TEST BORRADO, QUIZÁS LE INTERESE:
A 320 LANDING GEAR, DOORS AND EQUIPMENT Y LIGHTS
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Título del Test:
A 320 LANDING GEAR, DOORS AND EQUIPMENT Y LIGHTS Descripción: LANDING GEAR, DOORS AND EQUIPMENT Y LIGHTS Autor: Walter Moreira OTROS TESTS DEL AUTOR Fecha de Creación: 30/01/2014 Categoría: Test de conducir Número Preguntas: 81 |
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1.- If normal electrical power is lost, essenttial cockpit lighting is maintained
for the: A.- Captain\'s instrument panel. B.- Standby compass. C.- Right dome light (provided the dome selector is not off). D.- All off the above. 2.- All cabin signs come on automatically when the cabin altitude exceeds_________ feet, regardless of the respective switch position. A.- 9.550 B.- 10.000 C.- 11.300. 3.- The strobe light selector is set to auto. In this position, when do the strobe lights stop flashing? A.- When the aircraft touches down. B.- When the first reverser is deployed. C.- When the landing lights are switched off. D.- When the last engine has been shut down. 1.- If the accumulator on the alternate brake system is your only source pressure, which of the following will be available? A.- Auto brakes and antiskid. B.- Antiskid. C.- Seven applications of the brake pedals. 2.- Can normal landing gear operation be restored after a gravity extension if green hydraulic pressure is available? A.- Restoration is always possible. B.- It may be possible if the gravity extension was not caused by a failure of the landing gear mechanism. C.- No, only maintenance can restore normal operation. 3.- The.............. hydraulic system provides power for gear extension/retraction. A.- Yellow. B.- Blue. C.- Green. 4.- As long as the landing gear lever is up a hydraulic safety valve closes to cut off the hydraulic supply to the gear when the airspeed is: A.- Greater than 260 kias. B.- Greater than 230 kias. C.- Less than 260 kias. 5.- The normal brake system uses ________ hydraulic pressure and the alternate brakes use_______ system pressure, with_____ backup. A.- Green, blue, an electrical. B.- Green, yellow, an accumulator. C.- Green, yellow, an electrical. 6.- Autobraking is initiated by. A.- Strut compression. B.- Reverser action. C.- Ground spoiler extension command. 7.- The alternate brake system has the same capabilities as normal brakes except: A.- Anti-skid is inoperative. B.- Autobrakes are inoperative. C.- Both A and B. 8.- When using the alternate brake system on accumulator pressure only, the accumulator supplies: A.- Partial brakes. B.- At least seven full brake applications. C.- Alternate brakes with antiskid. 9.- The green decel light on the autobrake switch illuminates when the actual airplane deceleration corresponds to ________% of the selected rate. A.- 80 B.- 95 C.- 100. 10.- The brakes pressure indication on triple pressure indicator reads which system pressure? A.- Yellow. B.- Blue. C.- Green. 11.- Which hydraulic system supplies pressure to the nose wheel steering? A.- Green. B.- Blue. C.- Yellow and Blue. D.- Green and Blue. 12.- If the brake system automatically transitions to alternate brakes with the A/SKID & N/W STRG switch in the ON position, which of the following will be available? A.- Auto brakes and anti-skid. B.- Only auto brakes. C.- Brakes, auto brakes, anti-skid. D.- Anti-skid. 13.- What is indicated by the autobrake DECEL lights? A.- airplane deceleration is 25% of selected rate. B.- Airplane deceleraton is 50% of selected rate. C.- Airplane deceleration is 100% of selected rate. D.- Airplane deceleration is 80% of selected rate. 14.- On the E/WD, you notice the NW STRG DISC memo. What does it mean? A.- The nose wheel steering has been disconnnected by ground personnel. B.- A failure in the nose wheel steering system has been detected. C.- There is a discrepancy between the two nose wheel steering handwheel positions. D.- The nose wheel sterring computer has finished its self test. 15.- During pushback, you start engine #2. You observe the NW STRG DISC memo has changed to amber. Why? A.- The NW STRG disconnect mechanism has failed. B.- The yellow hydraulic system is now pressurized and the amber caption is a warning not to move the handwheel. C.- The nose wheel steering is being reconnected by ground personnel. It is amber because the pin is removed. D.- The memo has become amber because one engine is running. 16.- The maximun degree of nose wheel steering available when using the steering handwheel is ________. A.- +/- 60 B.- +/- 75 C.- +/- 95. 17.- If the Landing Gear was gravity extended using the hand crank on the center pedestal, landing gear position must be verified through. A.- The landing gear viewers. B.- The landing gear indications depicted on the ECAM and, if available, the center panel LDG GEAR indicator panel lights. C.- Both are correct. 18.- Landing gear operation is inhibited at speeds: A.- Below 100 knots. B.- Above 260 +/- 5 knots. C.- Below 100 knots and above 260 knots. D.- Above 250 knots. 19.- Can the gear be extended above 260 kts if necessary? A.- Never. B.- Yes, but manually only. C.- Yes, but the ultimate limit is 285 kt CAS. 20.- Which hydraulic system(s) supply pressure to the landing gear system? A.- Green. B.- Blue. C.- Yellow and Blue. D.- Green and Blue. 21.- The antiskid deactivates when ground speed is less than _____. A.- 10 kts. B.- 20 kts. C.- 25 kts. D.- 30 kts. 22.- If the BSCU detects a brake system malfunction in flight with the A/SKID & N/W STRG switch in the ON position. A.- The crew will be notified with an ECAM message after touchdown if the brake system does malfuncition. B.- The crew will be notified with an ECAM message. C.- The crew must manually select alternate brakes. D.- All of the above. 23.- What is required to arm the auto brakes? A.- Green hydraulic pressure available, anti-skid, no failures in the braking system. B.- Landing gear lever selected down and selection of an autobraking rate. C.- Both are correct. 24.- What does each turn of the gravity gear extension handle do? A.- Open gear door, unlock gear, drop gear. B.- Open gear doors, drop gear, shut doors. C.- Shutoff hydraulic pressure, open doors, unlocks gear. D.- Open gear doors, shutoffs hydraulics, unlock gear, drop gear. 25.- How do you manually extend the landing gear? A.- Lift the red handle and turn anticlockwise 4 turns. B.- Lift the red handle and turn anticlockwise a minimum of 2 turns. C.- Lift the red handle and turn clockwise a minimum of 4 turns. D.- Lift the red handle and turn clockwise a 3 tun. 26.- How many turns are required on the gravity extension hand crank to extend the landing gear? A.- 2 B.- 3 C.- 5 D.- 6. 27.- If the Landing Gear was gravity extended using the hand crank on the center pedestal, what other systems will be inoperative? A.- Nose wheel steering and auto braking B.- Nose wheel steering only. C.- Anti-skid and auto braking. D.- Nose wheeel steering and anti-skid. 28.- Auto brake may be armed with the parking brake on. A.- True. B.- False. 29.- When the landing gear is gravity extended, will nose wheel steering be available? A.- Only if the A/SKID & N/W STRG switch is selected ON. B.- No. C.- Limited nose wheel steering is available only through the captian's rudder pedals. 30.- Auto brakes, if selected, will only be activated by: A.- The wheels spinning up. B.- The struts being compressed. C.- The brake pedals being depressed. D.- The ground spoiler extension command. 31.- There are two triangles for each gear on the ECAM WHEEL page. What do they represent? A.- Each triangle represents one wheel on the gear. B.- Each triangle represents the position detected by one of the two computers systems. C.- Each triangle represents one of the braking systems available for that gear. D.- The front triangle indicates the position of that gear and the back triangle indicates the status of the brakes for that gear. 32.- What system pressure does the ACCU PRESS and BRAKES pressure indicator indicate? A.- Yellow brake accumulator and yellow brake system pressure to the left and right brakes. B.- Yellow brake accumulator and green brake system pressure to the left and right brakes. C.- Yellow brake accumulator and green or yellow brake system pressure to the left and right brakes. D.- Blue brake accumulator and green brake system pressure to the left and right brakes. 33.- ECAM: if you see a green arc shown over a wheel indication. A.- It marks the hottest brake with a temperature of more than 100ºC. B.- It indicates an abnormal high temperature. C.- The A/SKID system is automatically releasing the pressure of that brake. D.- TheL/G control system has detected a low tire profile. 34.- Nose wheels and main wheels have fusible plugs that prevent the tires from busting if they overheat. A.- True. B.- False. 35.- With the A/SKID & N/W STRG switch in the ON position, if the BSCU detects a brake system malfunction and/or normal braking is not available: A.- The crew will be notified with an ECAM message only if after touchdown the brake system does actually malfunction. B.- Transition to the alternate brake system is automatic. 36.- You have just set the parking brake handle to ON. Is it still possible to check the main brake system using the toe brakes? A.- Yes. As soon as you press the brake pedals the BRAKES indicator will read main system pressure. B.- No. It is not possible to press hard enough to obtain an accurate reading. C.- No. When the PARK BRK is set, the other braking modes are deactivated. 37.- The gear doors remain open after a manual extension. A.- True. B.- False. 38.- The steering handwheels, which are interconnected, can steer the nose wheel up to:_____ in either direction. A.- 55º B.- 65º C.- 75º D.- 90º. 39.- Each main wheel has an antiskid brake. A.- True. B.- False. 40.- The parking brake accumulator is designed to maintain the parking pressure for at least _____. A.- 6 hours. B.- 12 hours. C.- 18 hours. D.- 24 hours. 41.- The autobrake will arm if at least one ADIRS is functionning. A.- True. B.- False. 42.- What happens to the other brake modes when parking brakes are applied? A.- There is no change. B.- All other braking modes and antiskid are deactivated. C.- Antiskid mode only is deactivated. 43.- How can the brake accumulator be re-pressurized? A.- With the yellow electric hydraulic pump. B.- With the blue electric hydraulic pump. C.- Both are correct. 1.- The PBE provides a breathable atmosphere for approximately ____ minutes. A.- 10 B.- 15 C.- 16 D.- 18. 2.- What happens to the cockpit door with electrical power failure? A.- It operates normally on HOT BAT bus. B.- It automatically unlocks. C.- It automatically locks from outside but stays unlock from inside. 3.- When the electric pump is operating the FWD or AFT cargo doors, the only other yellow system devices that can operate are braking and engine 2 reverse. A.- True. B.- False. 4.- The cargo doors are powered by: A.- The blue electric pump. B.- The yellow hydraulic system before engine start and the green hydraulic system after engine start. C.- The yellow hydraulic system. D.- The blue hydraulic system before engine start and the green hydraulic system after engine start. 5.- The forward and aft cargo doors can be opened from: A.- The inside and the outside. B.- The outside only. 6.- If door handle is lifted and the white indicator illuminates, what does this mean? A.- The escape slide is armed and if you go on lifting the handle, door opens and slide will deploy. B.- Pneumatic assistance of the door has failed. C.- The escape slide is in disarmed configuration. D.- The cabin is still pressurized. 7.- On the cockpit overhead panel there is a three position EMERGENCY EXIT LT switch. What lights are associated with this switch? A.- Exit signs, emergency lights, and floor path lights. B.- Exit signs, emergency lights, main panel flood lights, and floor path lights. C.- Exit signs, emergency lithts, dome lights, main panel flood lights, and the standby compass light. D.- Exit signs, and the standby compass light. 8.- What is Crew Oxygen minumum pressure, where can it be read? A.- 850 PSI, ECAM DOOR/OXY page. B.- 950 PSI, gauge on the bottle. C.- 1000 PSI, gauge on the bottle. D.- 1500 PSI , ECAM DOOR/OXY page. 9.- There is no other way of deploying the overwing escape slide if it fails to deploy automatically on opening the emergency exit. A.- True. B.- False. 10.- What does illumination of the red cabin pressure light represent on the main cabin door? A.- This indicates that the evacuation slide is armed. B.- This indicates thar the aircraft cabin is still pressurized and the cabin door should not be opened. C.- Both are correct. 11.- You want to open the cabin door, while lifting the control handle the white light illuminates. What does it mean? A.- There is residual pressure in the cabin. B.- The ramp is not correctly positioned. C.- The slide is still armed. D.- Somebody is trying to open the door from aoutside. 12.- Which situation will automatically illuminate the escape path lighting? A.- The loss of power to the DC ESS SHED bus and the loss of power to the AC bus #1. B.- The loss of power to the AC ESS SHED bus and the loss of power to the AC bus #1. C.- The loss of power to the AC ESS SHED and the loss of power to the DC ESS SHED. D.- The loss of power to the AC ESS SHED. 13.- When the door arming lever is in the ARMED position, opening the door from the outside will: A.- Automatically deploy and inflate the evacuation slide. B.- Disarm the door. C.- The power assist will rapidly open the door. 14.- With the EMER EXIT LT selector in the ARM position. If AC bus #1 is unpowered: A.- The escape path markings will automatically illuminate. B.- The emergency lights and exit signs will illuminate automatically. C.- Both are correct. 15.- Opening an emergency overwing exit will: A.- Inflate the slide at the leading edge of the wing. B.- Automatically inflate the double lane slide off the trailing edge of the wing. C.- Only arm the overwing slide. 16.- What are the indications that the PBE oxygen supply has depleted? A.- The hood collapses to the point that it touches your face or by a flashing red light in addition to the flashing green light. B.- The sound of the oxyen flow stops and flashing red and green lights appear. C.- No 02 supply indications & lights only indicate time. D.- all of the above. 17.- How many cabin entrance, overwing emergency exits and cargo doors are on the A-320? A.- Four cabin, two overwings, and two cargo, plus the bulk cargo. B.- Four cabin, four overwings , an two cargo, plus the bulk cargo. C.- Two cabin, four overwings, and three cargo, plus the bulk cargo. 18.- The SLIDE ARMED LIGHT illuminates white on the passenger cabin entry doors when: A.- The door is not armed. B.- The door is armed. C.- The control handle is operated with the slide armed. 19.- The ECAM will display a door not locked in: A.- Amber. B.- Red. C.- Green. 20.- The A-320 cargo doors can be operated by either an ___ or a ____to pressurize the _____ hydraulic system. A.- Electric pump, hand pump, green. B.- Mechanical pump, hand pump, yellow. C.- Electric pump, hand pump, yellow. 21.- How is it determined that the cockpit sliding window is closed and locked? A.- The red ring below the release button should not be in view. B.- The red ring below the release button should be in view. C.- The locking pin was placed in the forward position when the window was closed. D.- The pin is engaged. 22.- How is crew oxygen provide? A.- From a single bottle. B.- There is one bottle per crew member except for jump seats. C.- Oxygen generator. D.- One oxygen bottle with an oxygen generator. 23.- What cockpit lighting is available during an Emergency Electrical Configuration (EEC)? A.- All lights are fully functional. B.- Dome lights, main panel flood lights, and the standby compass light. C.- Dome light (right side only), main panel flood lights, and the standby compass light. D.- Dome light (right side only), main panel flood lights (left two columns only), and the standby compass light. 24.- What does HORN SHUTOFF on the EVAC panel do? A.- Cancels the EVAC alert. B.- Silences EVAC signals throughout the cabin and cockpit. C.- Silences Horn in cockpit. D.- None of the above. 25.- The HALON fire extinguisher should be used on what type fires? A.- Electrical fires only. B.- Electrical and burning metals. C.- Electrical and flammable liquid fires. D.- Electrical and ordinary combustibles. 26.- On the ECAM DOOR/OXY page, the SLIDE indication appears ____ when the slide is not disarmed. A.- White. B.- Amber. C.- Green. D.- Red. 27.- Each passenger door has one CABIN PRESSURE warning light that: A.- Warns of residual pressure in the cabin. B.- Shows a possible unlocked door. C.- Both are correct. 28.- Where does the Door and Slide Control System (DSCS) generate warnings? A.- On ECAM. B.- On the doors. C.- Both are correct. 29.- What does illumination of the white slide armed light represent on the main cabin door? A.- This indicates that the slide has properly inflated and is safe for use. B.- This indicates that the slide is armed and the slide will inflate if the door is opened from inside the aircraft. C.- This indicates that the main cabin door has not been properly closed. D.- This indicates that the main cabin door has not been properly closed but the slide is properly armed. 30.- Can the flight compartment sliding windows be used as emergency exits? A.- Yes, in the cockpit coat closet is a rope ladder that can be used in such an event. B.- Yes, there are escape ropes mounted above each window behind an access panel. C.- No. They are not approved emergency exits. D.- No, they are too small. 31.- When the slide arming liver, on the emergency opening system, is in the ARMED position, where is the slide connected? A.- To the brackets on the underside of the fuselage. B.- To the brakets on the above the door. C.- To the floor brackets on both sides of the door. D.- All of the above. 32.- When the Cargo door switch for the yellow hydraulic pump is in use, the flight controls are: A.- Fully operational. B.- Inhibited. C.- Hydraulically locked by pressure from the electric pump. D.- Only operated by the green system. 33.- The cockpit door: A.- Can only be open into the cockpit. B.- Can only open into the cabin. C.- Normally opens into the cockpit but can be forced in either direction. D.- Slides in either direction. 34.- When opened in an emergency, the passenger entry doors: A.- They are Pneumatically assisted into the open position. B.- Will need two cabin crew to push them open. C.- Are assisted to the open position by slide inflation. D.- Are electrically assisted into the open position. 35.- The cockpit windows can be opened both from inside and outside. A.- True. B.- False. C.- From inside only. |
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