TEST BORRADO, QUIZÁS LE INTERESE: FER
COMENTARIOS |
ESTADÍSTICAS |
RÉCORDS
|
|---|
REALIZAR TEST
|
Título del Test:
FER Descripción: T INTERIORES PART = 8 Autor: FER OTROS TESTS DEL AUTOR Fecha de Creación: 23/03/2025 Categoría: Otros Número Preguntas: 65 |
COMPARTE EL TEST
Comentar
No hay ningún comentario sobre este test.
Temario:
|
Where are hydraulic pipes located within the aircraft? Passenger cabin and flight compartment Only in the flight compartment Only in the passenger cabin In the aircraft except in Passenger cabin and flight compartment. What is the nitrogen pressure set to during the pressurization of the reservoir? 30 PSI 40 PSI 50 PSI 60 PSI. Before starting the filling procedure, what must be the position of the flight control surfaces and cargo doors? Neutral retracted position Fully extended position Open position Any position. What should the triple indicator show when the yellow electric pump is selected to OFF? Hydraulic system pressure Brake accumulator pressure Nitrogen pressure Green hydraulic pressure. Why should a warning notice be placed before operating the hydraulic system? To indicate the system is depressurized To prevent others from operating the system To remind the operator to wear gloves To indicate the cargo doors are closed. What is done with the hand pump lever from the yellow panel during the filling operation? It is removed and assembled for use on the green panel It is left in place It is disconnected and stored in a toolbox It is used to depressurize the system. What precautions should be taken before removing the flexible hose from its housing? Wear proper protection gloves and goggles Disconnect the hydraulic system Depressurize the nitrogen pressure Ensure the cargo doors are open. How is the selection of the hydraulic system to be filled confirmed? A colored LED on the indication panel A sound alert A pressure gauge reading An audible beep. Where should the system reservoir be filled to during the filling operation? To the end of the scale To the last white line in the related colored band To the top of the reservoir To the halfway mar. What subsystem protects the engine air intake from ice? Probe ice protection Windshield ice and rain protection Engine air intake ice protection Drain mast ice protection. Which part of the aircraft's electrical system heats the water and waste system for ice protection? Visual lighted ice detection Electronic ice detection system Engine bleed air Hot air from the pneumatic system. How is the operation of the rain repellent system controlled on the CAPT and F/O sides? Independently Simultaneously Manually Automatically. What is used to initiate a new cycle of rain repellent fluid spray? Press the P/B once Press and hold the P/B Release and press the P/B again It starts automatically. The wing anti-ice supply to both wings is controlled by a single pushbutton switch on the overhead ANTI ICE panel True False. Engine anti-ice is only available in flight and not on the ground with the engine running. True False . The PROBE/WINDOW HEAT pushbutton switch is used to select windshield anti-icing when the engines are shut down. True False. Each Control Unit (CU) regulates the heating temperature of the associated drain mast tube between ______ 0°C (32°F) to 6°C (43°F) 6°C (43°F) to 10°C (50°F) 10°C (50°F) to 15°C (59°F) 15°C (59°F) to 20°C (68°F). The system status is sent to the Cabin Intercommunication Data System (CIDS) for indication on the _______ pilot's display maintenance logbook Flight Attendant Panel (FAP) Centralized Fault Display Interface Unit (CFDIU). If there is a failure of the Heater (HTR) or CU, a _______ light is illuminated on the Flight Attendant Panel (FAP). green red CAUTion maintenance. The drain mast data is stored in the ______ aircraft's central server maintenance logbook Centralized Fault Display Interface Unit (CFDIU) Flight Attendant Panel (FAP). To perform a complete test of the drain mast system, two tests must be carried out, one from the MCDU, and the second one on each ______ flight attendant maintenance technician Control Unit (CU) aircraft. How are the CLeaR P/Bs used in response to a system failure? They turn off the power to the Display Units (DUs) They release the Fault lights on the hydraulic panel They indicate the phase of the flight They clear the warnings and cautions. What are the primary parameters displayed in the upper area of the Engine/Warning Display (EWD)? Engine Pressure Ratio (EPR) Slat/flap position Fuel On Board (FOB) All of above. The Electronic Centralized Aircraft Monitoring (ECAM) system displays weather information. True False. In normal operation, DMC 1 drives the Captain's Primary Flight Display (PFD), while DMC 2 drives the First Officer's PFD. True False. The CLeaR P/Bs are used to activate the warnings and cautions. True False. The STATUS REMINDER and RECALL FUNCTION reminds the crew of cleared warnings. True False. The System Data Acquisition Concentrators (SDACs) send data to the Electronic Flight Instrument System (EFIS) displays True False. Level 3 alerts correspond to an emergency configuration where corrective or palliative action must be taken by the crew ___ immediately without any action after a crew meeting during routine maintenance. A primary failure is a failure of an equipment or system causing the loss of __________ equipment. secondary other independent advisory. In ECAM Normal Dual Display mode, the flashing ADV symbol indicates multiple advisories on different pages or a failure _ on the currently displayed page detected by the FWC requiring immediate action in the ECP. In ECAM MONO Display mode, when a value drifts from its normal range, a white ADV message flashes in the center of the EWD to attract crew _____ monitoring attention routine maintenance emergency response. Level 3 warnings are associated with a Continuous Repetitive Chime (CRC), warning messages on Liquid Crystal Display (LCD), and a flashing _______ caution light advisory light caution message MASTER WARNing light. What are the two primary functions of the Flight Data Interface and Management Unit (FDIMU)? Flight Data Interface Unit (FDIU) and Data Management Unit (DMU) Data Loading Selector (DLS) and Multipurpose Disk Drive Unit (MDDU) Digital Flight Data Recorder (DFDR) and Quick Access Recorder (QAR) Linear Accelerometer (LA) and System Data Acquisition Concentrator (SDAC). What does the FDIU-part of the FDIMU do with the input parameters? Transmits them to the Digital AIDS Recorder (DAR) Converts, compares, and checks them Records them in data frames Routes them to the Data Loading Routing Box (DLRB. When does the FDIU-part check the integrity of the mandatory parameters during a flight? Continuously throughout the flight After the engines are shut down Before engine start Only during maintenance checks. What is the purpose of the underwater locator beacon on the DFDR? To activate the DFDR To provide the location of the recorder in water after an accident To transmit data to the CFDIU To control the power interlock circuit. How long does the DFDR store data? 24 hours 48 hours 25 hours 72 hours. What type of data frames are stored in the Quick Access Recorder (QAR)? Identical to the DFDR data frames Data frames with additional information Video data frames Audio data frames. What is the purpose of the Data Loading Selector (DLS)? To select the computer on which data will be loaded To upload or download data To stow data disks To route data between the disk unit and target computer. The Flight Data Interface and Management Unit (FDIMU) combines two functions: the Flight Data Interface Unit (FDIU) and the _______ Data Management Unit (DMU) Quick Access Recorder (QAR) System Data Acquisition Concentrator (SDAC) Linear Accelerometer (LA). The FDIU-part of the FDIMU converts, compares, andchecks the input parameters for the Digital Flight Data Recorder (DFDR), optional Quick Access Recorder (QAR), and the Digital AIDS Recorder (DAR). This conversion process is crucial for data ________ recording transmission storage analysis. The DFDR stores data for the last ________ hours, with each data frame containing information from one second of flight. 24 48 25 72. The Quick Access Recorder (QAR) records the same data parameters as the DFDR but is primarily used for on-ground performance, maintenance, and condition monitoring tasks. It also includes Built-In Test Equipment (BITE) functions to ensure data ____. accuracy integrity encryption compression. The LA generates an analog signal, which is then digitalized and sent to the FDIU-part through an ____________ bus. Ethernet USB ARINC 429 HDMI. The Data Loading Selector (DLS) is responsible for selecting the ____ on which data will be loaded during maintenance processes computer technician disk drive software. The Multipurpose Disk Drive Unit (MDDU) is used to upload or download data, and it has a stowage box with a maximum capacity of ______ data disks. 12 24 36 42. When does the active LGCIU change in the extension/retraction system? After each gear cycle During a DOWN selection When a failure occurs in the active LGCIU When the LGCIUs are electrically segregated. In what conditions is normal braking obtained? With the parking brake OFF When gear control lever is set to UP Without green hydraulic pressure With A/SKID switch OFF. When is electrical control for normal braking obtained? In flight when the gear control lever is set to UP On the ground by the auto brake system When the green hydraulic pressure is available Through the pedals. What system energizes the alternate brake system in the Airbus A320 family aircraft? Green hydraulic system Brake accumulator Normal brake system Parking Brake control switch. When does the ABCU become active in the alternate brake system? When normal brake system is defective When the A/SKID & N/W STeeRinG switch is OFF When the green system has low hydraulic pressure When the BSCU is working properly. What happens if there is a BSCU failure or low pressure in the hydraulic systems in relation to the anti-skid function? The pilot must use the triple pressure indicator to control brake pressure The ABCU sets a minimum limit of 1000 PSI for brake pressure The anti-skid function is lost, and braking is unavailable The A/SKID & N/W STeeRinG switch is disabled. How many full brake pedal applications can be done with the accumulator pressure alone? 3 7 Unlimited 5. What are the limits for the N/WS angle controlled by the BSCU? Rudder pedals: max 6 degrees; Hand wheels: max 74 degrees Rudder pedals: max 10 degrees; Hand wheels: max 50 degrees Rudder pedals: max 5 degrees; Hand wheels: max 80 degrees Rudder pedals: max 8 degrees; Hand wheels: max 60 degrees. What does the Brake Temperature Monitoring Unit (BTMU) transmit to the BSCU? Brake temperature data Hydraulic pressure Brake pedal inputs Brake accumulator pressure. If a failure occurs in the active LGCIU, the __________ LGCIU becomes active. secondary standby duplicate alternate. Normal braking is obtained when: - The green hydraulic pressure is available, - The Anti/SKID and Nose/Wheel Steering control switch is in the __________ position, - The Parking Brake control switch is in the OFF position. ON OFF standby alternate. Where are ANN LT TEST AND INTERFACE BOARDS located? In the cockpit In the avionics compartment In the passenger cabin In the engine room. How many relays supply the ANN LTs when the switch 33LP is in the TEST position? 1 relay 2 relays 4 relays 10 relays . Where is the COCKPIT ANN LT SWITCH located? In the avionics compartment On the overhead control panel In the cabin 2000 VU Panel. How are cabin lights controlled in the aircraft? Through the Cabin Intercommunication Data System Through the landing gear Through the cockpit controls Through the engine system. What is the purpose of DEUs in controlling cabin lights? To control the engine To control the cockpit lights To control the fluorescent lamps To control the landing gear. How many strobe lights are installed at each wingtip and tail cone? One strobe light Two strobe lights Three strobe lights Four strobe lights. What does the "STROBE LT OFF" ECAM memo message indicate? The strobe lights are malfunctioning The strobe lights are on The strobe lights are off The strobe lights are dimming. |
Denunciar Test