the fuel metering unit. None of the above. By means of electrical signals supplied by the thrust lever resolvers.

Which component from the lubrication system is utilized to monitor if any of the gearbox internal components is suffering from excessive wear. The scavenge pump. The pressure filter. The No. 4 bearing scavenge valve. The master magnetic chip detector.

What air is used in the turbines Active Clearance Control ACC. Fan air. 7th and 10th compressor stage air. Engine core air. 12th compressor stage air.