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TEST BORRADO, QUIZÁS LE INTERESEA320

COMENTARIOS ESTADÍSTICAS RÉCORDS
REALIZAR TEST
Título del test:
A320

Descripción:
A320 A1

Autor:
AVATAR

Fecha de Creación:
25/06/2018

Categoría:
Otros

Número preguntas: 27
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Temario:
Conditioned air is distributed to Cockpit, cargo bays and cabin Cockpit, fwd and aft cabins Cockpit, avionics bay and cabin Cockpit, cabin and holds 1 and 2 only.
The main function of the Pack Flow Control Valve (FCV) is to regulate. Bleed air flow Bleed air pressure Bleed air temperature.
The Emergency Ram air supply system is controlled Automaticaly by the Air Conditioning System Controller (ACSC) Manually throungh the Air Cond Panel 30vu Automatically by the FCV.
To Control the Avionics Ventilation, The AEVC uses. Air conditioning temperature, EIU signals and groundflight signals. Air conditioning pressure, FADEC signals and ducts temperature Fuselage skin temperature and GroundFlight logics.
The Pressurization system is automatically controlled by the Cabin Pressure Controller (CPC) Avionics Equipment Ventilation Controller (AEVC) Air Conditioning System Controller (ACSC).
The air which supplies the Avioonics Equipment Ventilation during flight comes from External air The cabin air LH pack.
The Lavatory and Galley air extraction is ensured by Differencial pressure only Differencial pressure and three fans. An extraction fan.
The Residual Pressure Control Unit (RPCU) is used In flight as a back-up of the CPC's To avoid any residual pressure in the cabin,when the aircraft is on ground For manual control of both outflow valves via the cabin press panel.
Both Air Conditioning System Controller (ACSC), Are connected to the CFDIU Directly Via the Air Conditioning System Control 2 These control's are not connected to the CFDIU.
The Flow Control Valve (FCV) Closes By Energized a torque motor De-energized a torque motor De-energized a solenoid 1.
To dispatch the aircraft, tne skin air outlet valve must be "de-activated" according by MEL with The main flap open The auxiliary internal flap open The main and auxiliary flap closed.
The purpose of the BY-Pass Valve is Add some hot or cool air to maintain the selected termperature Add hot air to maintain the basic temperature Add cool air to maintain the selected temperature.
THE PURPOSE OF THE PACK CHECK VALVE IS TO STOP BYPASS The primary and main heat exchangers The ACM (air Cycle Machine) turbine in case of ACM failure Leakage of air from distribution system in case of ACM failure.
IN NORMAL MODE, THE PACK TEMPERATURE REGULATION IS ACHIEVED THROUGH THE Anti-ice Valve and the ram air doors Ram air doors and by pass valve Antu-ice valve and the by pass valve.
ICE BUILD-UP PREVENTION IN THE AIR CYCLE MACHINE (ACM) IS ENSURED BY THE Temperature control valve Ram air flaps Anti-ice valve.
THE EMERGENCY RAM AIR INLET FLAP OPENS Whenever the RAM AIR pushbuttom is selected ON and DITCHING P/B remain OFF When the DITCHING P/B is selected ON AND the difference of pressure < 1PSI In auto mode with a loos of both packs.
IN FLIGHT, WHEN SWITCHING THE EMERGENCY RAM AIR PUSHBUTTON TO ON, THE OUTFLOW VALVES Open immediately slowly opens Open at half position when cabin differential pressure is less than 1psi.
IN NORMAL CONDITION, THE AVIONICS VENTILATION SYSTEM IS Automatically controlled by the Landing Gear Control Interface Unit (LGCIU) Manually controlled by the EXTRACT or DITCHING P/B SW Automatically controlled by the Avionics Equipment Ventilation Controller (AEVC).
THE CHECK RECIRCULATION VALVES ARE Always open as soon the recirculation fans run Closed if both packs are off Closed if both packs are on.
THE COLS AIR SOURCE FOR THE FORWARD CARGO COMPARTMENT IS Pack 1 Pack 2 Pack 3.
THE FORWARD CARGO INLET AND OUTLET ISOLATION VALVES CLOSE IF THE Extraction fan fails Air conditioning pack 2 fails Forward cargo smoke warining is geven .
ONE FUNCTION OF EACH AIR CONDITIONING PACK IS TO PROVIDE A basic temperature regulation according to a demand from the ACSC (air conditioning system controller) A fine temperature regulation according to a demand from the pach controllers A temperature regulation of air coming from the recirculation fans.
THE RAM AIR INLET FLAP AND BY PASS VALVE MODULATE THE AIR TEMPERATURE By adding hot air to the ACM outlet To obtain a short term temperature regulation To obtain a long term temperature regulation.
SETTING THE HOT AIR 1P/BSW MANUALLY TO OFF, LEADS TO Automatic opening of the Trim Air Shut-off Valve (TASOV) Automatic opening of Trim Air Pressurizing Valve 1 (TAPRV) De.energizing of TAPRV1 solenoid and keedping the TAV in closed position.
ON GROUND. DIRECT CABIN VENTILATION CAN BE OBTAINED BY CONNECTING A GROUND The pneumatic HP port The LP ground connectors The emergency ram air inlet.
THE MAIN FUNCTIONS OF THE FLOW CONTROL VALVE (FCV) ARE TO Shut off bleed air supply and to regulate bleed air flow Optimize fresh air supply to the cabin and to supply air to the avionics equioment Prevent ice build-up in the water extraction loop and to regulate bleed air flow.
WHEN DOES THE SKIN EXCHANGER INLET BY PASS VALVE OPEN In open circuit configuration In closed or intermediate circuit configuration Whrn the ambient avionics bay temoerature is above 35*C.
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