TEST BORRADO, QUIZÁS LE INTERESE: FER
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FER Descripción: T INTERIOES PART = 9 Autor: FER OTROS TESTS DEL AUTOR Fecha de Creación: 23/03/2025 Categoría: Otros Número Preguntas: 53 |
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What triggers the NEOL indication on the strobe light assemblies landing gear malfunction The strobe lights are on The strobe lights are off The strobe lights are near the end of their useful life. What is the purpose of wing and engine scan lights? To signal to air traffic control To illuminate the wings and engine air intake To control the landing gear To provide light for passengers. The ANN LT TEST AND INTERFACE BOARDS are located in the passenger cabin True False. The COCKPIT ANN LT SWITCH has only two positions: DIM and BRT. True False. DEUs control the cabin fluorescent lamps based on signals from the FAP True False. How do ring laser gyros measure rotation? By detecting differences in laser beam frequencies By analyzing magnetic field variations By measuring changes in air pressure tracking GPS satellite positions. What is the primary output of the ring laser gyros? Analog rotation information Digital altitude data Magnetic heading information Inertial velocity measurements. What do the accelerometers in the ADIRUs provide? Linear accelerations Barometric altitude data Air temperature variations Aircraft ground speed. How is the acceleration signal processed in the ADIRUs? Sent to an analog/digital converter Transmitted directly to the MMR units Converted into GPS coordinates Sent to the Weather Radar system. How is the ILS descent axis determined? By the intersection of a Localizer and Glide Slope beam By GPS coordinates By analyzing air pressure variations By the aircraft's altitude. What is the primary function of the ILS (Instrument Landing System)? Supply signals transmitted by ground stations Provide GPS coordinates Measure atmospheric corrections Control air traffic in the vicinity of the airport. How is a descent axis determined in the ILS? By the intersection of a Localizer beam and Glide Slope beam By analyzing the aircraft'saltitude By measuring magnetic field variations By tracking GPS satellite positions. What is the primary purpose of the GPS (Global Positioning System)? Provide accurate navigation information Control air traffic Measure atmospheric pressure variations Transmit signals to ILS ground stations. How is the GPS spatial segment composed in terms of satellite arrangement? 24 satellites in six separate orbital planes 12 satellites in one orbital plane 48 satellites in 12 orbital planes 6 satellites in a single orbital plane. Where are the Multi-mode Receivers (MMR) typically located on the aircraft? In the forward avionics bay 90VU In the cockpit dashboard On the wings of the aircraft In the upper fuselage near the GPS antennas. What are the external sensors that provide inputs to the ADIRUs in the ADIRS system? Angle Of Attack (AOA), Total Air Temperature (TAT), and Air Data Module (ADM) Static Air Temperature (SAT), International Standard Atmosphere (ISA), and Total Air Temperature (TAT) Static ports, Pitot probes, and AOA sensors GPS coordinates, ground speed, and altitude. What are the primary components of the WXR and PWS system? Weather radar transceiver and weather antenna drive Aircraft engines and landing gear Avionics bay and ILS Weather radar transmitter/receiver and dual weather radar control unit. Why is the crew oxygen system used? To supply oxygen during normal flight To supply oxygen during cabin pressurization loss To supply oxygen during passenger emergencies To supply oxygen to the cabin attendants. How is the pressure of the oxygen cylinder indicated to the crew? By a pressure regulator By a direct-reading pressure gauge By a pressure switch By a low-pressure warning light. Under what conditions do the passenger oxygen masks automatically deploy? When the cabin altitude exceeds 14,000 feet When the cabin altitude is below 10,000 feet When a passenger pushes the MASK MANual ON button When a crew member pushes the MASK MANual ON button. What happens when the TiMeR RESET pushbutton is pushed in the passenger oxygen system? The masks retract automatically The electrical system is rearmed The passenger address system is activated The oxygen supply is shut off. What initiates the chemical generation in the oxygen masks? Pulling the mask towards the user's face Pressing the oxygen supply button Opening the container door Pushing the ON white light. How many Crew oxygen bottles the A320 Neo has? 1 3 2 None. What is the purpose of the tamper seal in the portable oxygen container? To indicate the oxygen level To indicate if the PBE is operational To show if the container is properly sealed To signal low oxygen pressure. The oxygen system includes: the crew system the passenger system the portable system all above. The flight crew oxygen system is used if there is a loss of cabin pressurization or ____________ in the cockpit. Fire Water Smoke smoke or dangerous gases. The high-pressure portable cylinder includes continuousflow type masks and supplies first aid oxygen to the passengers the cargo hold the overhead bins the cabin attendants. There are two types of chemical generators supplying oxygen for 15 minutes or 22 minutes True False. The Portable Breathing Equipment (PBE) is designed to help crew members and cabin attendants extinguish fires by supplying oxygen True False. How is the engine air bleed pressure pneumatically regulated in the Airbus A320 family of aircraft? High Pressure (HP) Valve (VLV), Pressure Regulating Valve (PRV) Bleed Monitoring Computers (BMCs), Wing Anti-Ice (WAI) Pressure Regulating Valve (PRV), High Pressure (HP) Valve (VLV) Wing Anti-Ice (WAI), Bleed Monitoring Computers (BMCs). When does the HP VLV pneumatically regulate the air supply, and within what pressure range does it operate? At low engine speed, 8 to 36 psi At high engine speed, 44 to 85 psi At idle, 110 to 240 psi At high altitude, 15,000 ft to 35,000 ft. What is the primary function of the IP check valve, and when does it come into play? Protects the IP stage from reverse flow when HP VLV is open Regulates the pressure downstream from the PRV Monitors engine fire at 450°C Controls bleed pressure at high altitude. Describe the two operating modes of the PRV control solenoid and the conditions under which each is used. Pneumatic mode for reverse flow protection, electrical mode for ENGine BLEED P/B OFF Pneumatic mode for overpressure, electrical mode for engine fire Pneumatic mode for engine fire, electrical mode for altitude > 15,000 ft Pneumatic mode for delta pressure, electrical mode for precooler temperature. The engine air bleed pressure is pneumatically regulated by the _____ when air is supplied by the HP stage, or by the _____ when the air is supplied by the Intermediate Pressure (IP) stage. High Pressure (HP) Valve (VLV), Pressure Regulating Valve (PRV) Bleed Monitoring Computers (BMCs), Wing Anti-Ice (WAI) Pressure Regulating Valve (PRV), High Pressure (HP) Valve (VLV) Wing Anti-Ice (WAI), Bleed Monitoring Computers (BMCs). When does the HP VLV pneumatically regulate the air supply, and within what pressure range does it operate? At low engine speed, 8 to 36 psi At high engine speed, 44 to 85 psi At idle, 110 to 240 ps At high altitude, 15,000 ft to 35,000 ft. What controls and monitors the system functions and related electric components in the vacuum toilet system? The Flight Attendant Panel (FAP) The waste holding tank The Flush Control Unit (FCU) The Cabin Intercommunication Data System (CIDS). What happens when the waste holding tank is full in the toilet system? The waste is automatically ejected The toilet system shuts down The waste is recycled The waste is diverted to the potable water tank. The water and waste indications are displayed automatically as soon as the service panel is open. True False. On the Flight Attendant Panel (FAP), the filling quantity cannot be selected as an option True False. There is only one control handle on the water service panel. True False. On the A320, the overflow valve opens mechanically when the fill/drain control handle is set to the drain position. True False. When does the "Overflow Valve Light" come on, and what does it indicate when the valve is in the open position? The "Overflow Valve Light" comes on during draining, indicating that the valve is closed The "Overflow Valve Light" comes on during filling, indicating that the valve is open The "Overflow Valve Light" comes on when the air compressor is activated The "Overflow Valve Light" comes on when the tank is empty. The Fill/Drain control handle is initially positioned to "drain" when filling the water tank. True False. The "Green Tank Full Light" comes on when the tank is empty. True False. What happens when the toilet service panel door is open on the ground? All toilet operations are stopped through DEU B Flush signals are inhibited The vacuum generator starts automatically The waste holding tank is drained. What is the primary purpose of the drain control handle located at the service panel? Initiating the vacuum generator Controlling cabin pressurization Initiating waste holding tank draining Activating the DEU B. The Fuel Tank Inerting System (FTIS) includes two subsystems: The Fuel Tank Ventilation System (FTVS) The Air Conditioning System (ACS) The Engine Bleed Air System (EBAS) The Airplane Mode Selector (AMS) . The CSAS gets hot air from the Engine bleed air system and decreases its temperature to a level compatible with the IGGS sub-system. The CSAS Inert Gas Generation System (IGGS) The CSAS Conditioned Service Air System (CSAS) The CSAS Engine Bleed Air System (EBAS) The CSAS Air Conditioning System (ACS). Engine 1 is the primary bleed source and Eng 2, through the X Bleed valve, is the secondary bleed source. Engine 1 is the secondary bleed source Engine 2 is the primary bleed source Engine 2 is the secondary bleed source Engine 1 is the primary bleed source. . The bypass valve is installed in the heat exchanger bypass duct and is controlled by the CSAS The bypass valve adds cold air downstream of the heat exchanger The bypass valve adds hot air downstream of the heat exchanger The bypass valve controls the ozone converter The bypass valve is not used in the CSAS. If there is over-pressure or over-temperature, the CSAS isolation valve closes to stop the system The CSAS isolation valve opens to release pressure The CSAS isolation valve remains unaffected by temperature changes The CSAS isolation valve closes in normal operation The CSAS isolation valve has no impact on pressure. In normal operation, the CSAS isolation valve is open to let the air go through the ozone converter The CSAS isolation valve remains closed The CSAS isolation valve opens after the ozone converter The CSAS isolation valve opens after the heat exchanger The CSAS isolation valve is not used in normal operation. What is the primary function of the IP check valve, and when does it come into play? Protects the IP stage from reverse flow when HP VLV is open Monitors engine fire at 450°C Regulates the pressure downstream from the PRV Controls bleed pressure at high altitude. |
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